Howmet Aerospace Inc.

United States of America

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2024 March 1
2024 January 2
2023 December 1
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IPC Class
F16B 19/10 - Hollow rivets; Multi-part rivets fastened by expanding mechanically 16
F16B 19/05 - Bolts fastening by swaged-on collars 14
B21J 15/02 - Riveting procedures 12
B23K 11/00 - Resistance welding; Severing by resistance heating 10
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 10
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Status
Pending 28
Registered / In Force 120
Found results for  patents
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1.

Vehicle wheel hub cover

      
Application Number 29799398
Grant Number D1017495
Status In Force
Filing Date 2021-07-14
First Publication Date 2024-03-12
Grant Date 2024-03-12
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Mason, Douglas P.
  • Wallace, Spencer

2.

FASTENING COLLARS, MULTI-PIECE FASTENERS, AND METHODS FOR FASTENING

      
Application Number 18256571
Status Pending
Filing Date 2021-12-14
First Publication Date 2024-01-25
Owner HOWMET AEROSPACE INC. (USA)
Inventor Arciniega, Oviedo

Abstract

The present disclosure relates to fastening collars, multi-piece fasteners, and methods for fastening. A fastening collar comprises a first collar end, a second collar end, and an elongate portion intermediate the first collar end and the second collar end and defining a longitudinal axis of the fastening collar. The elongate portion comprises a first region adjacent the first collar end, extending a first distance along the longitudinal axis; a second region adjacent to the second collar end, extending a second distance along the longitudinal axis, and comprising a flange; and an inner collar surface defining collar cavity extending through the elongate portion from the first collar end to the second collar end. The second collar end extends away from the longitudinal axis of the elongate portion at a first angle offset from an angle perpendicular to the longitudinal axis of the elongate portion.

IPC Classes  ?

  • F16B 19/05 - Bolts fastening by swaged-on collars
  • 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 31/04 - Screwed connections specially modified in view of tensile load; Break-bolts for maintaining constant tensile load

3.

METALLIC SUBSTRATE TREATMENT METHODS AND ARTICLES COMPRISING A PHOSPHONATE FUNCTIONALIZED LAYER

      
Application Number 18478059
Status Pending
Filing Date 2023-09-29
First Publication Date 2024-01-25
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Scott, Ryan N.
  • Robare, Kevin M.
  • Giocondi, Jennifer L.
  • Menegazzo, Nicola
  • Weiler, Kelly M.

Abstract

Metallic substrate treatment methods and articles comprising a phosphonate functionalized layer are provided. The method comprises contacting a metallic substrate comprising at least one of aluminum and an aluminum alloy with a fluid to form a phosphonate functionalized layer on at least a region of the metallic substrate. The fluid comprises at least one of a phosphonate containing acid and a derivative thereof. At least one of the phosphonate containing acid and the derivative thereof comprises a pKa of a first acidic proton. The fluid comprises a pH at least 0.5 pH value greater than the pKa of the first acidic proton. The article comprises a metallic substrate comprising aluminum or an aluminum alloy and a phosphonate functionalized layer on at least a region of the metallic substrate.

IPC Classes  ?

  • C23C 22/07 - Chemical surface treatment of metallic material by reaction of the surface with a reactive liquid, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using aqueous solutions using aqueous acidic solutions with pH < 6 containing phosphates
  • B05D 7/14 - Processes, other than flocking, specially adapted for applying liquids or other fluent materials to particular surfaces or for applying particular liquids or other fluent materials to metal, e.g. car bodies
  • C23C 22/73 - Chemical surface treatment of metallic material by reaction of the surface with a reactive liquid, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals characterised by the process
  • C23C 22/76 - Applying the liquid by spraying
  • C23G 1/12 - Light metals
  • C23G 1/22 - Light metals

4.

Fastening collars, multi-piece fastening systems, and methods of fastening

      
Application Number 16826941
Grant Number 11841041
Status In Force
Filing Date 2020-03-23
First Publication Date 2023-12-12
Grant Date 2023-12-12
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Wilcox, Robert B.
  • Branch, Justin
  • White, Ryan J.

Abstract

Fastening collars, multi-piece fastening systems, and methods of fastening are provided. The fastening collar comprises a first end, a second end, and an elongate portion intermediate the first end and the second end and defining a longitudinal axis of the fastening collar. The elongate portion comprises a first region adjacent the first end, a second region intermediate the first region and the second end, and a cavity. The first region comprises a first diameter and is configured to be received by a bore of a structure. The second region comprises a second diameter greater than the first diameter. The cavity extends through the elongate portion and is configured to receive at least a portion of a shank of the multi-piece fastening system. The elongate portion is configured to at least partially deform onto the shank responsive to forcible contact between the second region and an installation tool.

IPC Classes  ?

  • F16B 19/10 - Hollow rivets; Multi-part rivets fastened by expanding mechanically

5.

Vehicle wheel cover

      
Application Number 29799402
Grant Number D1003797
Status In Force
Filing Date 2021-07-14
First Publication Date 2023-11-07
Grant Date 2023-11-07
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Mason, Douglas P.
  • Wallace, Spencer

6.

Methods for fastening

      
Application Number 17906122
Grant Number 11802581
Status In Force
Filing Date 2021-03-15
First Publication Date 2023-10-31
Grant Date 2023-10-31
Owner Howmet Aerospace Inc. (USA)
Inventor
  • Fedusa, Anthony J.
  • Spinella, Donald J.

Abstract

Methods of fastening are provided. A method comprises contacting a fastener with a first layer of an assembly at a first location. The assembly comprises the first layer, a third layer, and a second layer positioned intermediate the first layer and the third layer. The first layer, the third layer, and the fastener are electrically conductive. The second layer defines a gap and the first location is in communication with the gap. Electrical communication is formed between the assembly and the fastener. The first layer is fastened to the third layer through the gap in the second layer with the fastener. The fastening comprises resistance welding the fastener to the third layer.

IPC Classes  ?

  • F16B 5/04 - Joining sheets or plates to one another or to strips or bars parallel to them by means of riveting
  • B23K 11/11 - Spot welding
  • B21J 15/08 - Riveting by applying heat to the end parts of the rivets to enable heads to be formed
  • B23K 11/00 - Resistance welding; Severing by resistance heating
  • F16B 5/08 - Joining sheets or plates to one another or to strips or bars parallel to them by means of welds or the like
  • B21J 15/02 - Riveting procedures
  • B23K 103/18 - Dissimilar materials

7.

