Raytheon Technologies Corporation

United States of America

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IPC Class
H01M 8/18 - Regenerative fuel cells, e.g. redox flow batteries or secondary fuel cells 35
H01M 8/20 - Indirect fuel cells, e.g. fuel cells with redox couple being irreversible 21
H01M 8/04186 - Arrangements for control of reactant parameters, e.g. pressure or concentration of liquid-charged or electrolyte-charged reactants 11
F17C 1/16 - Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge constructed of plastics materials 10
B29L 31/00 - Other particular articles 8
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1.

AXIAL COMPRESSOR STATOR

      
Application Number 17960514
Status Pending
Filing Date 2022-10-05
First Publication Date 2024-04-18
Owner RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor Power, Bronwyn

Abstract

An airfoil includes a high pressure surface and a low pressure surface that are connected at a leading edge and a trailing edge. The high pressure surface and the low pressure surface extend from a first end to a second end. A camber line extends between the leading edge and the trailing edge and a camber angle is defined as a plurality of camber-angle distributions that extend between the leading edge end and the trailing edge. The plurality of camber-angle distributions include a uniform portion that extends from the leading edge to a forced non-equilibrium boundary layer diffusion (FNBD) feature. The uniform portion includes a non-dimensionalized camber-angle unit that is constant the FNBD feature includes a rapidly increasing camber-angle that is 0.2 non-dimensional camber-angle units higher than the non-dimensionalized camber-angle of the uniform portion.

IPC Classes  ?

  • F01D 9/04 - Nozzles; Nozzle boxes; Stator blades; Guide conduits forming ring or sector

2.

SEGMENTED HEAT EXCHANGER

      
Application Number 17966652
Status Pending
Filing Date 2022-10-14
First Publication Date 2024-04-18
Owner Raytheon Technologies Corporation (USA)
Inventor
  • Snyder, Isabella
  • Gerlach, David W
  • Snape, Nathan A

Abstract

A method can comprise dividing a heat exchanger design into a plurality of modules, the plurality of modules arranged in a grid, each module in the plurality of modules including: a first fluid conduit defining an inlet, an outlet, and a heat-transfer surface, and a first flow direction, and a second fluid conduit defining a second inlet, a second outlet, a second heat-transfer surface, and a second flow direction, the second flow direction different from the first flow direction; and determining a heat-transfer augmenter arrangement for the first fluid conduit and the second fluid conduit of each module in the plurality of modules based on a stress threshold of the module in the plurality of modules.

IPC Classes  ?

  • F28F 13/06 - Arrangements for modifying heat transfer, e.g. increasing, decreasing by affecting the pattern of flow of the heat-exchange media

3.

INTEGRALLY BLADED ROTOR WITH LEADING EDGE SHIELD

      
Application Number 17967361
Status Pending
Filing Date 2022-10-17
First Publication Date 2024-04-18
Owner Raytheon Technologies Corporation (USA)
Inventor Knaul, David A.

Abstract

An integrally bladed rotor for a gas turbine engine, including: a plurality of blades integrally formed with a hub as a single component, each of the plurality of blades having a blade body extending from the hub to an opposing blade tip surface along a longitudinal axis, each blade body having a pressure side and a suction side each extending between a leading edge and a trailing edge of the blade body; and each of the plurality of blades including a leading edge shield secured to the leading edge of the blade body.

IPC Classes  ?

  • F01D 5/14 - Form or construction
  • F01D 5/34 - Rotor-blade aggregates of unitary construction

4.

COOLING FEATURES FOR A COMPONENT OF A GAS TURBINE ENGINE

      
Application Number 17965311
Status Pending
Filing Date 2022-10-13
First Publication Date 2024-04-18
Owner Raytheon Technologies Corporation (USA)
Inventor
  • Maldonado, Billie R.
  • Drake, Jeremy T.
  • Tyler, Terence
  • Romanov, Dmitriy A.

Abstract

A component for a gas turbine engine, including: at least one internal channel extending through a first portion of the component, the at least one internal channel having at least one inlet opening and at least one outlet opening each being in fluid communication with the at least one internal channel; a plurality of cooling features extending from a surface of the at least one internal channel; and at least one internal channel extending through a second portion of the component, the at least one internal channel extending through the second portion of the component is in fluid communication with the at least one internal channel extending through the first portion of the component, the second portion being located on top of the first portion, the at least one internal channel extending through the second portion of the component having a plurality of openings extending from the least one internal channel extending through the second portion of the component through the plurality of cooling features to an outer surface of the component.

IPC Classes  ?

  • F01D 11/24 - Actively adjusting tip-clearance by selectively cooling or heating stator or rotor components
  • F01D 25/12 - Cooling

5.

REDUCING NOISE FROM A COMBUSTOR OF A GAS TURBINE ENGINE

      
Application Number 18164491
Status Pending
Filing Date 2023-02-03
First Publication Date 2024-03-28
Owner RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Locke, Justin M
  • Moura, Dennis M
  • Mccormick, Duane C
  • Liljenberg, Scott A
  • Strickland, Theodore R
  • Proscia, William

Abstract

A method of reducing noise from a combustor of a gas turbine engine includes the steps of establishing a maximum noise limit that may be for a particular frequency range. A primary fuel flow percentage, which may be emitted from a fuel nozzle arrangement having various groupings of simplex and duplex nozzles, is then established. An immersion depth measured between an aft rim of a swirler and a distal tip of the fuel nozzles may then be reduced thereby reducing the noise amplitude.

IPC Classes  ?

  • F23R 3/28 - Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
  • F23D 11/38 - Nozzles; Cleaning devices therefor
  • F23K 5/06 - Liquid fuel from a central source to a plurality of burners
  • F23R 3/06 - Arrangement of apertures along the flame tube
  • F23R 3/12 - Air inlet arrangements for primary air inducing a vortex
  • F23R 3/14 - Air inlet arrangements for primary air inducing a vortex by using swirl vanes
  • F23R 3/34 - Feeding into different combustion zones
  • F23R 3/50 - Combustion chambers comprising an annular flame tube within an annular casing

6.

STEAM INJECTED INTER-TURBINE BURNER ENGINE

      
Application Number 17951879
Status Pending
Filing Date 2022-09-23
First Publication Date 2024-03-28
Owner RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Lei Ma, David
  • Staubach, Joseph B.

Abstract

A turbine engine assembly includes a turbine section including at plurality of turbine stages through which the gas flow expands to generate a mechanical power output. An inter-turbine burner between at least two of the plurality of turbine stages reheats the gas flow. A condenser extracts water from the gas flow exhausted from the turbine section, and an evaporator heats the water extracted by the condenser to generate a steam flow with the steam flow communicated to the inter-turbine burner and added to the gas flow expanded through the turbine section.

IPC Classes  ?

  • F02C 3/30 - Adding water, steam or other fluids to the combustible ingredients or to the working fluid before discharge from the turbine

7.

AIR RECUPERATED ENGINE WITH AIR REINJECTION

      
Application Number 17951972
Status Pending
Filing Date 2022-09-23
First Publication Date 2024-03-28
Owner RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Taylor, Stephen H.
  • Retersdorf, Alan
  • Atassi, Oliver V.
  • Snape, Nathan A.

Abstract

A gas turbine engine assembly including a tap that is at a location up stream of the combustor section for drawing a bleed airflow. An exhaust heat exchanger is configured to transfer thermal energy from the exhaust gas flow into the bleed airflow and communicate the heated bleed airflow into the turbine section where it is expanded to drive the turbine section.

IPC Classes  ?

  • F02C 6/08 - Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas the gas being bled from the gas-turbine compressor
  • F02C 9/18 - Control of working fluid flow by bleeding, by-passing or acting on variable working fluid interconnections between turbines or compressors or their stages
  • F02G 5/00 - Profiting from waste heat of combustion engines, not otherwise provided for
  • F02K 3/02 - Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber

8.

PIN-FIN COOLING FOR PRINTED CIRCUIT BOARDS (PCBS)

      
Application Number 17946160
Status Pending
Filing Date 2022-09-16
First Publication Date 2024-03-21
Owner Raytheon Technologies Corporation (USA)
Inventor
  • Lee, Yongduk
  • Gupta, Ankit
  • Alahyari, Abbas A.
  • Kshirsagar, Parag M.

Abstract

Direct pin-fin cooling assemblies are disclosed for a high-power printed circuit boards (PCBs). The disclosure can solve the classical coldplate problem associated with liquid cooling of high-power PCBs namely: (1) Inhomogeneous cooling due to the calorimetric heating up of the coolant, (2) thermal interface material (TIM) related quality issues such as dry-out effects, (3) high cost due to complicated metal coldplate structure, and (4) low thermal conductivity due to multi-layer structure. This includes incorporating pin-fin direct cooling into high-power PCB structures without additional coldplate structure or TIM. In this approach, a TIM and a top plate of coldplate can be removed. Thus, the cooling performance can be improved because the thermal conductivity between a liquid coolant and a power device is increased.

IPC Classes  ?

  • H05K 1/02 - Printed circuits - Details
  • H05K 3/30 - Assembling printed circuits with electric components, e.g. with resistor

9.

IN-SITU SOLID CHEMICAL VAPOR DEPOSITION PRECURSOR DELIVERY

      
Application Number 17888757
Status Pending
Filing Date 2022-08-16
First Publication Date 2024-02-22
Owner Raytheon Technologies Corporation (USA)
Inventor
  • Nable, Jun
  • She, Ying
  • Sudre, Olivier H.

Abstract

A chemical vapor deposition system comprises a reactor including at least one wall extending between an inlet end and an outlet end, and an internal volume defined by the at least one wall, the inlet end, and the outlet end. The reactor further comprises a heat source in thermal communication with the internal volume, and a solid precursor container removably placed within the internal volume. The solid precursor container includes at least one internal cavity for holding an amount of the solid precursor, and an opening fluidly connecting the at least one internal cavity to the internal volume of the reactor. The solid precursor comprises at least one of aluminum, zirconium, hafnium, and a rare earth metallic element.

IPC Classes  ?

  • C23C 16/448 - Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition (CVD) processes characterised by the method of coating characterised by the method used for generating reactive gas streams, e.g. by evaporation or sublimation of precursor materials
  • C23C 16/34 - Nitrides

10.

SEAL COAT

      
Application Number 17888996
Status Pending
Filing Date 2022-08-16
First Publication Date 2024-02-22
Owner Raytheon Technologies Corporation (USA)
Inventor
  • Nable, Jun
  • She, Ying

Abstract

A coating for an article includes a seal coat comprising self-healing particles disposed in a seal coat matrix and a bond coat disposed on the seal coat. The bond coat includes a matrix, diffusive particles disposed in the matrix, and gettering particles disposed in the matrix. A coating for an article and a method of applying a coating to an article are also disclosed.

IPC Classes  ?

  • C04B 41/50 - Coating or impregnating with inorganic materials
  • C04B 41/45 - Coating or impregnating
  • C04B 41/87 - Ceramics
  • C04B 41/89 - Coating or impregnating for obtaining at least two superposed coatings having different compositions

11.

SURFACE TREATMENT SYSTEM DESIGN FOR HIGH FATIGUE LIFE HOLLOW FAN BLADES

      
Application Number 17892541
Status Pending
Filing Date 2022-08-22
First Publication Date 2024-02-22
Owner Raytheon Technologies Corporation (USA)
Inventor
  • Kuczek, Andrzej E.
  • El-Wardany, Tahany
  • Bedard, Benjamin
  • Klecka, Michael A.
  • Salva, Randy P.
  • Barnat, Krzysztof

Abstract

A system for deep rolling a fan blade including a shaft assembly disposed along a first axis; a hub connected to a distal end of the shaft assembly, the hub having an upper hub portion and a lower hub portion extending along a second axis, the second axis forming an angle relative to a first axis; a roller disk joined to the lower portion of the hub, the roller disk configured to contact a fan blade; a fixture supporting the fan blade; the fixture comprising a body supporting a pivot clamp attached to the body with a pivot; a support attached to the body, the support is configured to engage an airfoil portion of the fan blade; a receiver formed in the body for supporting a root of the fan blade; and a shoulder attached to the body configured to support a platform portion of the fan blade.

IPC Classes  ?

  • C22F 1/04 - Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
  • F01D 5/14 - Form or construction

12.

PREDICTIVE ANALYTICS SYSTEMS AND METHODS

      
Application Number 18222534
Status Pending
Filing Date 2023-07-17
First Publication Date 2024-02-08
Owner Raytheon Technologies Corporation (USA)
Inventor
  • Morris Ii, Robert Glenn
  • Montag, Mario
  • Thys, Phillippe

Abstract

Various examples of methods and systems are provided for improved predictive analytics. In one example, a method of managing operation of an asset or group of assets of interest includes comparing a generated prediction with one or more prediction range associated with a risk profile assigned to an operational outcome of interest, presenting a notification to an operator in response to the comparison, and incorporating operator-generated input as updated source data for the generation of subsequent predictions. The operator-generated input can comprise an operator-defined selection such as, e.g.,.; acceptance of the notification, or rejection of the notification. The operator-generated input can provide real time or near real time information based upon context-specific knowledge that the operator holds that is substantially independent of historical source data.

IPC Classes  ?

  • G06Q 10/0635 - Risk analysis of enterprise or organisation activities
  • G06N 5/04 - Inference or reasoning models

13.

RADIAL LIFT SEAL

      
Application Number 18224130
Status Pending
Filing Date 2023-07-20
First Publication Date 2023-11-16
Owner Raytheon Technologies Corporation (USA)
Inventor
  • Miller, Jonathan Logan
  • Zimmitti, Jonathan F.
  • Schwartz, Benstone
  • Tessier, Jeffrey E.

Abstract

A bearing compartment seal for a gas turbine engine includes a seal ring that defines an axis and has a radially inward facing sealing surface. A seal runner is configured to rotate relative to the seal ring. The seal runner has a runner surface facing the radially inward facing sealing surface. A plurality of grooves are spaced circumferentially along the runner surface. The plurality of grooves have a length in an axial direction that is at least 50% of an axial length of the runner surface.

IPC Classes  ?

  • F01D 11/00 - Preventing or minimising internal leakage of working fluid, e.g. between stages
  • F01D 25/16 - Arrangement of bearings; Supporting or mounting bearings in casings

14.

GEARED GAS TURBINE ENGINE WITH OIL DEAERATOR AND AIR REMOVAL

      
Application Number 18358524
Status Pending
Filing Date 2023-07-25
First Publication Date 2023-11-16
Owner Raytheon Technologies Corporation (USA)
Inventor Sheridan, William G.

Abstract

A gas turbine engine has a fan drive turbine for driving a gear reduction. The gear reduction drives a fan rotor. A lubrication system supplies oil to the gear reduction, and includes a lubricant pump to supply an air/oil mixture to an inlet of a deaerator. The deaerator includes a separator for separating oil and air, delivering separated air to an air outlet, and delivering separated oil back into an oil tank. The separated oil is first delivered into a pipe outwardly of the oil tank, and then into a location beneath a minimum oil level in the tank. Air within the oil tank moves outwardly through an air exit into the deaerator. A method of designing a gas turbine engine is also disclosed.

IPC Classes  ?

15.