Self-forming thread blind fastener

      
Application Number 18004717
Grant Number 11959504
Status In Force
Filing Date 2021-07-16
First Publication Date 2023-08-10
Grant Date 2024-04-16
Owner HOWMET AEROSPACE INC. (USA)
Inventor Brennetot, Thomas

Abstract

Self-forming thread blind fasteners and methods for fastening are provided. The self-forming thread blind fastener comprises a sleeve and a pin. The sleeve comprises a first sleeve end, a second sleeve end, an elongate portion, and an inner wall defining a bore. The pin is configured to be at least partially received by the bore. The pin comprises a first pin end, a second pin end, a pin head portion, an at least partially threaded portion, a shank intermediate, and a driving portion. The at least partially threaded portion is configured to form threads on at least a portion of the inner wall of the sleeve. The driving portion is configured to receive a torque to rotate the pin within the sleeve and thereby axially compress and deform the sleeve and form the threads on the at least a portion of the inner wall of the sleeve.

IPC Classes  ?

  • F16B 19/10 - Hollow rivets; Multi-part rivets fastened by expanding mechanically

8.

FLUID TIGHT BLIND FASTENERS AND METHODS FOR FASTENING

      
Application Number 18000143
Status Pending
Filing Date 2021-06-16
First Publication Date 2023-08-03
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Haylock, Luke L.
  • Balls, Todd A.
  • Huang, Junjie

Abstract

Fluid tight blind fasteners and methods tor fastening are provided. The sleeve comprises a first sleeve end comprising a first inner surface, a second sleeve end comprising a second inner surface, and an elongate portion extending from the first sleeve end to the second sleeve end. The first inner surface and the second inner surface define a sleeve cavity extending into the sleeve from the first sleeve end toward or to the second sleeve end. The pin is configured to be at least partially received by the sleeve cavity. The pin comprises a first pin end portion configured to receive a torque, a second pin end, and a shank extending from the first pin end portion to the second pin end. Tire shank comprises threads and the threads are configured to form threads on the second inner surface of the sleeve.

IPC Classes  ?

  • F16B 19/10 - Hollow rivets; Multi-part rivets fastened by expanding mechanically
  • F16B 5/04 - Joining sheets or plates to one another or to strips or bars parallel to them by means of riveting

9.

BLIND FASTENER

      
Application Number 18188951
Status Pending
Filing Date 2023-03-23
First Publication Date 2023-07-20
Owner Howmet Aerospace Inc. (USA)
Inventor Haylock, Luke L.

Abstract

A method includes inserting a machining tool through a hole of at least one workpiece that includes a first surface and a second surface opposite the first surface and extends from the first surface to the second surface. The hole forms an inner wall. The machining tool includes a shaft and a cutting tip proximate to one end of the shaft. The cutting tip includes a cutting portion. The method includes positioning the cutting portion of the cutting tip to abut an edge of the hole. The edge is located at a junction of the second surface of the one of the at least one workpiece and the inner wall. The method includes forming a surface modification at the edge with the cutting tip. The method includes removing the machining tool from the hole. The method includes installing a fastener within the hole. The fastener engages the surface modification.

IPC Classes  ?

  • B23B 27/14 - Cutting tools of which the bits or tips are of special material

10.

BLIND FASTENER

      
Application Number 17542036
Status Pending
Filing Date 2021-12-03
First Publication Date 2023-06-08
Owner Howmet Aerospace Inc. (USA)
Inventor Haylock, Luke L.

Abstract

A method includes inserting a machining tool through a hole of at least one workpiece that includes a first surface and a second surface opposite the first surface and extends from the first surface to the second surface. The hole forms an inner wall. The machining tool includes a shaft and a cutting tip proximate to one end of the shaft. The cutting tip includes a cutting portion. The method includes positioning the cutting portion of the cutting tip to abut an edge of the hole. The edge is located at a junction of the second surface of the one of the at least one workpiece and the inner wall. The method includes forming a surface modification at the edge with the cutting tip. The method includes removing the machining tool from the hole. The method includes installing a fastener within the hole. The fastener engages the surface modification.

IPC Classes  ?

  • B23B 35/00 - Methods for boring or drilling, or for working essentially requiring the use of boring or drilling machines; Use of auxiliary equipment in connection with such methods

11.

FASTENING SYSTEMS, FASTENING SYSTEM INSTALLATION APPARATUS, AND METHODS FOR FASTENING

      
Application Number 17906874
Status Pending
Filing Date 2021-04-02
First Publication Date 2023-05-11
Owner Howmet Aerospace Inc. (USA)
Inventor Wilcox, Robert B.

Abstract

Fastening systems, fastening system installation apparatus, and methods for fastening are provided. The fastening system installation apparatus comprises a sleeve and an anvil. The sleeve comprises a first sleeve end and a second sleeve end. A sleeve cavity extends into the sleeve from the first sleeve end. The anvil is slidably received by the sleeve cavity. The anvil comprises a first anvil end, a second anvil end, and at least two portions formed by at least two channels extending from the first anvil end. The at least two portions define an anvil cavity configured to receive a fastening collar and inner surfaces of the at least two portions are configured to deform the fastening collar. The sleeve is configured to radially displace the at least two portions inward relative to the longitudinal axis responsive to forcible contact between the first anvil end and the first sleeve end.

IPC Classes  ?

12.

BLIND FASTENER

      
Application Number 17515108
Status Pending
Filing Date 2021-10-29
First Publication Date 2023-05-04
Owner Howmet Aerospace Inc. (USA)
Inventor Haylock, Luke L.

Abstract

A fastener includes a sleeve having a tubular portion including a first end and a second end; a head located at the first end; a deformable portion located at the second end; and a core pin having a first end and a second end. The core pin has an elongated shank portion between the first end of the core pin and the second end of the core pin including a threaded portion proximate the second end of the core pin and a head at the first end of the core pin. The sleeve is configured to receive the core pin. The fastener is configured to secure a plurality of workpieces to one another. The deformable portion is configured deflect in response to compression of the deformable portion by the head of the core pin, to form a flared connection that engages a surface of one of the plurality of workpieces.

IPC Classes  ?

  • F16B 19/10 - Hollow rivets; Multi-part rivets fastened by expanding mechanically

13.

Wheel Cover Assembly with Installable Wheel Rib and Wheel Cover

      
Application Number 18084022
Status Pending
Filing Date 2022-12-19
First Publication Date 2023-04-20
Owner Howmet Aerospace Inc. (USA)
Inventor
  • Wallace, Spencer
  • Brest, Matt

Abstract

A wheel cover assembly for a vehicle wheel may include a wheel rib that is attachable to a rim inner surface of a wheel rim of the vehicle wheel, a cover body having a cover body outer surface, a cover body inner surface, and a cover body outer edge having an outer diameter that is greater than an inner diameter of the wheel rib and less than an inner diameter of an open end flange of the wheel rim. A cover mounting mechanism operatively connected to the cover body has a cover locking position wherein the cover mounting mechanism engages the wheel rib to retain the wheel rib between the cover mounting mechanism and the cover body and secure the wheel cover assembly to the vehicle wheel when the wheel rib is attached to the rim inner surface.