REDOX FLOW BATTERY WITH RAMAN SPECTROMETER

      
Application Number 17721509
Status Pending
Filing Date 2022-04-15
First Publication Date 2023-10-19
Owner RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Davenport, Timothy C.
  • Saraidaridis, James Demetrios

Abstract

A redox flow battery includes a cell that has first and second electrodes and an ion-exchange layer there between, first and second circulation loops that are fluidly connected with, respectively, the first and second electrodes, first and second electrolyte storage tanks in, respectively, the first and second circulation loops, first and second electrolytes contained in, respectively, the first and second circulation loops, and a Raman spectrometer on at least one of the first or second circulation loops for determining a state-of-charge of at least one of the first or second electrolytes. The Raman spectrometer includes a laser source that is rated to emit a laser of a wavelength of 694 nanometers to 1444 nanometers.

IPC Classes  ?

  • H01M 8/18 - Regenerative fuel cells, e.g. redox flow batteries or secondary fuel cells
  • G01R 31/382 - Arrangements for monitoring battery or accumulator variables, e.g. SoC
  • G01R 31/378 - Arrangements for testing, measuring or monitoring the electrical condition of accumulators or electric batteries, e.g. capacity or state of charge [SoC] specially adapted for the type of battery or accumulator
  • G01N 21/65 - Raman scattering
  • H01M 8/0444 - Concentration; Density
  • H01M 8/04186 - Arrangements for control of reactant parameters, e.g. pressure or concentration of liquid-charged or electrolyte-charged reactants

16.

NON-CONTACTING DYNAMIC SEAL

      
Application Number 18311443
Status Pending
Filing Date 2023-05-03
First Publication Date 2023-09-21
Owner RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Wilson, Ross
  • Farris, John R.
  • Mccaffrey, Michael G.
  • Hall, Theodore W.
  • Korzendorfer, John J.
  • Vinson, Elizabeth F.
  • Jacques, Jeffrey Michael
  • Paul, John E.
  • Otero, Edwin
  • Stoner, Alan W.

Abstract

A method of damping vibrations in a seal includes inserting a first wave spring between a first beam and a second beam of the seal. The seal can be for a gas turbine engine and can include a full hoop outer ring, a shoe coupled to the full hoop outer ring via the first beam (e.g., an outer beam) and the second beam (e.g., an inner beam), and the first wave spring in contact with the first beam and the second beam.

IPC Classes  ?

  • F01D 11/02 - Preventing or minimising internal leakage of working fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type
  • F16J 15/44 - Free-space packings
  • F16F 15/06 - Suppression of vibrations of non-rotating, e.g. reciprocating, systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating system using elastic means with metal springs
  • F01D 25/04 - Antivibration arrangements

17.

LOW NOISE TURBINE FOR GEARED TURBOFAN ENGINE

      
Application Number 18201875
Status Pending
Filing Date 2023-05-25
First Publication Date 2023-09-21
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • MTU Aero Engines AG (Germany)
Inventor
  • Morin, Bruce L.
  • Korte, Detlef

Abstract

An aircraft system includes, among other things, an aircraft and a gas turbine engine coupled to the aircraft. The gas turbine engine includes a propulsor section including a propulsor, a compressor section, a turbine section including a first turbine and a second turbine, and a gear reduction between the propulsor and the second turbine. The second turbine includes a number of turbine blades in each of a plurality of rows of the second turbine. The second turbine blades operating at least some of the time at a rotational speed. The number of blades and the rotational speed being such that the following formula holds true for a majority of the blade rows of the second turbine: 5500 Hz≤(number of blades×speed)/60 sec≤10000 Hz. The gas turbine engine is rated to produce 15,000 pounds of thrust or more.

IPC Classes  ?

  • F04D 29/66 - Combating cavitation, whirls, noise, vibration, or the like; Balancing
  • F02C 3/107 - Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with two or more rotors connected by power transmission
  • F02K 3/04 - Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low-pressure outputs, for augmenting jet thrust, e.g. of double-flow type
  • G06F 30/17 - Mechanical parametric or variational design
  • F01D 15/12 - Combinations with mechanical gearing
  • F04D 29/32 - Rotors specially adapted for elastic fluids for axial-flow pumps
  • F01D 5/14 - Form or construction
  • F02C 3/04 - Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
  • F02K 3/06 - Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low-pressure outputs, for augmenting jet thrust, e.g. of double-flow type with front fan
  • F01D 5/06 - Blade-carrying members, e.g. rotors - Details thereof, e.g. shafts, shaft connections
  • F01D 25/24 - Casings; Casing parts, e.g. diaphragms, casing fastenings
  • F02C 7/36 - Power transmission between the different shafts of the gas-turbine plant, or between the gas-turbine plant and the power user
  • F04D 25/04 - Units comprising pumps and their driving means the pump being fluid-driven
  • F04D 29/053 - Shafts

18.

CELL FOR ELECTROCHEMICALLY DETERMINING ACTIVE SPECIES CONCENTRATIONS IN REDOX FLOW BATTERIES

      
Application Number 18088440
Status Pending
Filing Date 2022-12-23
First Publication Date 2023-04-27
Owner RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Saraidaridis, James D.
  • Yang, Zhiwei

Abstract

A redox flow battery system with a redox flow battery includes a redox flow cell, and a supply/storage system external of the redox flow cell. The supply/storage system includes first and second electrolytes for circulation through the redox flow cell. At least the first electrolyte is a liquid electrolyte that has electrochemically active species with multiple, reversible oxidation states. A secondary cell is fluidly connected with the first electrolyte and is operable to monitor concentration of one or more of the electrochemically active species. The secondary cell includes a counter electrode, a working microelectrode, and an ionically conductive path formed by the first electrolyte between the counter electrode and the working microelectrode.

IPC Classes  ?

  • H01M 8/04186 - Arrangements for control of reactant parameters, e.g. pressure or concentration of liquid-charged or electrolyte-charged reactants
  • H01M 8/04082 - Arrangements for control of reactant parameters, e.g. pressure or concentration
  • H01M 8/0444 - Concentration; Density
  • H01M 8/18 - Regenerative fuel cells, e.g. redox flow batteries or secondary fuel cells

19.

PHYSIOLOGICAL AND BEHAVIOURAL METHODS TO ASSESS PILOT READINESS

      
Application Number 17746539
Status Pending
Filing Date 2022-05-17
First Publication Date 2022-12-08
Owner RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Rao, Arjun Harsha
  • Wu, Peggy
  • Matessa, Michael P.
  • Wittkop, Timothy J.
  • George, Christopher L
  • Johnson, Wade T.

Abstract

A system and method for automatically assessing pilot readiness via a plurality of biometric sensors includes continuously receiving biometric data including vision-based data; the biometric vision-based data is compared to a task specific set of movements and facial expressions as defined by known anchor points. A deviation is calculated based on the vision-based data and task specific set of movements and expressions, and the deviation is compared to an acceptable threshold for pilot readiness. Other biometric data may be included to refine the readiness assessment.

IPC Classes  ?

  • A61B 5/18 - Devices for psychotechnics; Testing reaction times for vehicle drivers
  • A61B 5/16 - Devices for psychotechnics; Testing reaction times
  • A61B 5/318 - Heart-related electrical modalities, e.g. electrocardiography [ECG]
  • A61B 5/369 - Electroencephalography [EEG]
  • A61B 5/308 - Input circuits therefor specially adapted for particular uses for electrocardiography [ECG]
  • A61B 5/31 - Input circuits therefor specially adapted for particular uses for electroencephalography [EEG]
  • A61B 5/00 - Measuring for diagnostic purposes ; Identification of persons
  • G10L 13/02 - Methods for producing synthetic speech; Speech synthesisers
  • G10L 25/57 - Speech or voice analysis techniques not restricted to a single one of groups specially adapted for particular use for comparison or discrimination for processing of video signals
  • G06V 20/40 - Scenes; Scene-specific elements in video content
  • G06V 20/59 - Context or environment of the image inside of a vehicle, e.g. relating to seat occupancy, driver state or inner lighting conditions
  • G06V 40/18 - Eye characteristics, e.g. of the iris
  • B64D 45/00 - Aircraft indicators or protectors not otherwise provided for

20.

Alkaline manganese redox flow battery with inhibitor

      
Application Number 17326518
Grant Number 11664518
Status In Force
Filing Date 2021-05-21
First Publication Date 2022-11-24
Grant Date 2023-05-30
Owner RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Davenport, Timothy
  • Saraidaridis, James D.
  • Darling, Robert Mason

Abstract

A redox flow battery includes a redox flow cell and a supply and storage system external of the redox flow cell. The supply and storage system includes first and second electrolytes for circulation through the redox flow cell. The first electrolyte is a liquid electrolyte having electrochemically active manganese species with multiple, reversible oxidation states in the redox flow cell. The electrochemically active manganese species may undergo reactions that cause precipitation of manganese oxide solids. The first electrolyte includes an inhibitor that limits the self-discharge reactions. The inhibitor includes an oxoanion compound.

IPC Classes  ?

  • H01M 8/18 - Regenerative fuel cells, e.g. redox flow batteries or secondary fuel cells

21.

Three-dimensional diffuser-fin heat sink with integrated blower

      
Application Number 17171389
Grant Number 11686536
Status In Force
Filing Date 2021-02-09
First Publication Date 2022-08-11
Grant Date 2023-06-27
Owner RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Savlers, Kimberly Rae
  • Pearson, Matthew Robert

Abstract

A heat exchanger system is provided and includes a heat sink, fins arrayed on a central region of the heat sink to form channels between adjacent fins and an integrated blower. Each of the fins extends radially outwardly from the central region and has a height that increases with increasing distance from the central region. The integrated blower is disposed at the central region to generate flows of coolant directed into and through the channels.

IPC Classes  ?

  • F28F 3/02 - Elements or assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with recesses, with corrugations
  • H01L 23/467 - Arrangements for cooling, heating, ventilating or temperature compensation involving the transfer of heat by flowing fluids by flowing gases, e.g. air
  • F28F 13/06 - Arrangements for modifying heat transfer, e.g. increasing, decreasing by affecting the pattern of flow of the heat-exchange media

22.

Redox flow battery with improved efficiency

      
Application Number 17119427
Grant Number 11271226
Status In Force
Filing Date 2020-12-11
First Publication Date 2022-03-08
Grant Date 2022-03-08
Owner Raytheon Technologies Corporation (USA)
Inventor
  • Saraidaridis, James D.
  • Perry, Michael L.
  • Darling, Robert Mason

Abstract

A method for a redox flow battery includes using a cell of a redox flow battery to store electrical energy and discharge the stored electrical energy. The using includes circulating a first electrolyte solution through a first circulation loop in fluid connection with the first electrode of the cell; circulating a second electrolyte solution through a second circulation loop in fluid connection with the second electrode of the cell; and at least one of a first element from the first electrolyte solution in the first electrode permeates through the separator layer and precipitates as a first solid product in the second electrode and a second element from the second electrolyte solution permeates through the separator layer and precipitates a second solid product in the first electrode. The method also includes removing at least a portion of the first solid product or the second solid product from the first electrode and the second electrode, respectively.

IPC Classes  ?

  • H01M 8/04186 - Arrangements for control of reactant parameters, e.g. pressure or concentration of liquid-charged or electrolyte-charged reactants
  • H01M 8/18 - Regenerative fuel cells, e.g. redox flow batteries or secondary fuel cells
  • H01M 8/08 - Fuel cells with aqueous electrolytes
  • H01M 8/04082 - Arrangements for control of reactant parameters, e.g. pressure or concentration

23.

REMOVING NON-HOMOGENEOUS ICE FROM A FUEL SYSTEM

      
Application Number 17460617
Status Pending
Filing Date 2021-08-30
First Publication Date 2021-12-16
Owner Raytheon Technologies Corporation (USA)
Inventor Hagshenas, Behzad

Abstract

The presently disclosed embodiments utilize an ice separator vessel to trap ice particles in a non-homogeneous ice/fuel mixture flowing in a fuel system. A source of heat, such as heated fuel provided to the ice separator vessel, is used to melt at least a portion of the ice particles so that they do not enter the fuel system downstream of the ice separator vessel.

IPC Classes  ?

  • F02C 7/224 - Heating fuel before feeding to the burner
  • F02C 7/236 - Fuel delivery systems comprising two or more pumps
  • B01D 21/00 - Separation of suspended solid particles from liquids by sedimentation
  • B01D 21/26 - Separation of sediment aided by centrifugal force
  • B04B 15/02 - Other accessories for centrifuges for cooling, heating, or heat insulating

24.

INTERMEDIATE TEMPERATURE METAL SUPPORTED SOLID OXIDE ELECTROLYZER

      
Application Number 17262246
Status Pending
Filing Date 2018-07-25
First Publication Date 2021-11-11
Owner RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Zhu, Tianli
  • Hawkes, Justin R.
  • Rampone, Joseph C.

Abstract

A metal-supported electrolyzer includes an electrolysis cell that has, in stacked order, an electrode unit having a first solid oxide electrode layer, a solid oxide electrolyte layer that is proton-conductive in a temperature range of 650° C. or lower, and a second solid oxide electrode layer. A porous metal sheet in contact with the second solid oxide electrode layer supports the electrode unit, a metal separator sheet bonded to the porous metal sheet, and a metal interconnect backing the metal separator sheet.

IPC Classes  ?

  • H01M 4/90 - Selection of catalytic material
  • C25B 9/73 - Assemblies comprising two or more cells of the filter-press type
  • C25B 9/23 - Cells comprising dimensionally-stable non-movable electrodes; Assemblies of constructional parts thereof with diaphragms comprising ion-exchange membranes in or on which electrode material is embedded
  • H01M 8/126 - Fuel cells with solid electrolytes operating at high temperature, e.g. with stabilised ZrO2 electrolyte characterised by the process of manufacturing or by the material of the electrolyte the electrolyte consisting of oxides the electrolyte containing cerium oxide
  • C25B 15/08 - Supplying or removing reactants or electrolytes; Regeneration of electrolytes
  • H01M 4/86 - Inert electrodes with catalytic activity, e.g. for fuel cells

25.

Redox flow battery with electrolyte balancing and compatibility enabling features

      
Application Number 17361385
Grant Number 11637298
Status In Force
Filing Date 2021-06-29
First Publication Date 2021-10-21
Grant Date 2023-04-25
Owner RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor Perry, Michael L.

Abstract

A redox flow battery includes first and second cells. Each cell has electrodes and a separator layer arranged between the electrodes. A first circulation loop is fluidly connected with the first electrode of the first cell. A polysulfide electrolyte solution has a pH 11.5 or greater and is contained in the first recirculation loop. A second circulation loop is fluidly connected with the second electrode of the second cell. An iron electrolyte solution has a pH 3 or less and is contained in the second circulation loop. A third circulation loop is fluidly connected with the second electrode of the first cell and the first electrode of the second cell. An intermediator electrolyte solution is contained in the third circulation loop. The cells are operable to undergo reversible reactions to store input electrical energy upon charging and discharge the stored electrical energy upon discharging.

IPC Classes  ?

  • H01M 8/04186 - Arrangements for control of reactant parameters, e.g. pressure or concentration of liquid-charged or electrolyte-charged reactants
  • H01M 4/36 - Selection of substances as active materials, active masses, active liquids
  • H01M 8/04082 - Arrangements for control of reactant parameters, e.g. pressure or concentration
  • H01M 8/04791 - Concentration; Density
  • H01M 8/08 - Fuel cells with aqueous electrolytes
  • H01M 8/18 - Regenerative fuel cells, e.g. redox flow batteries or secondary fuel cells
  • H01M 8/2455 - Grouping of fuel cells, e.g. stacking of fuel cells with liquid, solid or electrolyte-charged reactants
  • H01M 8/20 - Indirect fuel cells, e.g. fuel cells with redox couple being irreversible

26.

Regeneration of flow battery

      
Application Number 16959703
Grant Number 11462761
Status In Force
Filing Date 2018-01-10
First Publication Date 2021-03-18
Grant Date 2022-10-04
Owner RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Perry, Michael L.
  • Sullivan, Joseph

Abstract

A redox flow battery includes a redox flow cell, a supply/storage system external of the redox flow cell, and a controller. The supply/storage system includes first and second electrolytes for circulation through the redox flow cell. The first electrolyte is a liquid electrolyte having electrochemically active species with multiple, reversible oxidation states. The electrochemically active species can form a solid precipitate blockage in the redox flow cell. The controller is configured to identify whether there is the solid precipitate blockage in the redox flow cell and, if so, initiate a regeneration mode that reduces the oxidation state of the electrochemically active species in the liquid electrolyte to dissolve, in situ, the solid precipitate blockage.

IPC Classes  ?

  • H01M 6/50 - Methods or arrangements for servicing or maintenance, e.g. for maintaining operating temperature
  • H01M 8/18 - Regenerative fuel cells, e.g. redox flow batteries or secondary fuel cells
  • H02J 7/00 - Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
  • H01M 8/04007 - Auxiliary arrangements, e.g. for control of pressure or for circulation of fluids related to heat exchange
  • H01M 8/0438 - Pressure; Ambient pressure; Flow
  • H01M 8/0444 - Concentration; Density
  • H01M 8/04746 - Pressure; Flow
  • H01M 8/04858 - Electric variables

27.

Redox flow battery system with electrochemical recovery cell

      
Application Number 16418120
Grant Number 11362359
Status In Force
Filing Date 2019-05-21
First Publication Date 2020-11-26
Grant Date 2022-06-14
Owner RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Perry, Michael L.
  • Darling, Robert Mason
  • Saraidaridis, James D.

Abstract

A redox flow battery system includes a redox flow battery that has a redox flow cell, and a supply/storage system external of the redox flow cell. The supply/storage system includes first and second electrolytes for circulation through the redox flow cell. At least the first electrolyte is an aqueous liquid electrolyte that has electrochemically active species with multiple, reversible oxidation states. There is a gas vent passage connected with the redox flow battery to receive water byproduct that evolves from side reaction of the first electrolyte. A bypass passage is connected with the supply/storage system to receive the aqueous electrolyte. An electrochemical recovery cell includes a first half-cell connected to the gas vent passage to receive as a reactant the water byproduct and a second half-cell connected to the bypass passage to receive as a reactant the first electrolyte.

IPC Classes  ?

  • H01M 8/18 - Regenerative fuel cells, e.g. redox flow batteries or secondary fuel cells
  • H01M 8/0662 - Treatment of gaseous reactants or gaseous residues, e.g. cleaning

28.

Brake roller with one way jaw clutch

      
Application Number 16506039
Grant Number 10882698
Status In Force
Filing Date 2019-07-09
First Publication Date 2020-11-26
Grant Date 2021-01-05
Owner Raytheon Technologies Corporation (USA)
Inventor
  • Shivalinga, Vinodkumar
  • Paliwal, Manu Siddharth

Abstract

A brake roller may comprise a brake shaft and a brake stack assembly located around the brake shaft. A one-way jaw clutch assembly may be configured to apply a force to the brake stack. A roller shell may be located radially outward of the brake stack. The one-way jaw clutch assembly may be configured to vary the force applied to the brake stack in response to a rotation of the roller shell in a circumferential direction.

IPC Classes  ?

  • B65G 13/075 - Braking means
  • F16D 11/10 - Clutches in which the members have interengaging parts actuated by moving a non-rotating part axially with clutching members movable only axially
  • F16D 41/18 - Freewheels or freewheel clutches with non-hinged detent
  • F16D 55/39 - Brakes with a plurality of rotating discs all lying side by side mechanically actuated by means of an intermediate leverage

29.

Cell for electrochemically determining active species concentrations in redox flow batteries

      
Application Number 16383017
Grant Number 11539061
Status In Force
Filing Date 2019-04-12
First Publication Date 2020-10-15
Grant Date 2022-12-27
Owner RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Saraidaridis, James D.
  • Yang, Zhiwei

Abstract

A redox flow battery system includes a redox flow battery that has a redox flow cell and a supply/storage system. The supply/storage system has first and second electrolytes for circulation through the redox flow cell. At least the first electrolyte is a liquid electrolyte that has electrochemically active species with multiple, reversible oxidation states. A secondary cell is operable to monitor concentration of one or more of the electrochemically active species. The secondary cell has a counter electrode, a flow passage that connects the counter electrode with the redox flow battery to receive the first or second electrolyte, a working electrode, and a separator. The working electrode is isolated from receiving the electrochemically active species of the first and second electrolytes except for a transport passage connecting the flow passage and the working electrode. The transport passage limits movement of the electrochemically active species to the working electrode.

IPC Classes  ?

  • H01M 8/04186 - Arrangements for control of reactant parameters, e.g. pressure or concentration of liquid-charged or electrolyte-charged reactants
  • H01M 8/04082 - Arrangements for control of reactant parameters, e.g. pressure or concentration
  • H01M 8/0444 - Concentration; Density
  • H01M 8/18 - Regenerative fuel cells, e.g. redox flow batteries or secondary fuel cells

30.

Ejection seat occupant camera system

      
Application Number 16368626
Grant Number 10887557
Status In Force
Filing Date 2019-03-28
First Publication Date 2020-10-01
Grant Date 2021-01-05
Owner Raytheon Technologies Corporation (USA)
Inventor
  • Benjamin, Jeff
  • Salois, Matthew D.

Abstract

An occupant camera system for an aircraft ejection assembly may comprise a fixed structure and a camera mounted to the fixed structure. A digital video recorder may be mounted to the fixed structure and electrically coupled to the camera. A switch may be electrically coupled to the digital video recorder, and a battery may be electrically coupled to the switch.

IPC Classes  ?

  • H04N 7/18 - Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast
  • B64D 25/10 - Ejector seats
  • H04N 5/77 - Interface circuits between an apparatus for recording and another apparatus between a recording apparatus and a television camera

31.

Systems and methods for brake failure detection using retract braking

      
Application Number 16206482
Grant Number 10882500
Status In Force
Filing Date 2018-11-30
First Publication Date 2020-06-04
Grant Date 2021-01-05
Owner Raytheon Technologies Corporation (USA)
Inventor Burte, Paul R.

Abstract

A system for detecting aircraft brake failure using retract braking may comprise a landing gear including a wheel, a brake coupled to the wheel, and a wheel sensor coupled to the wheel. A brake controller may be coupled to the brake and the wheel sensor. The brake controller may be configured to receive a begin retract braking signal, command the brake to apply a braking force to the wheel, calculate a wheel speed characteristic using data from the wheel sensor, and determine whether the wheel speed characteristic indicates a failure of the brake.

IPC Classes  ?

  • B60T 8/32 - Arrangements for adjusting wheel-braking force to meet varying vehicular or ground-surface conditions, e.g. limiting or varying distribution of braking force responsive to a speed condition, e.g. acceleration or deceleration
  • B60T 8/88 - Arrangements for adjusting wheel-braking force to meet varying vehicular or ground-surface conditions, e.g. limiting or varying distribution of braking force responsive to a speed condition, e.g. acceleration or deceleration with failure responsive means, i.e. means for detecting and indicating faulty operation of the speed responsive control means
  • B60T 17/22 - Devices for monitoring or checking brake systems; Signal devices
  • B64C 25/34 - Alighting gear characterised by elements which contact the ground or similar surface wheeled type, e.g. multi-wheeled bogies
  • B64C 25/42 - Arrangement or adaptation of brakes
  • B64D 45/00 - Aircraft indicators or protectors not otherwise provided for
  • B64C 25/24 - Operating mechanisms electric

32.

Redox flow battery with electrolyte balancing and compatibility enabling features

      
Application Number 16052727
Grant Number 11056698
Status In Force
Filing Date 2018-08-02
First Publication Date 2020-02-06
Grant Date 2021-07-06
Owner RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor Perry, Michael L.

Abstract

A redox flow battery includes first and second cells. Each cell has electrodes and a separator layer arranged between the electrodes. A first circulation loop is fluidly connected with the first electrode of the first cell. A polysulfide electrolyte solution has a pH 11.5 or greater and is contained in the first recirculation loop. A second circulation loop is fluidly connected with the second electrode of the second cell. An iron electrolyte solution has a pH 3 or less and is contained in the second circulation loop. A third circulation loop is fluidly connected with the second electrode of the first cell and the first electrode of the second cell. An intermediator electrolyte solution is contained in the third circulation loop. The cells are operable to undergo reversible reactions to store input electrical energy upon charging and discharge the stored electrical energy upon discharging.

IPC Classes  ?

  • H01M 8/04186 - Arrangements for control of reactant parameters, e.g. pressure or concentration of liquid-charged or electrolyte-charged reactants
  • H01M 8/18 - Regenerative fuel cells, e.g. redox flow batteries or secondary fuel cells
  • H01M 8/2455 - Grouping of fuel cells, e.g. stacking of fuel cells with liquid, solid or electrolyte-charged reactants
  • H01M 8/08 - Fuel cells with aqueous electrolytes
  • H01M 4/36 - Selection of substances as active materials, active masses, active liquids
  • H01M 8/04082 - Arrangements for control of reactant parameters, e.g. pressure or concentration
  • H01M 8/04791 - Concentration; Density

33.

Adjustable upper thoracic support for aircraft seat

      
Application Number 16029869
Grant Number 10882620
Status In Force
Filing Date 2018-07-09
First Publication Date 2020-01-09
Grant Date 2021-01-05
Owner Raytheon Technologies Corporation (USA)
Inventor
  • Ferguson, Keith M.
  • Sharpe, Jason Michael

Abstract

A seat for an aircraft may comprise a seat pan and a back support coupled to the seat pan. An upper thoracic support may be located proximate an end of the back support opposite the seat pan. The upper thoracic support may be configured to rotate relative to the back support. A headrest may be coupled to the upper thoracic support.

IPC Classes  ?

  • B64D 11/06 - Arrangements or adaptations of seats

34.

Method of making an energy storage article

      
Application Number 16312696
Grant Number 10892112
Status In Force
Filing Date 2016-06-24
First Publication Date 2019-10-31
Grant Date 2021-01-12
Owner RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Mcgee, Randolph Carlton
  • She, Ying
  • Dardas, Zissis A.

Abstract

A method of making an energy storage article having a metal nitride electrode is disclosed where metal nitride is made by nitriding particles of a metal or oxide of a metal selected from vanadium molybdenum, titanium, niobium, tungsten, or combinations including any of the foregoing by contacting the particles with a gas of nitrogen and hydrogen, or ammonia, in a fluidized bed reactor to form particles of metal nitride for the electrode.

IPC Classes  ?

  • H01G 11/86 - Processes for the manufacture of hybrid or EDL capacitors, or components thereof specially adapted for electrodes
  • H01G 11/30 - Electrodes characterised by their material
  • H01G 11/46 - Metal oxides
  • H01G 11/58 - Liquid electrolytes
  • H01G 11/26 - Electrodes characterised by their structure, e.g. multi-layered, porosity or surface features
  • C23C 8/24 - Nitriding

35.

Composite brake disks with an integrated heat sink, methods for manufacturing the same, and methods for producing encapsulated heat sink material

      
Application Number 16262576
Grant Number 10865841
Status In Force
Filing Date 2019-01-30
First Publication Date 2019-05-30
Grant Date 2020-12-15
Owner Raytheon Technologies Corporation (USA)
Inventor
  • Opalka, Susanne M.
  • Zafiris, Georgios S.
  • Li, Weina

Abstract

Brake disks with integrated heat sink are provided. Brake disk includes a fiber-reinforced composite material and an encapsulated heat sink material impregnated into the fiber-reinforced composite material. The encapsulated heat sink material comprises a heat sink material encapsulated within a silicon-containing encapsulation layer. Methods for manufacturing the brake disk with integrated heat sink and methods for producing the encapsulated heat sink material are also provided.

IPC Classes  ?

  • C04B 35/622 - Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
  • C04B 35/80 - Fibres, filaments, whiskers, platelets, or the like
  • C04B 35/83 - Carbon fibres in a carbon matrix
  • C04B 35/573 - Fine ceramics obtained by reaction sintering
  • F16D 65/12 - Discs; Drums for disc brakes
  • F16D 69/02 - Composition of linings
  • C04B 41/85 - Coating or impregnating with inorganic materials
  • C04B 41/00 - After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
  • C04B 41/50 - Coating or impregnating with inorganic materials
  • C04B 41/51 - Metallising
  • C04B 111/00 - Function, property or use of the mortars, concrete or artificial stone

36.

Deep convolutional neural networks for crack detection from image data

      
Application Number 16099485
Grant Number 10860879
Status In Force
Filing Date 2016-05-16
First Publication Date 2019-05-16
Grant Date 2020-12-08
Owner RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Giering, Michael J.
  • Reddy, Kishore K.
  • Venugopalan, Vivek

Abstract

A method includes detecting at least one region of interest in a frame of image data. One or more patches of interest are detected in the frame of image data based on detecting the at least one region of interest. A model including a deep convolutional neural network is applied to the one or more patches of interest. Post-processing of a result of applying the model is performed to produce a post-processing result for the one or more patches of interest. A visual indication of a classification of defects in a structure is output based on the result of the post-processing.

IPC Classes  ?

  • G06T 7/00 - Image analysis
  • G06F 16/55 - Clustering; Classification
  • G06N 5/04 - Inference or reasoning models
  • G06K 9/32 - Aligning or centering of the image pick-up or image-field
  • G06K 9/00 - Methods or arrangements for reading or recognising printed or written characters or for recognising patterns, e.g. fingerprints
  • G06K 9/46 - Extraction of features or characteristics of the image

37.

Composite pressure vessel assembly with an integrated nozzle assembly

      
Application Number 16095584
Grant Number 11047529
Status In Force
Filing Date 2016-04-22
First Publication Date 2019-05-02
Grant Date 2021-06-29
Owner RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Kuczek, Andrzej Ernest
  • Sun, Ellen Y.
  • Hawkes, Justin R.
  • Croteau, Paul F
  • Zhao, Wenping

Abstract

A pressure vessel assembly includes a vessel having a wall defining a chamber and a circumferentially continuous lip projecting into the chamber from the wall. The lip defines a through-bore that is in fluid communication with the chamber. A nozzle assembly of the pressure vessel assembly includes a tube projecting at least in-part into the through-bore, and an o-ring disposed between, and in sealing contact with, the tube and the lip.

IPC Classes  ?

  • F17C 1/16 - Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge constructed of plastics materials
  • F17C 1/00 - Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge

38.

Composite pressure vessel assembly and method of manufacturing

      
Application Number 16095570
Grant Number 10907768
Status In Force
Filing Date 2016-04-22
First Publication Date 2019-04-11
Grant Date 2021-02-02
Owner RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Zhao, Wenping
  • Sun, Ellen Y.
  • Croteau, Paul F.
  • Hawkes, Justin R.
  • Kuczek, Andrzej Ernest

Abstract

A composite pressure vessel assembly includes a first vessel having a first inner layer and a second vessel having a second inner layer. An outer layer of the assembly is in contact with and substantially envelopes the first and second inner layers. A junction of the assembly has outer boundaries defined by segments of the first inner layer, the second inner layer and the outer layer. A cross-layered component of the assembly is disposed in the junction, the first and second inner layers and the outer layer for adding strength to the junction and restricting delamination.