IPC Classes  ?

  • B60B 7/08 - Fastening arrangements therefor having gripping elements consisting of formations integral with the cover
  • B60B 7/06 - Fastening arrangements therefor
  • B60B 21/02 - Rims characterised by transverse section

14.

MULTI-PIECE FASTENER INCLUDING A LOCKBOLT COLLAR ASSEMBLY AND METHOD OF FASTENING

      
Application Number 17907289
Status Pending
Filing Date 2021-04-30
First Publication Date 2023-04-13
Owner Howmet Aerospace Inc. (USA)
Inventor Wilcox, Robert B.

Abstract

Non-limiting embodiments of a multi-piece fastener and a fastening method are disclosed. The multi-piece fastener comprises a fastening collar and a pin. The fastening collar comprises a first collar end, a second collar end, and an inner collar surface extending from the first collar end to the second collar end. The inner collar surface comprises a first lock region and defines a collar cavity. The pin is configured to be at least partially received by the collar cavity. The pin comprises a first pin end, a second pin end, and a shank extending intermediate the first pin end and the second pin end. The shank comprises a second lock region configured to engage the first lock region to form an interference fit between the fastening collar and the pin when the pin is received in the collar cavity. The fastening collar is configured to be deformed onto the shank.

IPC Classes  ?

  • F16B 19/05 - Bolts fastening by swaged-on collars

15.

MULTI-PIECE FASTENER COMPRISING A TAPERED THREADED PORTION AND METHOD OF FASTENING

      
Application Number 17907350
Status Pending
Filing Date 2021-05-26
First Publication Date 2023-04-13
Owner Howmet Aerospace Inc. (USA)
Inventor
  • Branch, Justin S.
  • Wilcox, Robert B.

Abstract

A fastener comprising a pin and a collar. The pin comprising a shank comprising a tapered lock groove thread profile; and a head portion configured to receive a torque. The collar configured to be deformed onto and secured to the shank, wherein the collar comprises an external surface configured to receive a torque such that the collar can be removed from the shank after deformation.

IPC Classes  ?

  • 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
  • F16B 33/02 - Shape of thread; Special thread-forms
  • F16B 37/04 - Devices for fastening nuts to surfaces, e.g. sheets, plates

16.

ANTI-SHINGLE RIVETS

      
Application Number 17760405
Status Pending
Filing Date 2021-03-04
First Publication Date 2023-03-09
Owner Howmet Aerospace Inc. (USA)
Inventor
  • Wilcox, Robert B.
  • Wojciechowski, Stanley E.

Abstract

Anti-shingle rivets are provided. The anti-shingle rivets comprise a head portion comprising an outer edge configured to inhibit shingling in a rivet delivery system and a shank extending from the head portion.

IPC Classes  ?

17.

VEHICLE WHEELS AND METHODS OF MAKING VEHICLE WHEELS

      
Application Number 17758117
Status Pending
Filing Date 2020-09-21
First Publication Date 2023-02-16
Owner Howmet Aerospace Inc. (USA)
Inventor
  • Mason, Douglas P.
  • Ciccola, Gabriele F.
  • Wallace, Spencer
  • Finn, Kellen M.

Abstract

Vehicle wheels and methods of making vehicle wheels are provided. A vehicle wheel comprises a generally annular first region, a second region, and a flange extension. The first region comprises an inner surface and an outer surface comprising a tire bead seat. The second region extends radially inwardly from the first region. The second region is configured to mount to a vehicle axle. The flange extension extends from the first region in a direction away from the second region. The flange extension comprises a first extension end integral with the first region, a second extension end, and an elongate portion intermediate the first extension end and the second extension end. The elongate portion comprising a first portion with a thickness less than a thickness of the second extension end.

IPC Classes  ?

  • B60B 21/02 - Rims characterised by transverse section
  • B60B 21/10 - Rims characterised by the form of tyre-seat or flange, e.g. corrugated
  • B60B 7/06 - Fastening arrangements therefor
  • B60B 7/02 - Wheel cover discs, rings, or the like, for ornamenting, protecting, or obscuring, wholly or in part, the wheel body, rim, hub, or tyre sidewall made essentially in one part

18.

PRELOAD CONTROLLED STUD LOCKBOLT

      
Application Number 17966437
Status Pending
Filing Date 2022-10-14
First Publication Date 2023-02-02
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Brennetot, Thomas
  • Brunet, Arnaud
  • Coulon, Christophe

Abstract

A fastener including a pin member having a shank portion, a threaded portion having a thread, a lock portion having at least one lock groove, and a pull portion located having at least one pull groove. The threaded portion is adapted to be engaged threadedly with a threaded hole of a workpiece to install the pin member therein. The fastener includes a swage collar adapted to be installed into the at least one lock groove of the lock portion to secure a plurality of workpieces. The pull portion is adapted to break off when the fastener is installed.

IPC Classes  ?

  • F16B 19/05 - Bolts fastening by swaged-on collars
  • F16B 23/00 - Specially-shaped heads of bolts or screws for rotations by a tool
  • F16B 39/02 - Locking of screws, bolts, or nuts in which the locking takes place after screwing down
  • 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

19.

VEHICLE WHEELS AND METHODS OF USE

      
Application Number 17375460
Status Pending
Filing Date 2021-07-14
First Publication Date 2023-01-19
Owner Howmet Aerospace Inc. (USA)
Inventor
  • Mason, Douglas P.
  • Wallace, Spencer
  • Sutadji, Michael

Abstract

Vehicle wheels and methods of use are provided. The vehicle wheel comprises a first region, a second region, and a third region. The first region is generally annular and comprises a first flange, a second flange opposite the first flange, and a continuous wall comprising an inner surface and an outer surface. A first tire bead seat and a second tire bead seat are defined on the outer surface. The second region is configured to mount to a vehicle axle and is offset from the first flange by an offset distance. The third region connects the second region and the third region and extends inwardly towards the longitudinal axis from an attachment location on the first region to the second region. The third region comprises a first thickness and the second region comprises a second thickness. The first thickness is no greater than 75% of the second thickness.

IPC Classes  ?

  • B60B 21/02 - Rims characterised by transverse section
  • B60B 3/02 - Disc wheels, i.e. wheels with load-supporting disc body with a single disc body integral with rim
  • B60B 21/10 - Rims characterised by the form of tyre-seat or flange, e.g. corrugated
  • B60B 3/06 - Disc wheels, i.e. wheels with load-supporting disc body formed by casting

20.