IPC Classes  ?

  • F17C 1/04 - Protecting sheatings
  • F17C 1/16 - Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge constructed of plastics materials
  • F17C 1/14 - Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge constructed of non-magnetic steel
  • B29C 65/56 - Joining of preformed parts; Apparatus therefor using mechanical means
  • B29C 70/70 - Completely encapsulating inserts
  • B29C 70/88 - Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced
  • B29L 31/00 - Other particular articles

39.

Composite pressure vessel assembly with an integrated nozzle assembly

      
Application Number 15779161
Grant Number 11137112
Status In Force
Filing Date 2015-11-25
First Publication Date 2018-12-13
Grant Date 2021-10-05
Owner RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Kuczek, Andrzej Ernest
  • Zhao, Wenping
  • Croteau, Paul F.
  • Sun, Ellen Y.

Abstract

A pressure vessel assembly includes a vessel including a wall defining a chamber and a circumferentially continuous lip projecting into the chamber from the wall. The lip defines a through-bore in fluid communication with the chamber. A nozzle assembly including a tube and a flange projecting radially outward from the tube. The tube includes a first portion projecting from the flange and through the through-bore and an opposite second portion projecting outward from the flange. The flange is in contact with the wall and the first portion includes an outer surface having a contour configured to produce sealing friction between the lip and the outer surface.

IPC Classes  ?

  • F17C 1/06 - Protecting sheatings built-up from wound-on bands or filamentary material, e.g. wires
  • F17C 11/00 - Use of gas-solvents or gas-sorbents in vessels
  • F17C 13/00 - VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES - Details of vessels or of the filling or discharging of vessels
  • F17C 1/16 - Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge constructed of plastics materials

40.

Oxidation resistant shot sleeve for high temperature die casting and method of making

      
Application Number 15608735
Grant Number 10682691
Status In Force
Filing Date 2017-05-30
First Publication Date 2018-12-06
Grant Date 2020-06-16
Owner RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Marcin, John Joseph
  • Shah, Dilip M.

Abstract

Shot sleeves for high temperature die casting include a low modulus single crystal nickel-based alloy having less than 1 ppm sulfur, a low modulus single crystal nickel-based alloy doped with a sulfur active element, a low modulus single crystal nickel-based alloy having a protective oxide coating, or a combination of two or more of the foregoing.

IPC Classes  ?

  • B22D 17/20 - Pressure die casting or injection die casting, i.e. casting in which the metal is forced into a mould under high pressure - Details
  • C22C 19/03 - Alloys based on nickel or cobalt based on nickel
  • C23C 8/12 - Oxidising using elemental oxygen or ozone

41.

COMPOSITE PRESSURE VESSEL ASSEMBLY AND METHOD OF MANUFACTURING

      
Application Number 15779146
Status Pending
Filing Date 2015-11-25
First Publication Date 2018-12-06
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Zhao, Wenping
  • Croteau, Paul F.
  • Kuczek, Andrzej Ernest
  • Sun, Ellen Y.
  • Wesson, John P.

Abstract

A composite pressure vessel assembly includes a first and second vessels aligned side-by-side. Each vessel has a liner defining respective chambers. First and second mid-layers of the assembly cover the respective liners with portions of the respective mid-layers being in contact with one-another. An outer layer of the vessel assembly is in contact with and substantially envelops both mid-layers except for the mid-layer portions.

IPC Classes  ?

  • F17C 1/06 - Protecting sheatings built-up from wound-on bands or filamentary material, e.g. wires
  • F17C 1/16 - Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge constructed of plastics materials
  • F17C 11/00 - Use of gas-solvents or gas-sorbents in vessels
  • F17C 13/04 - Arrangement or mounting of valves

42.

Predictive analytics systems and methods

      
Application Number 15910719
Grant Number 11748684
Status In Force
Filing Date 2018-03-02
First Publication Date 2018-11-01
Grant Date 2023-09-05
Owner Raytheon Technologies Corp. (USA)
Inventor
  • Morris, Ii, Robert Glenn
  • Montag, Mario
  • Thys, Philippe Georges Ivan Marie

Abstract

Various examples of methods and systems are provided for improved predictive analytics. In one example, a method of managing operation of an asset or group of assets of interest includes comparing a generated prediction with one or more prediction range associated with a risk profile assigned to an operational outcome of interest, presenting a notification to an operator in response to the comparison, and incorporating operator-generated input as updated source data for the generation of subsequent predictions. The operator-generated input can comprise an operator-defined selection such as, e.g., acceptance of the notification, or rejection of the notification. The operator-generated input can provide real time or near real time information based upon context-specific knowledge that the operator holds that is substantially independent of historical source data.

IPC Classes  ?

  • G06Q 10/0635 - Risk analysis of enterprise or organisation activities
  • H04W 4/38 - Services specially adapted for particular environments, situations or purposes for collecting sensor information
  • G06N 5/04 - Inference or reasoning models
  • G06N 5/045 - Explanation of inference; Explainable artificial intelligence [XAI]; Interpretable artificial intelligence
  • G06N 7/01 - Probabilistic graphical models, e.g. probabilistic networks
  • G06N 5/02 - Knowledge representation; Symbolic representation

43.

Composite vessel assembly and method of manufacture

      
Application Number 15481597
Grant Number 10422477
Status In Force
Filing Date 2017-04-07
First Publication Date 2018-10-11
Grant Date 2019-09-24
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Zhao, Wenping
  • Kuczek, Andrzej Ernest
  • Sun, Ellen Y.

Abstract

A composite vessel assembly includes a circumferentially continuous wall and an end cap. The wall includes a plurality of layers, and the end cap includes a plurality of steps. Each step of the plurality of steps is engaged to a respective layer of the plurality of layers.

IPC Classes  ?

  • F17C 1/16 - Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge constructed of plastics materials
  • F17C 1/04 - Protecting sheatings
  • B29C 70/34 - Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression
  • F17C 1/00 - Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge
  • F17C 1/06 - Protecting sheatings built-up from wound-on bands or filamentary material, e.g. wires
  • F17C 13/00 - VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES - Details of vessels or of the filling or discharging of vessels
  • B29L 31/00 - Other particular articles
  • B29K 105/08 - Condition, form or state of moulded material containing reinforcements, fillers or inserts of continuous length, e.g. cords, rovings, mats, fabrics, strands or yarns

44.

Mold-less curing method of manufacturing a composite vessel assembly

      
Application Number 15440448
Grant Number 10913210
Status In Force
Filing Date 2017-02-23
First Publication Date 2018-08-23
Grant Date 2021-02-09
Owner RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Zhao, Wenping
  • Sun, Ellen Y.

Abstract

A method of manufacturing a composite vessel assembly includes the step of placing the composite vessel assembly in a pliable containment prior to curing of a resin of the composite vessel assembly. With the composite vessel assembly in the pliable containment, a vacuum is applied through an orifice in the pliable containment to evacuate air and compact the composite vessel assembly.

IPC Classes  ?

  • B29C 65/02 - Joining of preformed parts; Apparatus therefor by heating, with or without pressure
  • B29C 63/00 - Lining or sheathing, i.e. applying preformed layers or sheathings of plastics; Apparatus therefor
  • B29C 65/00 - Joining of preformed parts; Apparatus therefor
  • B65B 3/02 - Machines characterised by the incorporation of means for making the containers or receptacles
  • B65B 31/00 - Packaging articles or materials under special atmospheric or gaseous conditions; Adding propellants to aerosol containers
  • B29C 70/44 - Shaping or impregnating by compression for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
  • B33Y 70/00 - Materials specially adapted for additive manufacturing
  • F17C 1/16 - Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge constructed of plastics materials
  • F17C 1/04 - Protecting sheatings
  • B29L 31/00 - Other particular articles

45.

Universal power electronic cell for distributed generation

      
Application Number 15751549
Grant Number 10381952
Status In Force
Filing Date 2015-10-02
First Publication Date 2018-08-16
Grant Date 2019-08-13
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Arnedo, Luis
  • Krishnamurthy, Shashank
  • Blasko, Vladimir

Abstract

A method of configuring a power conversion cell for a distributed power system according to an example of the present disclosure includes: importing one or more software modules onto a controller of a conversion device configured to control power conversion with one or more of the modules selected based on one or more of a load or source device, and the results of a software simulation.

IPC Classes  ?

  • H02M 7/538 - Conversion of dc power input into ac power output without possibility of reversal by static converters using discharge tubes with control electrode or semiconductor devices with control electrode using devices of a triode or transistor type requiring continuous application of a control signal using semiconductor devices only, e.g. single switched pulse inverters in a push-pull configuration
  • H02M 7/5387 - Conversion of dc power input into ac power output without possibility of reversal by static converters using discharge tubes with control electrode or semiconductor devices with control electrode using devices of a triode or transistor type requiring continuous application of a control signal using semiconductor devices only, e.g. single switched pulse inverters in a bridge configuration
  • H02J 3/38 - Arrangements for parallelly feeding a single network by two or more generators, converters or transformers
  • H02J 3/00 - Circuit arrangements for ac mains or ac distribution networks
  • H02M 1/00 - APPARATUS FOR CONVERSION BETWEEN AC AND AC, BETWEEN AC AND DC, OR BETWEEN DC AND DC, AND FOR USE WITH MAINS OR SIMILAR POWER SUPPLY SYSTEMS; CONVERSION OF DC OR AC INPUT POWER INTO SURGE OUTPUT POWER; CONTROL OR REGULATION THEREOF - Details of apparatus for conversion

46.

Sensor data fusion for prognostics and health monitoring

      
Application Number 15535909
Grant Number 11340602
Status In Force
Filing Date 2015-12-18
First Publication Date 2018-08-02
Grant Date 2022-05-24
Owner RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Giering, Michael J.
  • Shashanka, Madhusudana
  • Sarkar, Soumik
  • Venugopalan, Vivek

Abstract

A method includes converting time-series data from a plurality of prognostic and health monitoring (PHM) sensors into frequency domain data. One or more portions of the frequency domain data are labeled as indicative of one or more target modes to form labeled target data. A model including a deep neural network is applied to the labeled target data. A result of applying the model is classified as one or more discretized PHM training indicators associated with the one or more target modes. The one or more discretized PHM training indicators are output.

IPC Classes  ?

  • G05B 23/02 - Electric testing or monitoring
  • G06N 3/04 - Architecture, e.g. interconnection topology
  • G06K 9/62 - Methods or arrangements for recognition using electronic means
  • G06V 10/44 - Local feature extraction by analysis of parts of the pattern, e.g. by detecting edges, contours, loops, corners, strokes or intersections; Connectivity analysis, e.g. of connected components
  • G06V 20/56 - Context or environment of the image exterior to a vehicle by using sensors mounted on the vehicle
  • G06T 7/246 - Analysis of motion using feature-based methods, e.g. the tracking of corners or segments
  • G06N 3/08 - Learning methods

47.

Microgrid system and controller

      
Application Number 15579990
Grant Number 10514663
Status In Force
Filing Date 2015-06-12
First Publication Date 2018-06-21
Grant Date 2019-12-24
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Lin, Yiqing
  • Oggianu, Stella M.

Abstract

A microgrid controller includes a database in communication with a processor. The processor is operable to receive at least one microgrid input, to determine a first plurality of optimal power characteristic levels at a corresponding one of a plurality of first time intervals for a first time period, and to determine a second plurality of optimal power characteristic levels of a device determined at a corresponding one of a plurality of second time intervals for a second time period. The first time intervals are found at a first frequency different than a second frequency of the second time intervals. One of the second plurality of optimal power characteristic level corresponds to one of the first plurality of optimal power characteristic levels at each first time interval. The processor is configured to control a device optimal power characteristic level in response to the second plurality of optimal power characteristic levels.

IPC Classes  ?

  • G05D 3/12 - Control of position or direction using feedback
  • G05D 5/00 - Control of dimensions of material
  • G05D 17/00 - Control of torque; Control of mechanical power
  • G05D 9/00 - Level control, e.g. controlling quantity of material stored in vessel
  • G05D 11/00 - Control of flow ratio
  • G05B 13/02 - Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric
  • H02J 3/38 - Arrangements for parallelly feeding a single network by two or more generators, converters or transformers
  • H02J 13/00 - Circuit arrangements for providing remote indication of network conditions, e.g. an instantaneous record of the open or closed condition of each circuitbreaker in the network; Circuit arrangements for providing remote control of switching means in a power distribution network, e.g. switching in and out of current consumers by using a pulse code signal carried by the network
  • G06F 1/30 - Means for acting in the event of power-supply failure or interruption, e.g. power-supply fluctuations
  • G06Q 50/06 - Electricity, gas or water supply
  • H02J 3/06 - Controlling transfer of power between connected networks; Controlling sharing of load between connected networks
  • H02J 3/00 - Circuit arrangements for ac mains or ac distribution networks

48.

Intra-microgrid communication architecture

      
Application Number 15737914
Grant Number 10559977
Status In Force
Filing Date 2015-07-10
First Publication Date 2018-06-07
Grant Date 2020-02-11
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Kim, Moon C.
  • Wang, Kaiyu
  • Oggianu, Stella M.
  • Thornton, Robert K.
  • Lin, Yiqing

Abstract

A microgrid according to an exemplary aspect of the present disclosure includes, among other things, a plurality of intelligent electronic devices configured to communicate directly with one another in a first language. Each of the intelligent electronic devices includes a controller and a gateway. The gateway is configured to convert incoming messages from the first language to a second language native to the controller. The first language is different than the second language. A method is also disclosed.

IPC Classes  ?

  • H02J 13/00 - Circuit arrangements for providing remote indication of network conditions, e.g. an instantaneous record of the open or closed condition of each circuitbreaker in the network; Circuit arrangements for providing remote control of switching means in a power distribution network, e.g. switching in and out of current consumers by using a pulse code signal carried by the network

49.

Ion-exchange membrane with molecular barrier

      
Application Number 15568497
Grant Number 10596526
Status In Force
Filing Date 2015-04-24
First Publication Date 2018-05-31
Grant Date 2020-03-24
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Burlatsky, Sergei F.
  • Atrazhev, Vadim
  • Xie, Wei
  • Darling, Robert Mason
  • Perry, Michael L.

Abstract

Disclosed is an ion-exchange membrane that includes a molecular barrier for influencing permeation selectivity through the membrane. The membrane includes fluorinated carbon backbone chains and fluorinated side chains that extend off of the fluorinated carbon backbone chains. The fluorinated side chains include acid groups for ionic conductivity. The acid groups surround and define permeable domains that are free of the fluorinated carbon backbone chains. Molecular barriers are located in the permeable domains and influence permeability through the domains.

IPC Classes  ?

  • B01D 71/32 - Polyalkenyl halides containing fluorine atoms
  • B01D 67/00 - Processes specially adapted for manufacturing semi-permeable membranes for separation processes or apparatus
  • B01D 69/02 - Semi-permeable membranes for separation processes or apparatus characterised by their form, structure or properties; Manufacturing processes specially adapted therefor characterised by their properties
  • C08J 5/22 - Films, membranes or diaphragms
  • H01M 8/102 - Polymeric electrolyte materials characterised by the chemical structure of the main chain of the ion-conducting polymer
  • H01M 8/1039 - Polymeric electrolyte materials halogenated, e.g. sulfonated polyvinylidene fluorides
  • H01M 8/1044 - Mixtures of polymers, of which at least one is ionically conductive

50.

Redox-air indirect fuel cell

      
Application Number 15564261
Grant Number 10490871
Status In Force
Filing Date 2015-04-08
First Publication Date 2018-05-17
Grant Date 2019-11-26
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor Perry, Michael L.

Abstract

An electrochemical device includes first and second spaced-apart electrodes. The first electrode is configured for redox reactions with a liquid electrolyte solution and the second electrode is configured for redox reactions with each of a gaseous reductant and a gaseous oxidant. An electrolyte separator is arranged between the electrodes.

IPC Classes  ?

  • H01M 12/08 - Hybrid cells; Manufacture thereof composed of a half-cell of a fuel-cell type and a half-cell of the secondary-cell type
  • H01M 4/90 - Selection of catalytic material
  • H01M 4/92 - Metals of platinum group
  • H01M 8/04089 - Arrangements for control of reactant parameters, e.g. pressure or concentration of gaseous reactants
  • H01M 8/04082 - Arrangements for control of reactant parameters, e.g. pressure or concentration
  • H01M 8/18 - Regenerative fuel cells, e.g. redox flow batteries or secondary fuel cells
  • H01M 4/20 - Processes of manufacture of pasted electrodes

51.

Method of treating carbon electrode

      
Application Number 15564278
Grant Number 10505199
Status In Force
Filing Date 2015-04-09
First Publication Date 2018-05-17
Grant Date 2019-12-10
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor Darling, Robert Mason

Abstract

A method of treating a carbon electrode includes heat treating a carbon-based electrode in an environment that is above approximately 325° C. and that includes an oxidizing gas, and prior to use of the carbon-based electrode in an electro-chemical battery device, soaking the carbon-based electrode in an oxidizer solution.

IPC Classes  ?

  • H01M 4/88 - Processes of manufacture
  • H01M 8/18 - Regenerative fuel cells, e.g. redox flow batteries or secondary fuel cells
  • H01M 4/96 - Carbon-based electrodes
  • C25B 1/12 - Electrolytic production of inorganic compounds or non-metals of hydrogen or oxygen by electrolysis of water in pressure cells
  • C25B 11/12 - Electrodes based on carbon

52.

Control systems using deep reinforcement learning

      
Application Number 15797035
Grant Number 11062207
Status In Force
Filing Date 2017-10-30
First Publication Date 2018-05-10
Grant Date 2021-07-13
Owner RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Giering, Michael J.
  • Reddy, Kishore K.
  • Venugopalan, Vivek
  • Surana, Amit
  • Sarkar, Soumalya

Abstract

Data indicative of a plurality of observations of an environment are received at a control system. Machine learning using deep reinforcement learning is applied to determine an action based on the observations. The deep reinforcement learning applies a convolutional neural network or a deep auto encoder to the observations and applies a training set to locate one or more regions having a higher reward. The action is applied to the environment. A reward token indicative of alignment between the action and a desired result is received. A policy parameter of the control system is updated based on the reward token. The updated policy parameter is applied to determine a subsequent action responsive to a subsequent observation.

IPC Classes  ?

  • G06N 3/08 - Learning methods
  • G06N 20/00 - Machine learning
  • G05B 13/02 - Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric
  • G06N 3/04 - Architecture, e.g. interconnection topology
  • G06N 5/02 - Knowledge representation; Symbolic representation

53.

Method of treating liquid electrolyte solution

      
Application Number 15562013
Grant Number 10619257
Status In Force
Filing Date 2015-04-03
First Publication Date 2018-04-19
Grant Date 2020-04-14
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor Smeltz, Andrew

Abstract

A method for treating a liquid redox electrolyte solution for use in a flow battery includes feeding a liquid redox electrolyte solution into a first half-cell of an electrochemical cell and feeding a gaseous reductant into a second half-cell of the electrochemical cell, and electrochemically reducing at least a portion of the liquid redox electrolyte solution in the electrochemical cell using the gaseous reductant.

IPC Classes  ?

  • C25B 15/08 - Supplying or removing reactants or electrolytes; Regeneration of electrolytes
  • C25B 1/00 - Electrolytic production of inorganic compounds or non-metals
  • C01G 31/00 - Compounds of vanadium
  • C01G 31/02 - Oxides
  • H01M 8/18 - Regenerative fuel cells, e.g. redox flow batteries or secondary fuel cells

54.

Multi-modal sensor data fusion for perception systems

      
Application Number 15536713
Grant Number 11422546
Status In Force
Filing Date 2015-12-18
First Publication Date 2017-12-28
Grant Date 2022-08-23
Owner RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Giering, Michael J.
  • Reddy, Kishore K.
  • Venugopalan, Vivek
  • Sarkar, Soumik

Abstract

A method includes fusing multi-modal sensor data from a plurality of sensors having different modalities. At least one region of interest is detected in the multi-modal sensor data. One or more patches of interest are detected in the multi-modal sensor data based on detecting the at least one region of interest. A model that uses a deep convolutional neural network is applied to the one or more patches of interest. Post-processing of a result of applying the model is performed to produce a post-processing result for the one or more patches of interest. A perception indication of the post-processing result is output.

IPC Classes  ?

  • G05B 23/02 - Electric testing or monitoring
  • G06K 9/62 - Methods or arrangements for recognition using electronic means
  • G06V 10/44 - Local feature extraction by analysis of parts of the pattern, e.g. by detecting edges, contours, loops, corners, strokes or intersections; Connectivity analysis, e.g. of connected components
  • G06V 20/56 - Context or environment of the image exterior to a vehicle by using sensors mounted on the vehicle
  • G06T 7/246 - Analysis of motion using feature-based methods, e.g. the tracking of corners or segments
  • G06N 3/04 - Architecture, e.g. interconnection topology
  • G06N 3/08 - Learning methods

55.

Pressure vessel assembly and method of forming

      
Application Number 15517010
Grant Number 10648616
Status In Force
Filing Date 2014-10-07
First Publication Date 2017-11-30
Grant Date 2020-05-12
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Garosshen, Thomas J.
  • Sun, Ellen Y.
  • Croteau, Paul F.
  • Kuczek, Andrzej Ernest
  • El-Wardany, Tahany Ibrahim
  • Zhao, Wenping
  • Hawkes, Justin R.
  • Sharon, John A.
  • Wesson, John P.
  • Viens, Daniel V.

Abstract

A pressure vessel assembly includes a plurality of lobes, each lobe having at least one vertically arranged interior wall, the lobes positioned in a side by side arrangement such that a first interior wall of a first lobe is positioned adjacent a second interior wall of a second lobe, the first interior wall having a first wall top and bottom side, the second interior wall having a second wall top and bottom side, the first wall top side joined to the second wall top side and the first wall bottom side joined to the second wall bottom side. Also included are first and second end wall surfaces of each of the plurality of lobes. Further included is a plurality of end caps, each of the end caps joined to the end wall surfaces of the lobes, each of the end caps joined to at least one adjacent end cap.

IPC Classes  ?

  • F17C 1/16 - Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge constructed of plastics materials
  • F17C 1/14 - Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge constructed of non-magnetic steel
  • B23K 15/00 - Electron-beam welding or cutting

56.

Coherent acoustic wave generation

      
Application Number 14614555
Grant Number 09812117
Status In Force
Filing Date 2015-02-05
First Publication Date 2017-11-07
Grant Date 2017-11-07
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Mantese, Joseph V.
  • Blanc, Arthur
  • Vincitore, Antonio M.

Abstract

An acoustic wave generator including a stack having a plurality of first layers configured to receive electrical and/or magnetic energy and a plurality of second layers configured in contact with the plurality of first layers, the plurality of second layers comprising one or more materials configured to change mechanical properties when electrical and/or magnetic energy is applied thereto. The generator further having at least one source configured in operational communication with the plurality of first layers and configured to supply at least one of phased electrical and/or magnetic energy to the plurality of first layers, wherein the stack is configured to (i) generate phased acoustic energy and (ii) at least one of amplify and store the generated phased acoustic energy in a first state and release said generator acoustic energy in a second state.

IPC Classes  ?

  • G10K 11/00 - Methods or devices for transmitting, conducting or directing sound in general; Methods or devices for protecting against, or for damping, noise or other acoustic waves in general
  • G10K 11/26 - Sound-focusing or directing, e.g. scanning

57.

Pressure vessel fluid manifold assembly

      
Application Number 15517017
Grant Number 10221999
Status In Force
Filing Date 2014-10-07
First Publication Date 2017-10-19
Grant Date 2019-03-05
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Croteau, Paul F.
  • Kuczek, Andrzej Ernest
  • Viens, Daniel V.
  • Hawkes, Justin R.
  • Zhao, Wenping
  • Garosshen, Thomas J.

Abstract

A pressure vessel fluid manifold assembly includes a pressure vessel having a plurality of lobes joined to each other, each of the plurality of lobes having a wall disposed in contact with an adjacent wall of an adjacent lobe, and wherein the manifold can be external or internal to the lobes.

IPC Classes  ?

  • F17C 13/00 - VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES - Details of vessels or of the filling or discharging of vessels
  • F17C 1/14 - Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge constructed of non-magnetic steel
  • F17C 1/16 - Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge constructed of plastics materials
  • F17C 1/00 - Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge

58.

Composite pressure vessel assembly and method of manufacturing

      
Application Number 15517025
Grant Number 11525545
Status In Force
Filing Date 2014-10-07
First Publication Date 2017-10-19
Grant Date 2022-12-13
Owner RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Zhao, Wenping
  • Sun, Ellen Y.
  • Wesson, John P.
  • Croteau, Paul F.
  • Kuczek, Andrzej Ernest

Abstract

A composite pressure vessel assembly includes a plurality of lobes, each of the lobes having at least one interior wall and at least one curved wall, the plurality of lobes being positioned in a side by side arrangement and extending in a longitudinal direction from a first end to a second end. Also included is a plurality of end caps disposed at the ends of the lobes, wherein the plurality of lobes and end caps are formed of at least one fiber-reinforced polymer. A method of manufacturing a composite pressure vessel assembly is provided. The method includes forming a plurality of lobes consisting of at least one fiber-reinforced polymer. The method also includes forming a main body with the plurality of lobes, the lobes disposed in a side by side arrangement.

IPC Classes  ?

  • F17C 1/16 - Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge constructed of plastics materials
  • B29C 63/04 - Lining or sheathing, i.e. applying preformed layers or sheathings of plastics; Apparatus therefor using sheet or web-like material by folding, winding, bending or the like
  • B29C 70/30 - Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
  • B29L 31/00 - Other particular articles

59.

Regeneration of flow battery electrode

      
Application Number 15511030
Grant Number 10680259
Status In Force
Filing Date 2014-09-15
First Publication Date 2017-08-31
Grant Date 2020-06-09
Owner RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Smeltz, Andrew
  • Perry, Michael L.
  • Darling, Robert Mason

Abstract

A method is disclosed for regenerating an electrode of a flow battery. The method can be executed during shutdown of the flow battery from an active charge/discharge mode to an inactive, shut-down mode in which neither a negative electrolyte nor a positive electrolyte are circulated through at least one cell of the flow battery. The method includes driving voltage of the least one cell of the flow battery toward zero by converting, in-situ, the negative electrolyte in the at least one cell to a higher oxidation state. The negative electrolyte is in contact with an electrode of the at least one cell. The higher oxidation state negative electrolyte is used to regenerate, in-situ, catalytically active surfaces of the electrode of the at least one cell.

IPC Classes  ?

  • H01M 8/04228 - Auxiliary arrangements, e.g. for control of pressure or for circulation of fluids during start-up or shut-down; Depolarisation or activation, e.g. purging; Means for short-circuiting defective fuel cells during shut-down
  • H01M 8/04223 - Auxiliary arrangements, e.g. for control of pressure or for circulation of fluids during start-up or shut-down; Depolarisation or activation, e.g. purging; Means for short-circuiting defective fuel cells
  • H01M 8/18 - Regenerative fuel cells, e.g. redox flow batteries or secondary fuel cells
  • H01M 8/20 - Indirect fuel cells, e.g. fuel cells with redox couple being irreversible
  • H01M 4/90 - Selection of catalytic material

60.

System and methods for removing core elements of cast components

      
Application Number 15590132
Grant Number 09808862
Status In Force
Filing Date 2017-05-09
First Publication Date 2017-08-24
Grant Date 2017-11-07
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Verner, Carl R.
  • Marcin, John Joseph

Abstract

A system and methods are provided for removing core elements of cast components. In one embodiment, a method includes controlling a first high temperature autoclave cycle for a cast component in a vessel with a first solution concentration to remove at least a first portion of core elements, wherein the first solution concentration, temperature and pressure in the vessel are controlled to expose one or more casting pins in the cast component. The method may also include controlling a second high temperature autoclave cycle for the cast component in the vessel with second solution concentration, wherein the second solution concentration, temperature and pressure in the vessel during the second high temperature autoclave cycle are controlled to loosen one or more of the casting pins from the cast component, and controlling one or more low temperature autoclave cycles to remove core and casting pins from the cast component.

IPC Classes  ?

  • B22D 29/00 - Removing castings from moulds, not restricted to casting processes covered by a single main group; Removing cores; Handling ingots
  • B22D 30/00 - Cooling castings, not restricted to casting processes covered by a single main group

61.

Container having an internal structure with minimum surfaces

      
Application Number 15302532
Grant Number 10302252
Status In Force
Filing Date 2014-04-14
First Publication Date 2017-02-02
Grant Date 2019-05-28
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Kuczek, Andrzej Ernest
  • Lynch, Matthew E.
  • Croteau, Paul F.
  • El-Wardany, Tahany Ibrahim
  • Sun, Ellen Y.
  • Zhao, Wenping
  • Viens, Daniel V.

Abstract

An illustrative example container includes a plurality of internal support members having a surface contour that at least approximates a minimum surface. The plurality of internal support members collectively provide structural support for carrying loads on the container. The plurality of internal support members collectively establish a plurality of cavities for at least temporarily containing fluid. An outer shell is connected with at least some of the internal support members. The outer shell includes a plurality of curved surfaces. The outer shell encloses the cavities.

IPC Classes  ?

  • F17C 1/08 - Integral reinforcements, e.g. ribs
  • F17C 1/14 - Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge constructed of non-magnetic steel
  • F28F 3/08 - Elements constructed for building-up into stacks, e.g. capable of being taken apart for cleaning
  • F28F 3/12 - Elements constructed in the shape of a hollow panel, e.g. with channels

62.

Engine speed optimization as a method to reduce APU fuel consumption

      
Application Number 14731047
Grant Number 09845806
Status In Force
Filing Date 2015-06-04
First Publication Date 2016-12-08
Grant Date 2017-12-19
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Pascu, Victor
  • Jones, Anthony C.

Abstract

Systems and methods for controlling an auxiliary power unit (APU) are provided. The systems and methods may comprise detecting an operating condition of the APU, determining an optimal APU frequency in response to the operating condition, and setting an angular velocity of the APU to the optimal APU frequency.

IPC Classes  ?

  • F04D 27/00 - Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
  • F04D 17/10 - Centrifugal pumps for compressing or evacuating
  • F02C 9/16 - Control of working fluid flow
  • F02C 9/28 - Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed

63.