MULTI-PIECE FASTENERS, FASTENING COLLAR INSTALLATION APPARATUS, AND METHODS OF FASTENING

      
Application Number 17754026
Status Pending
Filing Date 2019-11-06
First Publication Date 2022-12-15
Owner Howmet Aerospace Inc. (USA)
Inventor
  • Wilcox, Robert B.
  • Kingsbury, Thomas R.

Abstract

Multi-piece fasteners, fastening collar installation apparatus, and methods of fastening are provided. The multi-piece fastener comprises a fastening collar and a pin. The fastening collar comprises a first collar end, a second collar end, and a collar cavity. The collar cavity extends from the first collar end to the second collar end. The pin is configured to be at least partially received by the collar cavity. The pin comprises a first pin end comprising a head portion, a second pin end comprising a pull region, and a shank. The pull region is generally cylindrical and smooth and is configured to form at least one of an annular shoulder, a groove, a thread, and other feature responsive to forcible contact from a fastening collar installation apparatus. The shank extends intermediate the first pin end and the second pin end. The fastening collar is configured to be deformed onto the shank.

IPC Classes  ?

  • F16B 19/05 - Bolts fastening by swaged-on collars
  • F16B 5/04 - Joining sheets or plates to one another or to strips or bars parallel to them by means of riveting

21.

VEHICLE WHEELS AND METHODS OF MAKING VEHICLE WHEELS

      
Application Number 17755360
Status Pending
Filing Date 2020-12-08
First Publication Date 2022-11-24
Owner Howmet Aerospace Inc. (USA)
Inventor Wallace, Spencer

Abstract

Vehicle wheels and methods of making vehicle wheels are provided. The vehicle wheel comprises a generally annular first region, a second region, and a flange region. The first region comprises an outer surface, an inner surface, a first end, and a second end. The second region extends radially inwardly from the first region, and the second region is configured to mount to a vehicle axle. The flange region extends from the first region. The flange region comprises a first flange end adjacent to the first end of the first region, a second flange end, and a curved elongate portion extending intermediate the first flange end and the second flange end. The curved elongate portion comprises a first thickness no greater than 0.3 inches and a second thickness greater than 0.3 inches.

IPC Classes  ?

  • B60B 21/10 - Rims characterised by the form of tyre-seat or flange, e.g. corrugated
  • B21D 53/26 - Making other particular articles wheels or the like

22.

FASTENING COLLAR INSTALLATION APPARATUS AND METHODS OF INSTALLING A FASTENER SYSTEM

      
Application Number 17633713
Status Pending
Filing Date 2019-11-22
First Publication Date 2022-10-06
Owner Howmet Aerospace Inc. (USA)
Inventor Brunet, Arnaud

Abstract

Fastening collar installation apparatus and methods of installing a fastener system are provided. The fastening collar installation apparatus comprises an anvil, a sleeve, and a lever. The sleeve comprises a first section comprising a first sleeve end and a second sleeve end, a sleeve cavity, and a slot. The first sleeve end is intermediate the anvil and the second sleeve end. The slot extends a first distance from the first sleeve end. The lever is slidably received by the slot of the sleeve and configured to move between a first lever position in the slot and a second lever position in the slot. The lever comprises a second distance from a first lever end to a second lever end. The second distance is less than the first distance.

IPC Classes  ?

  • B21J 15/02 - Riveting procedures
  • B21J 15/32 - Devices for inserting or holding rivets in position with or without feeding arrangements

23.

METALLIC SUBSTRATE TREATMENT METHODS AND ARTICLES COMPRISING A PHOSPHONATE FUNCTIONALIZED LAYER

      
Application Number 17433312
Status Pending
Filing Date 2019-12-18
First Publication Date 2022-05-12
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Scott, Ryan N.
  • Robare, Kevin M.
  • Giocondi, Jennifer L.
  • Menegazzo, Nicola
  • Weiler, Kelly M.

Abstract

Metallic substrate treatment methods and articles comprising a phosphonate functionalized layer are provided. The method comprises contacting a metallic substrate comprising at least one of aluminum and an aluminum alloy with a fluid to form a phosphonate functionalized layer on at least a region of the metallic substrate. The fluid comprises at least one of a phosphonate containing acid and a derivative thereof. At least one of the phosphonate containing acid and the derivative thereof comprises a pKa of a first acidic proton. The fluid comprises a pH at least 0.5 pH value greater than the pKa of the first acidic proton. The article comprises a metallic substrate comprising aluminum or an aluminum alloy and a phosphonate functionalized layer on at least a region of the metallic substrate.

IPC Classes  ?

  • C23C 22/07 - Chemical surface treatment of metallic material by reaction of the surface with a reactive liquid, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using aqueous solutions using aqueous acidic solutions with pH < 6 containing phosphates
  • C23G 1/12 - Light metals
  • C23G 1/22 - Light metals
  • C23C 22/76 - Applying the liquid by spraying
  • C23C 22/73 - Chemical surface treatment of metallic material by reaction of the surface with a reactive liquid, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals characterised by the process
  • B05D 7/14 - Processes, other than flocking, specially adapted for applying liquids or other fluent materials to particular surfaces or for applying particular liquids or other fluent materials to metal, e.g. car bodies

24.

Vehicle wheel disc

      
Application Number 29676089
Grant Number D0951165
Status In Force
Filing Date 2019-01-08
First Publication Date 2022-05-10
Grant Date 2022-05-10
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Ciccola, Gabriele F.
  • Prasad, Santosh
  • Belousov, Igor
  • Degeorge, Grant A.
  • Rovito, Anton J.

25.

BLIND FASTENERS AND METHODS OF FASTENING

      
Application Number 17594569
Status Pending
Filing Date 2019-05-15
First Publication Date 2022-04-28
Owner Howmet Aerospace Inc. (USA)
Inventor
  • Pierce, Troy Don
  • Wilcox, Robert B.
  • Branch, Justin

Abstract

Blind fasteners and methods of fastening are provided. A blind fastener comprises a sleeve and a mandrel. The sleeve is adapted for installation into a threaded bore in a structure. The sleeve comprises a head portion configured to receive a torque, a first sleeve end, a second sleeve end, an elongate portion extending intermediate the first sleeve end and the second sleeve end, and a cavity extending from the first sleeve end to the second sleeve end. The mandrel is at least partially disposed through the cavity of the sleeve. The mandrel comprises a first mandrel end disposed adjacent to the first sleeve end. The first mandrel end comprises an enlarged portion having a diameter greater than a diameter of the cavity. The elongate portion is configured to at least partially deform into threads of the threaded bore responsive to forcible contact between the enlarged portion and the sleeve.

IPC Classes  ?

  • F16B 19/10 - Hollow rivets; Multi-part rivets fastened by expanding mechanically
  • F16B 37/00 - Nuts or like thread-engaging members

26.