Dynamically updated predictive modeling to predict operational outcomes of interest

      
Application Number 15134048
Grant Number 10984338
Status In Force
Filing Date 2016-04-20
First Publication Date 2016-12-01
Grant Date 2021-04-20
Owner RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Morris, Ii, Robert G.
  • Mcginnis, William

Abstract

Various examples are provided for dynamically updating or adapting predictive modeling for prediction of outcomes of interest for operating systems and processes. Embodiments of the disclosure may provide systems, apparatus, processes, and methods for generating and deploying dynamically updated predictive models. In some embodiments, the predictive model may be deployed for the purpose of predicting operational outcomes of interests in operating systems, hardware devices, machines and/or processes associated therewith prior to the operational outcomes of interest occurring. The predictions can, for example, provide sufficient time for maintenance or repairs to be scheduled and carried out to avoid the predicted operational outcome. Autonomous evaluation of features allows the predictive models to be dynamically updated in response to changes in the environment or monitored data.

IPC Classes  ?

64.

Flow battery with rotationally symmetric manifold plates

      
Application Number 15109670
Grant Number 10164283
Status In Force
Filing Date 2014-01-07
First Publication Date 2016-11-10
Grant Date 2018-12-25
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor Darling, Robert Mason

Abstract

A flow battery includes a stack of manifold plates that define first and second exclusive flow circuits through the stack between first and second stack inlets and first and second stack outlets. The manifold plates each include a frame that extends around a flow field of an electrochemically active area, with a plurality of port through-holes in the frame. The through-holes are arranged in a rotationally symmetric pattern about a center of the respective manifold plate.

IPC Classes  ?

  • H01M 8/18 - Regenerative fuel cells, e.g. redox flow batteries or secondary fuel cells
  • H01M 8/20 - Indirect fuel cells, e.g. fuel cells with redox couple being irreversible
  • H01M 8/0247 - Collectors; Separators, e.g. bipolar separators; Interconnectors characterised by the form

65.

Rebalancing electrolyte concentration in flow battery using pressure differential

      
Application Number 15107517
Grant Number 10050290
Status In Force
Filing Date 2013-12-26
First Publication Date 2016-10-27
Grant Date 2018-08-14
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Perry, Michael L.
  • Smeltz, Andrew
  • Xie, Wei

Abstract

A flow battery that includes an electrochemical cell having first and second half-cells and an ion-selective separator there between wherein a fluid pressure differential across the ion-selective separator for a controlled amount of time is selectively utilized to urge a concentration imbalance of the electrochemically active species between the first and second electrolytes toward a concentration balance.

IPC Classes  ?

  • H01M 8/20 - Indirect fuel cells, e.g. fuel cells with redox couple being irreversible
  • H01M 8/04276 - Arrangements for managing the electrolyte stream, e.g. heat exchange
  • H01M 8/04186 - Arrangements for control of reactant parameters, e.g. pressure or concentration of liquid-charged or electrolyte-charged reactants
  • H01M 8/0444 - Concentration; Density
  • H01M 8/04746 - Pressure; Flow
  • H01M 8/18 - Regenerative fuel cells, e.g. redox flow batteries or secondary fuel cells

66.

Distribution of electrolytes in a flow battery

      
Application Number 15107499
Grant Number 09853310
Status In Force
Filing Date 2013-12-23
First Publication Date 2016-10-27
Grant Date 2017-12-26
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Darling, Robert Mason
  • Smeltz, Andrew
  • Junker, Sven Tobias
  • Perry, Michael L.

Abstract

A method of determining a distribution of electrolytes in a flow battery includes providing a flow battery with a fixed amount of fluid electrolyte having a common electrochemically active specie, a portion of the fluid electrolyte serving as an anolyte and a remainder of the fluid electrolyte serving as a catholyte. An average oxidation state of the common electrochemically active specie is determined in the anolyte and the catholyte and, responsive to the determined average oxidation state, a molar ratio of the common electrochemically active specie between the anolyte and the catholyte is adjusted to increase an energy discharge capacity of the flow battery for the determined average oxidation state.

IPC Classes  ?

  • H01M 8/04791 - Concentration; Density
  • H01M 8/0432 - Temperature; Ambient temperature
  • H01M 8/0444 - Concentration; Density
  • H01M 8/18 - Regenerative fuel cells, e.g. redox flow batteries or secondary fuel cells
  • H01M 8/04186 - Arrangements for control of reactant parameters, e.g. pressure or concentration of liquid-charged or electrolyte-charged reactants
  • H01M 8/04276 - Arrangements for managing the electrolyte stream, e.g. heat exchange
  • H01M 8/20 - Indirect fuel cells, e.g. fuel cells with redox couple being irreversible

67.

High conformal pressure vessel

      
Application Number 15035060
Grant Number 10222001
Status In Force
Filing Date 2014-09-08
First Publication Date 2016-10-06
Grant Date 2019-03-05
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Croteau, Paul F.
  • Wesson, John P.
  • Kuczek, Andrzej Ernest
  • Lynch, Matthew E.
  • El-Wardany, Tahany Ibrahim
  • Sun, Ellen Y.
  • Zhao, Wenping
  • Viens, Daniel V.

Abstract

A pressure vessel configured to store a pressurized fluid is provided including a plurality of lobes. Each lobe includes at least one vertically arranged interior wall. The plurality of lobes are positioned in a side by side configuration such that a first interior wall of a first lobe is positioned adjacent a second interior wall of a second adjacent lobe. The first interior wall and the second interior wall are configured to contact one another at a first point of tangency. A first tangent intersects the first lobe at the first point of tangency and a second tangent intersects the second lobe at the first point of tangency. The first tangent and the second tangent are separated by about 120 degrees.

IPC Classes  ?

  • F17C 13/06 - Closures, e.g. cap, breakable member
  • F17C 1/14 - Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge constructed of non-magnetic steel
  • F17C 1/16 - Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge constructed of plastics materials
  • F17C 1/00 - Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge

68.

Acoustic metamaterial gate

      
Application Number 14614557
Grant Number 09779713
Status In Force
Filing Date 2015-02-05
First Publication Date 2016-06-30
Grant Date 2017-10-03
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Blanc, Arthur
  • Mantese, Joseph V.

Abstract

An acoustic wave gate is provided. The gate includes one or more layers of metamaterial configured to be in a first state and a second state and configured to change from the first state to the second state when electrical and/or magnetic energy is applied thereto. The gate also includes at least one source configured in operational communication with the one or more layers and configured to supply at least one of electrical and magnetic energy to the one or more layers. The one or more layers are configured to (i) prevent the passage of acoustic energy through the one or more layers when in the first state and (ii) permit the passage of acoustic energy through the one or more layers when in the second state, wherein the one or more layers are configured to be stimulated in phase with the acoustic energy.

IPC Classes  ?

  • G10K 11/00 - Methods or devices for transmitting, conducting or directing sound in general; Methods or devices for protecting against, or for damping, noise or other acoustic waves in general
  • G10K 11/04 - Acoustic filters

69.

Flow battery with manifold passage that varies in cross-section

      
Application Number 14897339
Grant Number 10115983
Status In Force
Filing Date 2013-06-13
First Publication Date 2016-05-12
Grant Date 2018-10-30
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Darling, Robert Mason
  • Perry, Michael L.
  • Ding, Jinlei
  • Walker, Craig R.

Abstract

A flow battery includes a cell stack that has electrochemically active cells and manifolds that define common manifold passages in fluid communication with the electrochemically active cells. A supply/storage system is external of the cell stack and includes at least one vessel fluidly connected with respective ones of the common manifold passages. Fluid electrolytes are in the supply/storage system. At least one of the fluid electrolytes is an ionic-conductive fluid. The manifolds extend in a length direction through the cell stack. The common manifold passages include a common manifold passage P that varies in cross-section along the length direction.

IPC Classes  ?

  • H01M 8/04 - Auxiliary arrangements, e.g. for control of pressure or for circulation of fluids
  • H01M 8/20 - Indirect fuel cells, e.g. fuel cells with redox couple being irreversible
  • H01M 8/18 - Regenerative fuel cells, e.g. redox flow batteries or secondary fuel cells
  • H01M 8/04186 - Arrangements for control of reactant parameters, e.g. pressure or concentration of liquid-charged or electrolyte-charged reactants
  • H01M 8/04082 - Arrangements for control of reactant parameters, e.g. pressure or concentration

70.

Flow battery with hydrated ion-exchange membrane having maximum water domain cluster sizes

      
Application Number 14891013
Grant Number 10135085
Status In Force
Filing Date 2013-05-16
First Publication Date 2016-05-05
Grant Date 2018-11-20
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Darling, Robert Mason
  • Perry, Michael L.
  • Xie, Wei

Abstract

A flow battery includes a cell that has a first electrode, a second electrode spaced apart from the first electrode and an electrolyte separator layer arranged between the first electrode and the second electrode. A supply/storage system is external of the at least one cell and includes first and second vessels that are fluidly connected with the at least one cell. First and second fluid electrolytes are located in the supply/storage system. The electrolyte separator layer includes a hydrated ion-exchange membrane of a polymer that has a carbon backbone chain and side chains extending from the carbon backbone chain. The side chains include hydrophilic chemical groups with water molecules attached by secondary bonding to form clusters of water domains. The clusters have an average maximum cluster size no greater than 4 nanometers, with an average number of water molecules per hydrophilic chemical group, λ (lambda), being greater than zero.

IPC Classes  ?

  • H01M 4/36 - Selection of substances as active materials, active masses, active liquids
  • H01M 8/1067 - Polymeric electrolyte materials characterised by their physical properties, e.g. porosity, ionic conductivity or thickness
  • H01M 8/1023 - Polymeric electrolyte materials characterised by the chemical structure of the main chain of the ion-conducting polymer having only carbon, e.g. polyarylenes, polystyrenes or polybutadiene-styrenes
  • H01M 8/1039 - Polymeric electrolyte materials halogenated, e.g. sulfonated polyvinylidene fluorides
  • H01M 8/20 - Indirect fuel cells, e.g. fuel cells with redox couple being irreversible
  • H01M 8/18 - Regenerative fuel cells, e.g. redox flow batteries or secondary fuel cells
  • H01M 8/1018 - Polymeric electrolyte materials

71.

Flow battery flow field having volume that is function of power parameter, time parameter and concentration parameter

      
Application Number 14768622
Grant Number 10892499
Status In Force
Filing Date 2013-03-15
First Publication Date 2016-01-21
Grant Date 2021-01-12
Owner Raytheon Technologies Corporation (USA)
Inventor
  • Smeltz, Andrew
  • Darling, Robert Mason
  • Perry, Michael L.
  • Ding, Zhongfen

Abstract

A flow battery includes a cell that has first and second flow fields spaced apart from each other and an electrolyte separator layer. A supply/storage system is external of the cell and includes first and second vessels fluidly connected with the first and second flow fields, and first and second pumps configured to selectively move first and second fluid electrolytes between the vessels and the first and second flow fields. The flow fields each have an electrochemically active zone that is configured to receive flow of the fluid electrolytes. The electrochemically active zone has a total open volume that is a function of at least one of a power parameter of the flow battery, a time parameter of the pumps and a concentration parameter of the fluid electrolytes.

IPC Classes  ?

  • H01M 8/04276 - Arrangements for managing the electrolyte stream, e.g. heat exchange
  • H01M 8/18 - Regenerative fuel cells, e.g. redox flow batteries or secondary fuel cells
  • H01M 8/20 - Indirect fuel cells, e.g. fuel cells with redox couple being irreversible
  • H01M 8/04186 - Arrangements for control of reactant parameters, e.g. pressure or concentration of liquid-charged or electrolyte-charged reactants
  • H01M 8/04992 - Processes for controlling fuel cells or fuel cell systems characterised by the implementation of mathematical or computational algorithms, e.g. feedback control loops, fuzzy logic, neural networks or artificial intelligence

72.

Reactivation of flow battery electrode by exposure to oxidizing solution

      
Application Number 14770969
Grant Number 10044058
Status In Force
Filing Date 2013-03-15
First Publication Date 2016-01-14
Grant Date 2018-08-07
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Darling, Robert Mason
  • Zaffou, Rachid
  • Perry, Michael L.
  • Walker, Craig R.

Abstract

A flow battery includes at least a cell that has a first electrode, a second electrode and an electrolyte separator layer arranged between the electrodes. A supply/storage system is external of the cell and includes a first vessel fluidly connected in a first loop with the first electrode and a second vessel fluidly connected in a second loop with the second electrode. The first loop and the second loop are isolated from each other. The supply/storage system is configured to fluidly connect the first loop and the second loop to move a second liquid electrolyte from the second vessel into a first liquid electrolyte in the first vessel responsive to a half-cell potential at the first electrode being less than a defined threshold half-cell potential.

IPC Classes  ?

  • H01M 8/18 - Regenerative fuel cells, e.g. redox flow batteries or secondary fuel cells
  • H01M 8/20 - Indirect fuel cells, e.g. fuel cells with redox couple being irreversible

73.

Removing non-homogeneous ice from a fuel system

      
Application Number 14768988
Grant Number 11105267
Status In Force
Filing Date 2014-02-21
First Publication Date 2016-01-07
Grant Date 2021-08-31
Owner RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor Hagshenas, Behzad

Abstract

The presently disclosed embodiments utilize an ice separator vessel to trap ice particles in a non-homogeneous ice/fuel mixture flowing in a fuel system. A source of heat, such as heated fuel provided to the ice separator vessel, is used to melt at least a portion of the ice particles so that they do not enter the fuel system downstream of the ice separator vessel.

IPC Classes  ?

  • F02C 7/224 - Heating fuel before feeding to the burner
  • F02C 7/236 - Fuel delivery systems comprising two or more pumps
  • B01D 21/00 - Separation of suspended solid particles from liquids by sedimentation
  • B01D 21/26 - Separation of sediment aided by centrifugal force
  • B04B 15/02 - Other accessories for centrifuges for cooling, heating, or heat insulating

74.

Cowl with pressure driven latch

      
Application Number 14764375
Grant Number 09376215
Status In Force
Filing Date 2013-01-29
First Publication Date 2015-12-24
Grant Date 2016-06-28
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor Forcier, Matthew J.

Abstract

A gas turbine engine includes an engine core, a core cowl extending circumferentially around the engine core, and a pressure actuated latch assembly. The core cowl includes a first cowl section on a first side of the engine core and a second cowl section on a second side of the engine core. The pressure actuated latch assembly connects the first cowl section to a support structure and is actuatable between an unlatched position when pressure within the core cowl is relatively low and a latched position when pressure within the core cowl is relatively high.

IPC Classes  ?

  • B64D 29/06 - Attaching of nacelles, fairings, or cowlings
  • B64D 29/00 - Power-plant nacelles, fairings, or cowlings
  • B64C 7/02 - Nacelles
  • F02C 7/20 - Mounting or supporting of plant; Accommodating heat expansion or creep

75.

Graphite-containing electrode and method related thereto

      
Application Number 14652131
Grant Number 10944108
Status In Force
Filing Date 2012-12-23
First Publication Date 2015-11-26
Grant Date 2021-03-09
Owner Raytheon Technologies Corporation (USA)
Inventor Darling, Robert Mason

Abstract

A graphite-containing electrode includes a porous body that has a plurality of first graphite-containing elements and a plurality of second graphite-containing elements intermingled with the first graphite-containing elements. The first graphite-containing elements have a first degree of graphitization and the second graphite-containing elements have a second, different degree of graphitization.

IPC Classes  ?