Blind fastener and method of installation thereof

      
Application Number 17423980
Grant Number 11885358
Status In Force
Filing Date 2019-02-07
First Publication Date 2022-04-21
Grant Date 2024-01-30
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Wilcox, Robert B.
  • Smith, James Thomas
  • Pierce, Troy Don

Abstract

The present disclosure relates to a blind fastener and a method of installation thereof. The blind fastener comprises a sleeve and a mandrel. The sleeve comprises a first sleeve end, a second sleeve end, and a cavity extending from the first sleeve end to the second sleeve end. The mandrel is configured to be at least partially received by the cavity of the sleeve. The mandrel comprises a first mandrel end disposed adjacent to the first sleeve end and comprising an enlarged portion having a diameter greater than a diameter of the cavity, a second mandrel end comprising a pull region, and a shank region extending intermediate the first mandrel end and the second mandrel end. The pull region comprises an axial length no greater than four times a diameter of the shank region and is configured to be engaged by an installation tool.

IPC Classes  ?

  • F16B 19/10 - Hollow rivets; Multi-part rivets fastened by expanding mechanically

27.

Fastening collar removal apparatus, methods of making a fastening collar removal apparatus, and methods of removing a fastening collar secured to a fastener

      
Application Number 17420729
Grant Number 11628507
Status In Force
Filing Date 2019-02-28
First Publication Date 2022-04-07
Grant Date 2023-04-18
Owner HOWMET AEROSPACE INC. (USA)
Inventor Kingsbury, Thomas R.

Abstract

Fastening collar removal apparatus, methods of making fastening collar removal apparatus, and methods of removing a fastening collar secured to a fastener are provided. A fastening collar removal apparatus includes a collet including a first section including a substantially cylindrical shape and a second section operatively coupled to the first section. The second section includes a collet cavity extending therein. The collet cavity is configured to receive at least a portion of a collar. The second section includes at least two fingers formed by at least two axial channels in the second section. At least one of the at least two fingers includes a blade extending inwardly relative to a longitudinal axis of the collet. In an open configuration of the collet, each of the at least two fingers includes an outward taper relative to a longitudinal axis of the collet.

IPC Classes  ?

  • B23D 29/00 - Hand-held metal-shearing or metal-cutting devices

28.

ALUMINUM-MAGNESIUM-ZINC ALUMINUM ALLOYS

      
Application Number 17400429
Status Pending
Filing Date 2021-08-12
First Publication Date 2022-03-31
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Lin, Jen C.
  • Wen, Wei
  • Prasad, Santosh
  • Crowley, Mark D.
  • Ciccola, Gabriele F.
  • Brest, Matthew C.

Abstract

New aluminum alloys having magnesium and zinc are disclosed. The new magnesium-zinc aluminum alloys may include from 2.5 to 4.0 wt. % Mg, from 2.25 to 4.0 wt. % Zn, wherein (wt. % Mg/wt. % Zn)≥1.0, and wherein (wt. % Mg/wt. % Zn)≤1.6, from 0.20 to 0.9 wt. % Mn, from 0.10 to 0.40 wt. % Cu, up to 1.0 wt. % Li, up to 0.50 wt. % Fe, up to 0.50 wt. % Si, and optional secondary element(s), the balance being aluminum, optional incidental elements and impurities.

IPC Classes  ?

  • C22C 21/08 - Alloys based on aluminium with magnesium as the next major constituent with silicon
  • C22F 1/047 - 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 of alloys with magnesium as the next major constituent
  • 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
  • B22F 3/24 - After-treatment of workpieces or articles

29.

ELECTRODES FOR RESISTANCE WELDING AND METHOD OF USE THEREOF

      
Application Number 17479816
Status Pending
Filing Date 2021-09-20
First Publication Date 2022-03-24
Owner Howmet Aerospace Inc. (USA)
Inventor
  • Spinella, Donald J.
  • Fedusa, Anthony J.

Abstract

A hybrid electrode for resistance spot welding and a method of resistance welding are provided. The hybrid electrode comprises a pin and a collar member. The pin comprises an electrically conductive material and a pin contact surface. The collar member comprises a material that is at least one of less electrically conductive than the electrically conductive material of the pin and less thermally conductive than the electrically conductive material of the pin. The collar member comprises a collar member contact surface, and defines an inner cavity and a longitudinal axis. The pin is at least partially disposed in the inner cavity and the pin contact surface extends away from the collar member and is offset a distance along the longitudinal axis from the collar member contact surface.

IPC Classes  ?

30.

RESISTANCE WELDING FASTENER, APPARATUS AND METHODS

      
Application Number 17519905
Status Pending
Filing Date 2021-11-05
First Publication Date 2022-02-24
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Spinella, Donald J.
  • Bergstrom, Daniel

Abstract

An apparatus and method for fastening dissimilar materials like steel, plastic and aluminum. A resistance welding fastener having multiple layers may be used with or without a sealant. The fastener may be used to form an aluminum covered steel laminate via a hemming pattern of attachment. The fastener may have a solid shaft or have an extended reach and have features for interacting with the welding electrode. A variety of electrode tips may be employed to cooperate with the fastener.

IPC Classes  ?

  • H01R 4/02 - Soldered or welded connections
  • B23K 11/11 - Spot welding
  • B23K 11/20 - Resistance welding; Severing by resistance heating taking account of the properties of the material to be welded of different metals
  • B23K 35/02 - Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape
  • H01R 43/02 - Apparatus or processes specially adapted for manufacturing, assembling, maintaining, or repairing of line connectors or current collectors or for joining electric conductors for soldered or welded connections
  • F16B 37/06 - Devices for fastening nuts to surfaces, e.g. sheets, plates by means of welding or riveting

31.

Rivet dispensing systems and methods of use thereof

      
Application Number 17295238
Grant Number 11471932
Status In Force
Filing Date 2019-12-13
First Publication Date 2021-12-23
Grant Date 2022-10-18
Owner
  • HOWMET AEROSPACE INC. (USA)
  • CenterLine (Windsor) Limited (Canada)
Inventor
  • Vanderzwet, Daniel Peter
  • Britton, Simon Maurice
  • Koscielski, Larry Frank
  • Michaud, Eric Jean
  • Simone, David Mario
  • Spinella, Donald J.
  • Iasella, Gino N.
  • Bergstrom, Daniel
  • Wilcox, Robert B.
  • Kingsbury, Thomas R.
  • Musgrove, Graham Scott

Abstract

Rivet dispenser systems and methods of use thereof are provided. In a non-limiting embodiment, the rivet dispenser system comprises a rivet receiving member defining a channel therein, and a seat member. The channel includes a curved region. The rivet receiving member comprises a first port and a second port. The first port communicates with the channel and is configured to receive rivets. The second port communicates with the channel and is configured to dispense rivets. The channel extends between the first port and the second port and is configured to transport rivets from the first port to the second port in a series arrangement and in a preselected orientation. The seat member communicates with the second port and is configured to selectively engage with a rivet holder of a resistance spot rivet welding apparatus and introduce a single rivet to the rivet holder at one time.