  • H01M 4/96 - Carbon-based electrodes
  • H01M 8/20 - Indirect fuel cells, e.g. fuel cells with redox couple being irreversible
  • H01M 4/86 - Inert electrodes with catalytic activity, e.g. for fuel cells
  • H01M 8/18 - Regenerative fuel cells, e.g. redox flow batteries or secondary fuel cells
  • H01M 4/583 - Carbonaceous material, e.g. graphite-intercalation compounds or CFx
  • H01M 4/88 - Processes of manufacture

76.

Flow battery having electrodes with a plurality of different pore sizes and or different layers

      
Application Number 14807590
Grant Number 09647273
Status In Force
Filing Date 2015-07-23
First Publication Date 2015-11-19
Grant Date 2017-05-09
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Zaffou, Rachid
  • Perry, Michael L.
  • Pandy, Arun
  • Burlatsky, Sergei F.
  • Atrazhev, Vadim

Abstract

A flow battery includes an electrode operable to be wet by a solution having a reversible redox couple reactant. In one embodiment, the electrode can have plurality of micro and macro pores, wherein the macro pores have a size at least one order of magnitude greater than a size of the micro pores. In another embodiment, the electrode includes a plurality of layers, wherein one of the plurality of layers has a plurality of macro pores, and wherein another one of the plurality of layers has a plurality of micro pores. In another embodiment, the electrode has a thickness less than approximately 2 mm. In still another embodiment, the electrode has a porous carbon layer, wherein the layer is formed of a plurality of particles bound together.

IPC Classes  ?

  • H01M 4/86 - Inert electrodes with catalytic activity, e.g. for fuel cells
  • H01M 8/20 - Indirect fuel cells, e.g. fuel cells with redox couple being irreversible
  • H01M 8/0234 - Carbonaceous material
  • H01M 8/18 - Regenerative fuel cells, e.g. redox flow batteries or secondary fuel cells

77.

Flow battery with voltage-limiting device

      
Application Number 14650126
Grant Number 09966618
Status In Force
Filing Date 2012-12-09
First Publication Date 2015-11-05
Grant Date 2018-05-08
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Darling, Robert Mason
  • Perry, Michael L.

Abstract

A flow battery includes at least one cell that has a first electrode, a second electrode spaced apart from the first electrode and an electrolyte separator layer that is arranged between the first electrode and the second electrode. A storage portion is fluidly connected with the at least one cell. At least one liquid electrolyte includes an electrochemically active specie and is selectively deliverable to the at least one cell. An electric circuit is coupled with the first electrode and the second electrode. The circuit includes a voltage-limiting device that is configured to limit a voltage potential across the first electrode and the second electrode in response to a transition of the at least one cell from an inactive, shut-down mode with respect to an active, charge/discharge mode.

IPC Classes  ?

  • H01M 8/04 - Auxiliary arrangements, e.g. for control of pressure or for circulation of fluids
  • H01M 8/04858 - Electric variables
  • H01M 8/18 - Regenerative fuel cells, e.g. redox flow batteries or secondary fuel cells
  • H01M 8/04223 - Auxiliary arrangements, e.g. for control of pressure or for circulation of fluids during start-up or shut-down; Depolarisation or activation, e.g. purging; Means for short-circuiting defective fuel cells
  • H01M 8/043 - Processes for controlling fuel cells or fuel cell systems applied during specific periods
  • H01M 8/20 - Indirect fuel cells, e.g. fuel cells with redox couple being irreversible
  • H01M 8/04746 - Pressure; Flow

78.

Electrochemical device and method for controlling corrosion

      
Application Number 14439679
Grant Number 10177389
Status In Force
Filing Date 2012-11-09
First Publication Date 2015-10-08
Grant Date 2019-01-08
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Darling, Robert Mason
  • Perry, Michael L.

Abstract

An electrochemical device includes a plurality of electrode assemblies that define a plurality of electrochemically active areas. A non-electrically-conductive manifold includes a common manifold passage and a plurality of branch passages that extend, respectively, between the electrochemically active areas and the common manifold passage. Each of the branch passages includes a first region and a second region that differ in surface area.

IPC Classes  ?

  • H01M 4/86 - Inert electrodes with catalytic activity, e.g. for fuel cells
  • H01M 8/04 - Auxiliary arrangements, e.g. for control of pressure or for circulation of fluids
  • H01M 8/24 - Grouping of fuel cells, e.g. stacking of fuel cells
  • H01M 8/04082 - Arrangements for control of reactant parameters, e.g. pressure or concentration
  • H01M 8/0273 - Sealing or supporting means around electrodes, matrices or membranes with sealing or supporting means in the form of a frame
  • H01M 8/2485 - Arrangements for sealing external manifolds; Arrangements for mounting external manifolds around a stack
  • H01M 8/18 - Regenerative fuel cells, e.g. redox flow batteries or secondary fuel cells
  • H01M 8/0258 - Collectors; Separators, e.g. bipolar separators; Interconnectors characterised by the configuration of channels, e.g. by the flow field of the reactant or coolant
  • H01M 8/2483 - Grouping of fuel cells, e.g. stacking of fuel cells - Details of groupings of fuel cells characterised by internal manifolds

79.

Pitch diameter shank bolt with shear sleeve

      
Application Number 14731584
Grant Number 09926965
Status In Force
Filing Date 2015-06-05
First Publication Date 2015-09-24
Grant Date 2018-03-27
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor Hyatt, Thomas B.

Abstract

A fastener includes a fastening portion including a head, a threaded portion having a first diameter, and a shank having a second diameter that is less than the first diameter. The shank is located between the head and the threaded portion. A sleeve surrounds the shank. The sleeve and the shank are uncoupled.

IPC Classes  ?

  • F16B 43/00 - Washers or equivalent devices; Other devices for supporting bolt-heads or nuts
  • F16B 5/02 - Joining sheets or plates to one another or to strips or bars parallel to them by means of fastening members using screw-thread
  • F16B 19/02 - Bolts or sleeves for positioning of machine parts, e.g. notched taper pins, fitting pins, sleeves, eccentric positioning rings
  • F16B 35/04 - Screw-bolts; Stay bolts; Screw-threaded studs; Screws; Set screws with specially-shaped head or shaft in order to fix the bolt on or in an object
  • F01D 25/24 - Casings; Casing parts, e.g. diaphragms, casing fastenings

80.

Die casting system and cell

      
Application Number 14536950
Grant Number 09289823
Status In Force
Filing Date 2014-11-10
First Publication Date 2015-03-05
Grant Date 2016-03-22
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Bochiechio, Mario P.
  • Marcin, John Joseph
  • Verner, Carl R.
  • Blondin, John F.
  • Bartholomew, Mark F.
  • Ristau, Raymond P.
  • Chittenden, Kevin W.
  • Tamiso, Gary M.
  • Renaud, Robert C.
  • Kraemer, Dennis M.
  • Lebrun, Robert E.
  • Zamjohn, Paul R.
  • Roohr, Charles A.
  • Kozaczuk, Kerry
  • Garrison, Roy A.
  • Bullied, Steven J.

Abstract

A method of manufacturing a component in a die casting cell that includes a die casting system according to an exemplary aspect of the present disclosure includes, among other things, isolating a first chamber from a second chamber of the die casting system, melting a charge of material in the first chamber, sealing the second chamber relative to the first chamber, and simultaneously injecting the charge of material within the second chamber to cast the component and melting a second charge of material within the first chamber.

IPC Classes  ?

  • B22D 17/02 - Hot chamber machines, i.e. with heated press chamber in which metal is melted
  • B22D 17/14 - Machines with evacuated die cavity
  • B22D 17/28 - Melting pots
  • B22D 17/30 - Accessories for supplying molten metal, e.g. in rations
  • B22D 17/20 - Pressure die casting or injection die casting, i.e. casting in which the metal is forced into a mould under high pressure - Details
  • B22D 17/22 - Dies; Die plates; Die supports; Cooling equipment for dies; Accessories for loosening and ejecting castings from dies
  • B22D 25/02 - Special casting characterised by the nature of the product of works of art
  • B22D 29/00 - Removing castings from moulds, not restricted to casting processes covered by a single main group; Removing cores; Handling ingots
  • B22D 31/00 - Cutting-off surplus material after casting, e.g. gates

81.

System and method for high temperature die casting tooling

      
Application Number 14518694
Grant Number 09452470
Status In Force
Filing Date 2014-10-20
First Publication Date 2015-02-05
Grant Date 2016-09-27
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Castle, Lea Kennard
  • Bochiechio, Mario P.

Abstract

A die casting and a method for die casting a metal having a melting temperature of at least 1500° F. (815° C.) are disclosed. A molten volume of metal is injected to a casting die which includes a main cavity corresponding to an as-cast structure, a first reservoir, and a first runner arrangement. The first runner arrangement is configured to fluidly communicate molten metal between the first reservoir and the main cavity. After the injecting step, the casting die is sealed. The injected molten volume of metal is equiaxially solidified generally from a first portion of the main cavity distal to the first reservoir toward a second portion of the main cavity proximal to the first reservoir. During the equiaxial solidifying step, the main cavity is backfilled with at least a portion of the injected molten volume via the first runner arrangement.

IPC Classes  ?

  • B22D 17/14 - Machines with evacuated die cavity
  • B22D 17/20 - Pressure die casting or injection die casting, i.e. casting in which the metal is forced into a mould under high pressure - Details
  • B22D 17/22 - Dies; Die plates; Die supports; Cooling equipment for dies; Accessories for loosening and ejecting castings from dies
  • B22D 30/00 - Cooling castings, not restricted to casting processes covered by a single main group
  • B22D 17/02 - Hot chamber machines, i.e. with heated press chamber in which metal is melted
  • B22D 21/00 - Casting non-ferrous metals or metallic compounds so far as their metallurgical properties are of importance for the casting procedure; Selection of compositions therefor
  • B22D 21/02 - Casting exceedingly oxidisable non-ferrous metals, e.g. in inert atmosphere
  • B22C 9/06 - Permanent moulds for shaped castings
  • B22C 9/08 - Features with respect to supply of molten metal, e.g. ingates, circular gates, skim gates
  • C22C 19/03 - Alloys based on nickel or cobalt based on nickel

82.

Method and system for operating a flow battery system based on energy costs

      
Application Number 14509685
Grant Number 10050297
Status In Force
Filing Date 2014-10-08
First Publication Date 2015-01-22
Grant Date 2018-08-14
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Pandy, Arun
  • Perry, Michael L.

Abstract

A method and system for storing and/or discharging electrical energy that has a cost, which method includes steps of: (a) providing a flow battery system comprising at least one flow battery cell and a controller; (b) operating the flow battery cell at a power density having a first value; and (c) changing the power density at which the flow battery cell is operated from the first value to a second value as a function of the cost of the electrical energy, wherein the power density is changed using the controller, and wherein the second value is different than the first value.

IPC Classes  ?

  • H01M 8/18 - Regenerative fuel cells, e.g. redox flow batteries or secondary fuel cells
  • H01M 8/20 - Indirect fuel cells, e.g. fuel cells with redox couple being irreversible
  • H02J 3/32 - Arrangements for balancing the load in a network by storage of energy using batteries with converting means
  • H01M 8/04858 - Electric variables
  • H01M 8/04992 - Processes for controlling fuel cells or fuel cell systems characterised by the implementation of mathematical or computational algorithms, e.g. feedback control loops, fuzzy logic, neural networks or artificial intelligence
  • H01M 10/48 - Accumulators combined with arrangements for measuring, testing or indicating the condition of cells, e.g. the level or density of the electrolyte
  • H01M 10/44 - Methods for charging or discharging

83.

Inlet duct screen assembly

      
Application Number 14446407
Grant Number 09340295
Status In Force
Filing Date 2014-07-30
First Publication Date 2014-11-13
Grant Date 2016-05-17
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Dede, Brian C.
  • Vitale, Jack V.
  • Stenberg, Jeffrey V.

Abstract

An example inlet duct screen assembly includes a grid portion including a plurality of apertures and a frame portion circumscribing the grid portion. The grid portion and the frame portion are formed from a single sheet of material.

IPC Classes  ?

  • B64D 33/02 - Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
  • B01D 39/10 - Filter screens essentially made of metal
  • B64D 41/00 - Power installations for auxiliary purposes
  • B26F 3/00 - Severing by means other than cutting; Apparatus therefor

84.

Flow battery with enhanced durability

      
Application Number 14364717
Grant Number 10158140
Status In Force
Filing Date 2011-12-20
First Publication Date 2014-10-23
Grant Date 2018-12-18
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Zaffou, Rachid
  • Perry, Michael L.

Abstract

A flow battery includes at least one electrochemical cell that has a first electrode, a second electrode spaced apart from the first electrode and a separator arranged between the first electrode and the second electrode. A first storage portion and a second storage portion are respectively fluidly connected with the at least one electrochemical cell. A first liquid electrolyte and a second liquid electrolyte are located in the respective first storage portion and second storage portion. The first electrode has an area over which it is catalytically active with regard to the first liquid electrolyte and the second electrode has an area over which it is catalytically active with regard to the second liquid electrolyte such that the area of the first electrode is greater than the area of the second electrode.

IPC Classes  ?

  • H01M 8/18 - Regenerative fuel cells, e.g. redox flow batteries or secondary fuel cells
  • H01M 8/20 - Indirect fuel cells, e.g. fuel cells with redox couple being irreversible
  • H01M 8/0273 - Sealing or supporting means around electrodes, matrices or membranes with sealing or supporting means in the form of a frame

85.

Flow battery with carbon paper

      
Application Number 14364685
Grant Number 10637082
Status In Force
Filing Date 2011-12-20
First Publication Date 2014-10-09
Grant Date 2020-04-28
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Darling, Robert Mason
  • Stolar, Laura Roen

Abstract

A flow battery includes a liquid electrolyte having an electrochemically active specie. A flow field plate includes a first flow field channel and a second flow field channel that is separated from the first flow field channel by a rib. There is a flow path for the liquid electrolyte to flow over the rib between the channels. An electrode is arranged adjacent the flow field plate such that the liquid electrolyte that flows over the rib must flow through the electrode. The electrode includes a carbon paper that is catalytically active with regard to liquid electrolyte. The carbon paper defines a compressive strain of less than 20% at a compressive stress of 0.8 MPa and an uncompressed porosity in the range 60-85%.

IPC Classes  ?

  • H01M 8/04186 - Arrangements for control of reactant parameters, e.g. pressure or concentration of liquid-charged or electrolyte-charged reactants
  • H01M 8/18 - Regenerative fuel cells, e.g. redox flow batteries or secondary fuel cells
  • H01M 4/86 - Inert electrodes with catalytic activity, e.g. for fuel cells
  • H01M 4/96 - Carbon-based electrodes
  • H01M 8/20 - Indirect fuel cells, e.g. fuel cells with redox couple being irreversible

86.

Sensor hoop storage and transport apparatus

      
Application Number 14096627
Grant Number 09394802
Status In Force
Filing Date 2013-12-04
First Publication Date 2014-09-11
Grant Date 2016-07-19
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Warren, Eli C.
  • Hatton, Erik W.
  • Rice, Erik D.
  • Benoit, Corey A.

Abstract

A hoop support device (202) supports a hoop assembly (100). The hoop assembly comprises a structural hoop (102) and a plurality of wires. The hoop support device comprises a pedestal (206) having a mounting feature (224, 226) for mounting the hoop and a cover (208 pivotally mounted or mountable to the pedestal for rotation about a pivot axis (510). The cover has at least a lateral portion (250, 252) and a peripheral portion (254) for enclosing at least one said wire in an installed/closed condition.

IPC Classes  ?

  • F16M 11/10 - Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand allowing pivoting around a horizontal axis
  • F16M 11/16 - Heads - Details concerning attachment of head-supporting legs, with or without actuation of locking members therefor
  • B64D 27/00 - Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
  • F01D 11/20 - Actively adjusting tip-clearance
  • F01D 17/02 - Arrangement of sensing elements
  • F01D 17/20 - Devices dealing with sensing elements or final actuators or transmitting means between them, e.g. power-assisted
  • F01D 21/00 - Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
  • F01D 21/04 - Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator, e.g. indicating such position
  • F01D 25/28 - Supporting or mounting arrangements, e.g. for turbine casing

87.

Cap drain plug

      
Application Number 14186435
Grant Number 09371743
Status In Force
Filing Date 2014-02-21
First Publication Date 2014-08-21
Grant Date 2016-06-21
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Snyder, Ryan K.
  • Kisselbrack, Kari L.
  • Ruckey, Curtis J.
  • Howard, Robert

Abstract

A cap assembly includes a plunger mounted to a retainer pin and a latch operable to retract the retainer pin.

IPC Classes  ?

  • B65D 51/18 - Arrangements of closures with protective outer cap-like covers or of two or more co-operating closures
  • F01D 25/18 - Lubricating arrangements
  • F01M 11/04 - Filling or draining lubricant of or from machines or engines
  • F16N 19/00 - Lubricant containers for use in lubricators or lubrication systems
  • F01D 25/00 - Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
  • F16N 31/00 - Means for collecting, retaining, or draining-off lubricant in or on machines or apparatus

88.

Flow battery with two-phase storage

      
Application Number 14345719
Grant Number 09350039
Status In Force
Filing Date 2011-09-28
First Publication Date 2014-08-14
Grant Date 2016-05-24
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor Perry, Michael L.

Abstract

A flow battery includes at least one cell that has a first electrode, a second electrode spaced apart from the first electrode, and an electrolyte separator layer arranged between the first electrode and the second electrode. A reactant material is stored within a storage portion and selectively delivered to the at last one cell. At least one reactant material is present in a solid phase in the storage portion and is present in a liquid phase in the at least one cell.

IPC Classes  ?

  • H01M 8/18 - Regenerative fuel cells, e.g. redox flow batteries or secondary fuel cells
  • H01M 8/06 - Combination of fuel cells with means for production of reactants or for treatment of residues
  • H01M 8/20 - Indirect fuel cells, e.g. fuel cells with redox couple being irreversible
  • H01M 8/22 - Fuel cells in which the fuel is based on materials comprising carbon or oxygen or hydrogen and other elements; Fuel cells in which the fuel is based on materials comprising only elements other than carbon, oxygen or hydrogen
  • H01M 8/04 - Auxiliary arrangements, e.g. for control of pressure or for circulation of fluids

89.

Flexible shield for fluid connectors

      
Application Number 13630932
Grant Number 09366191
Status In Force
Filing Date 2012-09-28
First Publication Date 2014-08-07
Grant Date 2016-06-14
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Lior, Raphael
  • Derosa, Robert J.

Abstract

A flexible shield for fluid connectors of a gas turbine engine is disclosed. The flexible shield may comprise a flexible sleeve adapted to surround the fluid connector, and a coupling configured to secure the flexible sleeve onto a fluid tube proximate the fluid connector. A gas turbine engine employing such a flexible shield is also disclosed, as is a method of enclosing a fluid connector in a gas turbine engine using such a flexible shield.

IPC Classes  ?

  • F02C 7/25 - Fire protection or prevention
  • F02C 7/24 - Heat or noise insulation
  • F23R 3/60 - Support structures; Attaching or mounting means
  • F16L 57/00 - Protection of pipes or objects of similar shape against external or internal damage or wear
  • F02C 7/22 - Fuel supply systems

90.

High temperature directionally solidified and single crystal die casting

      
Application Number 14220915
Grant Number 09545664
Status In Force
Filing Date 2014-03-20
First Publication Date 2014-07-24
Grant Date 2017-01-17
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Bullied, Steven J.
  • Marcin, John Joseph
  • Bochiechio, Mario P.

Abstract

A high-temperature die casting die includes a first die plate with a first recess and a second die plate with a second recess, the first and second recesses defining a main part cavity and gating. A grain selector is in fluid communication with the main cavity, and an in situ zone refining apparatus is adapted to apply a localized thermal gradient to at least one of the first and second die plates. The localized thermal gradient and the at least one die plate are movable relative to each other so as to apply the localized thermal gradient along a first direction extending from the grain selector longitudinally across the main part cavity.

IPC Classes  ?

  • B22D 17/00 - Pressure die casting or injection die casting, i.e. casting in which the metal is forced into a mould under high pressure
  • B22D 17/22 - Dies; Die plates; Die supports; Cooling equipment for dies; Accessories for loosening and ejecting castings from dies
  • B22D 15/04 - Machines or apparatus for chill casting
  • B22D 27/04 - Influencing the temperature of the metal, e.g. by heating or cooling the mould
  • B22C 9/06 - Permanent moulds for shaped castings
  • C30B 11/14 - Single-crystal-growth by normal freezing or freezing under temperature gradient, e.g. Bridgman- Stockbarger method characterised by the seed, e.g. its crystallographic orientation

91.

Method and apparatus for reconditioning oxidized powder

      
Application Number 13730903
Grant Number 09364897
Status In Force
Filing Date 2012-12-29
First Publication Date 2014-07-03
Grant Date 2016-06-14
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor O'Neill, Christopher F.

Abstract

A metal powder reconditioning apparatus and method recondition contaminated residual powder from an additive manufacturing device. The apparatus and method include a reducing chamber that receives contaminated residual powder resulting from an additive manufacturing process and remove oxygen from the contaminated residual powder to produce reconditioned powder. The reconditioned powder may be reused in the additive manufacturing process, or may be stored in a non-oxidizing atmosphere for later reuse.

IPC Classes  ?

  • B22F 1/00 - Metallic powder; Treatment of metallic powder, e.g. to facilitate working or to improve properties
  • B22F 3/105 - Sintering only by using electric current, laser radiation or plasma

92.

Gaseous based desulfurization of alloys

      
Application Number 13723081
Grant Number 09481917
Status In Force
Filing Date 2012-12-20
First Publication Date 2014-06-26
Grant Date 2016-11-01
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Bochiechio, Mario P.
  • Marcin, John Joseph
  • Newton, Kirk C.
  • Kmetz, Michael A.

Abstract

A method for desulfurizing a metal alloy comprises heating the metal alloy to a molten state. A gaseous desulfurizing compound is bubbled through the molten alloy to form a solid sulfur-containing waste phase and a molten reduced-sulfur alloy phase. The solid waste phase and the molten reduced-sulfur alloy phase are separated. The gaseous desulfurizing compound includes a constituent element selected from the group: alkali metals, alkaline earth metals, and rare earth metals.

IPC Classes  ?

  • C22B 9/05 - Refining by treating with gases, e.g. gas flushing
  • B22D 1/00 - Treatment of fused masses in the ladle or the supply runners before casting

93.

Ovate swirler assembly for combustors

      
Application Number 13717203
Grant Number 09376985
Status In Force
Filing Date 2012-12-17
First Publication Date 2014-06-19
Grant Date 2016-06-28
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor Burd, Steven W.

Abstract

A swirler includes an inner shroud positioned radially inside an outer shroud. At least one of the outer shroud and inner shroud has a major diameter and a minor diameter, the major diameter being greater than the minor diameter, the major and minor diameters defining an ovate shape. The swirler further includes a plurality of vanes extending between the inner and outer shrouds.

IPC Classes  ?

  • F23R 3/28 - Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
  • F02G 3/00 - Combustion-product positive-displacement engine plants
  • F23R 3/14 - Air inlet arrangements for primary air inducing a vortex by using swirl vanes

94.

Full ring inner air-seal with locking nut

      
Application Number 13628298
Grant Number 09327368
Status In Force
Filing Date 2012-09-27
First Publication Date 2014-05-22
Grant Date 2016-05-03
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor Hagan, Benjamin F.

Abstract

A vane assembly has a vane including an inner platform with a mount rail extending radially inwardly toward an engine center axis. An air seal is attached to the inner platform. The air seal has a single-piece ring extending circumferentially about the engine center axis. A ring nut secures the air seal to the inner platform. A biasing member cooperates with the ring nut and air seal to seal fore and aft locations on the vane.

IPC Classes  ?

  • F01D 11/00 - Preventing or minimising internal leakage of working fluid, e.g. between stages
  • F01D 11/02 - Preventing or minimising internal leakage of working fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type
  • B23P 15/04 - Making specific metal objects by operations not covered by a single other subclass or a group in this subclass turbine or like blades from several pieces
  • F02C 7/28 - Arrangement of seals
  • F01D 11/04 - Preventing or minimising internal leakage of working fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type using sealing fluid, e.g. steam
  • F01D 11/10 - Preventing or minimising internal leakage of working fluid, e.g. between stages for sealing space between rotor blade tips and stator using sealing fluid, e.g. steam
  • F01D 9/06 - Fluid supply conduits to nozzles or the like

95.

Blast shield for high pressure compressor

      
Application Number 13662900
Grant Number 09322415
Status In Force
Filing Date 2012-10-29
First Publication Date 2014-05-22
Grant Date 2016-04-26
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor Rioux, Philip Robert

Abstract

A high pressure compressor includes an inner case wall, a plurality of flanges extending outwardly from the inner case wall, a shield that surrounds at least a portion of at least one of the plurality of flanges to define a chamber that at least partially encases at least one of the plurality of flanges, and a passage at least partially defined by the shield that allows air to circulate into the chamber.

IPC Classes  ?

  • F01D 11/18 - Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing by self-adjusting means using stator or rotor components with predetermined thermal response, e.g. selective insulation, thermal inertia, differential expansion
  • F04D 29/58 - Cooling; Heating; Diminishing heat transfer
  • F04D 19/02 - Multi-stage pumps
  • F04D 29/54 - Fluid-guiding means, e.g. diffusers
  • F01D 25/24 - Casings; Casing parts, e.g. diaphragms, casing fastenings

96.

System and method for sensing and mitigating hydrogen evolution within a flow battery system

      
Application Number 14161219
Grant Number 09356303
Status In Force
Filing Date 2014-01-22
First Publication Date 2014-05-15
Grant Date 2016-05-31
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Zaffou, Rachid
  • Pandy, Arun
  • Perry, Michael L.

Abstract

A method is provided for mitigating hydrogen evolution within a flow battery system that includes a plurality of flow battery cells, a power converter and an electrochemical cell. The method includes providing hydrogen generated by the hydrogen evolution within the flow battery system to the electrochemical cell. A first electrical current generated by an electrochemical reaction between the hydrogen and a reactant is sensed, and the sensed current is used to control an exchange of electrical power between the flow battery cells and the power converter.

IPC Classes  ?

  • H01M 2/38 - Arrangements for moving electrolytes
  • H01M 8/04 - Auxiliary arrangements, e.g. for control of pressure or for circulation of fluids
  • H01M 8/18 - Regenerative fuel cells, e.g. redox flow batteries or secondary fuel cells
  • H01M 8/20 - Indirect fuel cells, e.g. fuel cells with redox couple being irreversible
  • H02M 1/00 - APPARATUS FOR CONVERSION BETWEEN AC AND AC, BETWEEN AC AND DC, OR BETWEEN DC AND DC, AND FOR USE WITH MAINS OR SIMILAR POWER SUPPLY SYSTEMS; CONVERSION OF DC OR AC INPUT POWER INTO SURGE OUTPUT POWER; CONTROL OR REGULATION THEREOF - Details of apparatus for conversion

97.

Power cable and connector arrangement for a gas turbine engine

      
Application Number 13647614
Grant Number 09297307
Status In Force
Filing Date 2012-10-09
First Publication Date 2014-05-15
Grant Date 2016-03-29
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Lior, Raphael
  • Snape, Nathan

Abstract

A gas turbine engine component assembly according to an exemplary aspect of the present disclosure includes, among other things, a nacelle including a moveable portion. A generator is configured to be received within a space established by the nacelle. A plurality of cables are at least partially supported on the moveable portion of the nacelle, the plurality of cables being selectively electrically coupled with the generator.

IPC Classes  ?

  • F01D 25/24 - Casings; Casing parts, e.g. diaphragms, casing fastenings
  • F02C 7/00 - Features, component parts, details or accessories, not provided for in, or of interest apart from, groups ; Air intakes for jet-propulsion plants

98.

Film cooling channel array with multiple metering portions

      
Application Number 13660132
Grant Number 09309771
Status In Force
Filing Date 2012-10-25
First Publication Date 2014-05-01
Grant Date 2016-04-12
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Xu, Jinquan
  • Levasseur, Glenn

Abstract

A cooling channel array for a gas turbine engine is provided. The cooling channel array is carried by a component wall having an inner surface and an outer surface and comprises at least two metering portions that communicate with a diffusion cavity.

IPC Classes  ?

  • F01D 5/18 - Hollow blades; Heating, heat-insulating, or cooling means on blades

99.

Film cooling channel array having anti-vortex properties

      
Application Number 13660148
Grant Number 09316104
Status In Force
Filing Date 2012-10-25
First Publication Date 2014-05-01
Grant Date 2016-04-19
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor Xu, Jinquan

Abstract

A cooling channel array carried by a component wall of a gas turbine engine is provided. The cooling channel array comprises a diffusion cavity and a metering section. The metering section comprises a main hole and two or more side holes. The side holes may be separate from the main hole or may branch off of the main hole. The diffusion cavity may incorporate a lobed configuration to help diffuse cooling fluid as it exits the cooling channel array.

IPC Classes  ?

  • F28F 3/12 - Elements constructed in the shape of a hollow panel, e.g. with channels
  • F01D 5/18 - Hollow blades; Heating, heat-insulating, or cooling means on blades
  • F01D 9/06 - Fluid supply conduits to nozzles or the like
  • F23R 3/00 - Continuous combustion chambers using liquid or gaseous fuel

100.

Gas turbine engine cooling hole with circular exit geometry

      
Application Number 13629705
Grant Number 09376920
Status In Force
Filing Date 2012-09-28
First Publication Date 2014-04-03
Grant Date 2016-06-28
Owner
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
  • RAYTHEON TECHNOLOGIES CORPORATION (USA)
Inventor
  • Mcbrien, John
  • Spangler, Brandon W.
  • Devore, Matthew A.

Abstract

A gas turbine engine component includes a structure having an exterior surface. A cooling hole extends from a cooling passage to the exterior surface to provide an exit area on the exterior surface that is substantially circular in shape. A gas turbine engine includes a compressor section and a turbine section. A combustor is provided between the compressor and turbine sections. A component in at least one of the compressor and turbine sections has an exterior surface. A film cooling hole extends from a cooling passage to the exterior surface to provide an exit area that is substantially circular in shape. A method of machining a film cooling hole includes providing a component having an internal cooling passage and an exterior surface, machining a film cooling hole from the exterior surface to the internal cooling passage to provide a substantially circular exit area on the exterior surface.

IPC Classes  ?

  • F01D 5/18 - Hollow blades; Heating, heat-insulating, or cooling means on blades
  • F23R 3/00 - Continuous combustion chambers using liquid or gaseous fuel
  • F23R 3/06 - Arrangement of apertures along the flame tube
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