IPC Classes  ?

  • B21J 15/32 - Devices for inserting or holding rivets in position with or without feeding arrangements
  • B21J 15/08 - Riveting by applying heat to the end parts of the rivets to enable heads to be formed
  • B23K 11/11 - Spot welding

32.

Rivet dispenser reloading systems and methods of use thereof

      
Application Number 17288346
Grant Number 11541449
Status In Force
Filing Date 2019-12-13
First Publication Date 2021-12-09
Grant Date 2023-01-03
Owner
  • HOWMET AEROSPACE INC. (USA)
  • CENTERLINE (WINDSOR) LIMITED (Canada)
Inventor
  • Cosgrave, Stuart Cameron
  • Wasyliniuk, Kyle Alexander
  • Spinella, Donald J.
  • Bergstrom, Daniel
  • Iasella, Gino N.

Abstract

Rivet dispenser reloading systems and methods of use thereof are provided. A non-limiting embodiment of a rivet dispenser reloading system comprises a receiving member defining a channel therein, and a first gate. The rivet receiving member comprises a first port and a second port that communicate with the channel. The first port is configured to receive rivets. The second port is configured to selectively engage with a rivet dispenser and introduce rivets to the rivet dispenser. The channel extends between the first port and the second port and is configured to transport rivets from the first port to the second port in a series arrangement and in a preselected orientation. The first gate is in communication with the second port and is selectively positionable between a first configuration inhibiting movement of rivets through the second port, and a second configuration enabling movement of rivets through the second port.

IPC Classes  ?

  • B21J 15/32 - Devices for inserting or holding rivets in position with or without feeding arrangements
  • B21J 15/02 - Riveting procedures
  • B23K 11/00 - Resistance welding; Severing by resistance heating
  • B23K 11/30 - Features relating to electrodes

33.

AERODYNAMIC WHEEL COVER MOUNTING DESIGN

      
Application Number 17263827
Status Pending
Filing Date 2019-05-28
First Publication Date 2021-09-23
Owner
  • HOWMET AEROSPACE INC. (USA)
  • HOWMET AEROSPACE INC. (USA)
Inventor
  • Wallace, Spencer
  • Brest, Matt

Abstract

A wheel cover assembly for a vehicle wheel may include a cover body having a cover body outer surface, a cover body inner surface, and a cover body outer edge having an outer diameter that is greater than an inner diameter of a stiffener rib extending inward from an inner surface of the wheel rim and less than an inner diameter of an open end flange of the wheel rim. The wheel cover assembly may further include a cover mounting mechanism operatively connected to the cover body and having a locking position wherein the cover mounting mechanism engages the stiffener rib when the cover body inner surface is facing and engaging the stiffener rib and a cover locking position wherein the cover mounting mechanism engages the stiffener rib to secure the wheel cover assembly to the vehicle wheel.

IPC Classes  ?

  • B60B 7/12 - Fastening arrangements therefor comprising an annular spring or gripping element mounted on the cover
  • B60B 7/06 - Fastening arrangements therefor

34.

Wheel flange

      
Application Number 29653944
Grant Number D0929299
Status In Force
Filing Date 2018-06-20
First Publication Date 2021-08-31
Grant Date 2021-08-31
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Belousov, Igor
  • Prasad, Santosh
  • Ciccola, Gabriele F.
  • Sklyut, Henry
  • Rovito, Anton J.
  • Degeorge, Grant
  • Fulton, Erin
  • Pacek, Michael A.

35.

VEHICLE WHEEL AND METHODS OF MAKING AND USING A VEHICLE WHEEL

      
Application Number 17267880
Status Pending
Filing Date 2018-10-26
First Publication Date 2021-06-17
Owner Howmet Aerospace Inc. (USA)
Inventor Mason, Douglas P.

Abstract

A vehicle wheel for mounting at least two tires, an assembly comprising the vehicle wheel, methods of making the vehicle wheel, and methods of using the vehicle wheel. The vehicle wheel comprises a generally cylindrical first region, a generally cylindrical second region, a third region, and a fourth region. The first region comprises a first tire mount disposed about a circumference of an outer surface of the first region. The second region comprises a second tire mount disposed about a circumference of an outer surface of the second region. The third region is disposed intermediate and connecting the first region and the second region. The fourth region is integral with and extends radially inward from an inner surface of the third region. The fourth region is configured to mount to a vehicle axle. The first, second, third, and fourth regions are regions of a monolithic body.

IPC Classes  ?

  • B60B 11/04 - Wheels with a rim capable of carrying more than one tyre
  • B60B 3/02 - Disc wheels, i.e. wheels with load-supporting disc body with a single disc body integral with rim

36.

FASTENER INCLUDING A TRANSITION ZONE AND METHOD OF USE THEREOF

      
Application Number 16967913
Status Pending
Filing Date 2018-05-21
First Publication Date 2021-01-28
Owner Howmet Aerospace Inc. (USA)
Inventor Arciniega, Oviedo

Abstract

A fastener and a method of fastening are provided. The fastener can comprise a first end, an oppositely disposed second end, and an elongate portion intermediate the first end and the second end. The elongate portion comprises a first region adjacent to the first end and a second region adjacent to the second end. The first region extends a distance along the elongate portion and has a first diameter. The second region extends a distance along the elongate portion and has a second diameter different from the first diameter. The fastener comprises a transition zone which extends a distance along the elongate portion and connects the first region and the second region. The transition zone comprises a radiused region and a taper region.

IPC Classes  ?

  • 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
  • F16B 19/05 - Bolts fastening by swaged-on collars

37.

Vehicle wheels, methods of making vehicle wheels, and dual wheel assemblies

      
Application Number 16801389
Grant Number 11738595
Status In Force
Filing Date 2020-02-26
First Publication Date 2020-11-26
Grant Date 2023-08-29
Owner HOWMET AEROSPACE INC. (USA)
Inventor Wallace, Spencer

Abstract

Vehicle wheels, methods of making vehicle wheels, and dual wheel assemblies are provided. The vehicle wheel includes a generally cylindrical first region and a second region extending radially inwardly from the first region. The second region includes a first surface, a second surface, an opening, and a hub surface. A distance from the first surface to the second surface defines a thickness. The opening is configured to receive at least a portion of a hub of the vehicle axle. The hub surface is adjacent to and surrounds the opening and extends from the first surface to the second surface. The hub surface includes a generally flat portion and a relief portion adjacent to at least one of the first surface and the second surface. The relief portion surrounds the opening and extends along the hub surface for a distance of at least 25% of the thickness.

IPC Classes  ?

  • B60B 3/00 - Disc wheels, i.e. wheels with load-supporting disc body
  • B60B 3/02 - Disc wheels, i.e. wheels with load-supporting disc body with a single disc body integral with rim

38.

Resistance spot rivet welding systems and methods of use thereof

      
Application Number 16768157
Grant Number 11684992
Status In Force
Filing Date 2018-12-13
First Publication Date 2020-11-19
Grant Date 2023-06-27
Owner
  • HOWMET AEROSPACE INC. (USA)
  • CENTERLINE (WINDSOR) LIMITED (Canada)
Inventor
  • Vanderzwet, Daniel Peter
  • Britton, Simon Maurice
  • Koscielski, Larry Frank
  • Michaud, Eric Jean
  • Simone, David Mario
  • Cosgrave, Stuart Cameron
  • Wasyliniuk, Kyle Alexander
  • Spinella, Donald J.
  • Iasella, Gino N.
  • Bergstrom, Daniel
  • Wilcox, Robert B.
  • Kingsbury, Thomas R.
  • Musgrove, Graham Scott

Abstract

Resistance spot rivet welding systems, subsystems, and methods of use thereof are provided.

IPC Classes  ?

39.

Aluminum alloys, and methods for producing the same

      
Application Number 16848656
Grant Number 11608551
Status In Force
Filing Date 2020-04-14
First Publication Date 2020-09-03
Grant Date 2023-03-21
Owner Howmet Aerospace Inc. (USA)
Inventor
  • Lin, Jen C.
  • Ciccola, Gabriele F.
  • Prasad, Santosh
  • Wen, Wei
  • Kilmer, Raymond J.

Abstract

New aluminum alloys are disclosed and generally include 0.6-1.4 wt. % Si, 0.25-0.90 wt. % Mg, wherein the ratio of wt. % Si to wt. % Mg is from 1.05:1 to 5.0:1, 0.25-2.0 wt. % Cu, 0.10-3.5 wt. % Zn, 0.01-1.0 wt. % Fe, up to 0.8 wt. % Mn, up to 0.25 wt. % Cr, up to 0.20 wt. % Zr, up to 0.20 wt. % V, and up to 0.15 wt. % Ti, wherein the total of Fe+Mn+Cr+Zr+V+Ti is not greater than 2.0 wt. %, the balance being aluminum and impurities. The new aluminum alloys may include Q phase precipitates. In some embodiments, the solvus temperature of the Q phase precipitates is not greater than 950° F.

IPC Classes  ?

  • C22F 1/057 - 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 of alloys with copper as the next major constituent
  • C22C 21/02 - Alloys based on aluminium with silicon as the next major constituent
  • C22C 21/10 - Alloys based on aluminium with zinc as the next major constituent
  • C22C 21/14 - Alloys based on aluminium with copper as the next major constituent with silicon
  • C22C 21/16 - Alloys based on aluminium with copper as the next major constituent with magnesium
  • C22C 21/18 - Alloys based on aluminium with copper as the next major constituent with zinc
  • C22F 1/043 - 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 of alloys with silicon as the next major constituent
  • C22F 1/053 - 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 of alloys with zinc as the next major constituent

40.

Wheel Having a Stiffening Rib

      
Application Number 16829054
Status Pending
Filing Date 2020-03-25
First Publication Date 2020-08-20
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Sklyut, Henry
  • Peer, Gregory L.
  • Ciccola, Gabriele F.
  • Prasad, Santosh
  • Fulton, Erin
  • Pacek, Michael A.
  • Burg, James T.
  • Degeorge, Grant
  • Rovito, Anton J.
  • Carraher, Courtney
  • Au, Christopher

Abstract

A wheel is provided including a disc face, an open end opposing the disc face, and a wheel rim extending between the disc face and the open end, the wheel rim including a rib extending radially inward from the rim and a rim section including the rib.

IPC Classes  ?

  • B60B 21/02 - Rims characterised by transverse section
  • B60B 3/02 - Disc wheels, i.e. wheels with load-supporting disc body with a single disc body integral with rim

41.

Titanium alloy products and methods of making the same

      
Application Number 16846800
Grant Number 11421303
Status In Force
Filing Date 2020-04-13
First Publication Date 2020-07-30
Grant Date 2022-08-23
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Sun, Fusheng
  • Crist, Jr., Ernest M.

Abstract

The present disclosure relates to new titanium alloys and methods for making the same. The new titanium alloys generally include 4.75-6.75 wt. % Al, 6.5-8.5 wt. % (Nb+Ta), 1.5-3.5 wt. % Sn, up to 5.0 wt. % Zr, and up to 2.5 wt. % Mo, the balance being titanium, optional incidental elements, and impurities. Due to their composition and methods of manufacture, the new titanium alloys may find use in several applications, such as aerospace and/or automotive applications.

IPC Classes  ?

  • C22C 14/00 - Alloys based on titanium
  • B33Y 70/00 - Materials specially adapted for additive manufacturing
  • C22F 1/18 - High-melting or refractory metals or alloys based thereon

42.

Wheel flange

      
Application Number 29631442
Grant Number D0889375
Status In Force
Filing Date 2017-12-29
First Publication Date 2020-07-07
Grant Date 2020-07-07
Owner Howmet Aerospace Inc. (USA)
Inventor
  • Prasad, Santosh
  • Burg, James T.
  • Ciccola, Gabriele F.
  • Degeorge, Grant
  • Pacek, Michael A.
  • Fulton, Erin
  • Rovito, Anton J.
  • Carraher, Courtney
  • Au, Christopher A.
  • Sklyut, Henry

43.

Wheel flange

      
Application Number 29631444
Grant Number D0889376
Status In Force
Filing Date 2017-12-29
First Publication Date 2020-07-07
Grant Date 2020-07-07
Owner Howmet Aerospace Inc. (USA)
Inventor
  • Prasad, Santosh
  • Burg, James T.
  • Ciccola, Gabriele F.
  • Pacek, Michael A.
  • Fulton, Erin
  • Rovito, Anton J.
  • Lee, Jason C
  • Globig, Michael A

44.

Single piece heavy duty wheel

      
Application Number 16801246
Grant Number 11345188
Status In Force
Filing Date 2020-02-26
First Publication Date 2020-06-18
Grant Date 2022-05-31
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Zehnder, Craig M.
  • Ciccola, Gabriele F.
  • Degeorge, Grant
  • Prasad, Santosh
  • Sklyut, Henry
  • Rovito, Anton
  • Tan, Christopher J.
  • Goodman, Jay H.

Abstract

A wheel rim including a flange profile on a tire side of an open end flange of the wheel rim, the flange profile defined by the equation: 1≤1, aTheta1 is between −1.004 to −0.974, aTheta2 is between −−1.049 to −1.0182, aTheta3 is between −3.601 to −2.760, aTheta4 is between 18.791 to 25.965, and aTheta5 is between 0.185 to 0.277.

IPC Classes  ?

  • B60B 21/10 - Rims characterised by the form of tyre-seat or flange, e.g. corrugated

45.

Collet assembly for fastener feeding apparatus

      
Application Number 16789466
Grant Number 11801567
Status In Force
Filing Date 2020-02-13
First Publication Date 2020-06-11
Grant Date 2023-10-31
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Wilcox, Robert
  • Kingsbury, Thomas
  • Vanderzwet, Dan Peter
  • Britton, Simon Maurice
  • Spinella, Donald J.
  • Bergstrom, Daniel
  • Michaud, Eric Jean
  • Koscielski, Larry Frank
  • Iasella, Gino Norman

Abstract

A collet assembly including an actuator and a collet connected to the actuator. The collet assembly is adapted to be installed on a welding electrode holder having an electrode. The collet is moveable by the actuator from an advanced position, in which the collet is adapted to grip a fastener such as a welding rivet, and a retracted position, in which at least a portion of the collet is retracted into the actuator to enable the electrode to engage the fastener for welding to a work piece, and the collet is adapted to release the fastener.

IPC Classes  ?

46.

Preload controlled stud lockbolt

      
Application Number 16776732
Grant Number 11473605
Status In Force
Filing Date 2020-01-30
First Publication Date 2020-05-28
Grant Date 2022-10-18
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Brennetot, Thomas
  • Brunet, Arnaud
  • Coulon, Christophe

Abstract

A fastener including a pin member having a shank portion, a threaded portion having a thread, a lock portion having at least one lock groove, and a pull portion located having at least one pull groove. The threaded portion is adapted to be engaged threadedly with a threaded hole of a workpiece to install the pin member therein. The fastener includes a swage collar adapted to be installed into the at least one lock groove of the lock portion to secure a plurality of workpieces. The pull portion is adapted to break off when the fastener is installed.

IPC Classes  ?

  • F16B 19/05 - Bolts fastening by swaged-on collars
  • F16B 23/00 - Specially-shaped heads of bolts or screws for rotations by a tool
  • F16B 39/02 - Locking of screws, bolts, or nuts in which the locking takes place after screwing down
  • 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
  • F16B 31/02 - Screwed connections specially modified in view of tensile load; Break-bolts for indicating or limiting tensile load

47.

Tabbed collar for use with lock bolt

      
Application Number 16734633
Grant Number 11767871
Status In Force
Filing Date 2020-01-06
First Publication Date 2020-05-07
Grant Date 2023-09-26
Owner HOWMET AEROSPACE INC. (USA)
Inventor Wojciechowski, Stanley E.

Abstract

A lockbolt collar having a shank including a first end, a second end opposite the first end, a through-bore extending from the first end to the second end, an inner wall extending from the first end to the second end, and a tab extending radially and outwardly from the inner wall, the tab including a top surface having an arcuate shape, the arcuate shape of the tab being sized and shaped to mate with at least one lock groove of a threaded portion of a pin member.

IPC Classes  ?

  • F16B 19/05 - Bolts fastening by swaged-on collars
  • 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

48.

Wheel cover assembly with installable wheel rib and wheel cover

      
Application Number 16563526
Grant Number 11529826
Status In Force
Filing Date 2019-09-06
First Publication Date 2020-03-12
Grant Date 2022-12-20
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Wallace, Spencer
  • Brest, Matt

Abstract

A wheel cover assembly for a vehicle wheel may include a wheel rib that is attachable to a rim inner surface of a wheel rim of the vehicle wheel, a cover body having a cover body outer surface, a cover body inner surface, and a cover body outer edge having an outer diameter that is greater than an inner diameter of the wheel rib and less than an inner diameter of an open end flange of the wheel rim. A cover mounting mechanism operatively connected to the cover body has a cover locking position wherein the cover mounting mechanism engages the wheel rib to retain the wheel rib between the cover mounting mechanism and the cover body and secure the wheel cover assembly to the vehicle wheel when the wheel rib is attached to the rim inner surface.

IPC Classes  ?

  • B60B 7/08 - Fastening arrangements therefor having gripping elements consisting of formations integral with the cover
  • B60B 7/06 - Fastening arrangements therefor
  • B60B 21/02 - Rims characterised by transverse section

49.

Advanced nut and bolt

      
Application Number 16407439
Grant Number 11519452
Status In Force
Filing Date 2019-05-09
First Publication Date 2019-08-29
Grant Date 2022-12-06
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Busby, Donald C.
  • Franklin, Richard
  • Wollard, James L.

Abstract

A fastener including a bolt having an elongated shank having a first end, a second end opposite the first end, and a threaded portion having an external bolt thread, the bolt thread including a bolt pitch. The fastener includes a nut having a first end, a second end opposite the first end of the nut, and an internal nut thread extending between the first and second ends of the nut and adapted to engage threadedly the bolt thread of the bolt. The nut thread includes a nut pitch and a hardness that changes gradationally between the first and second ends of the nut. The bolt pitch of the bolt thread of the bolt is mismatched with the nut pitch of the nut thread of the nut.

IPC Classes  ?

  • F16B 39/30 - Locking exclusively by special shape of the screw-thread
  • F16B 39/34 - Locking by deformable inserts or like parts

50.

Resistance Welding Fastener, Apparatus and Methods

      
Application Number 16369117
Status Pending
Filing Date 2019-03-29
First Publication Date 2019-07-25
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Spinella, Donald J.
  • Bergstrom, Daniel

Abstract

An apparatus and method for fastening dissimilar metals like steel and aluminum utilizes a steel rivet and a spot welding machine. The rivet and metals are stacked and the heat from the welder's electric current softens the lower melting point aluminum allowing the rivet to penetrate the aluminum and weld to the steel layer. The fastener may be used to join stacks with several layers of different materials and may be used to apply a threaded socket or stud made from steel or titanium to an aluminum or magnesium alloy structure. Layers of non-conductive materials like plastic and ceramics may also be affixed to a conductive layer using the fastener made from a compatible material that extends through a pilot hole.

IPC Classes  ?

  • B23K 11/00 - Resistance welding; Severing by resistance heating
  • B21D 39/02 - Application of procedures in order to connect objects or parts, e.g. coating with sheet metal otherwise than by plating; Tube expanders of sheet metal by folding, e.g. connecting edges of a sheet to form a cylinder
  • F16B 37/06 - Devices for fastening nuts to surfaces, e.g. sheets, plates by means of welding or riveting
  • F16B 5/08 - Joining sheets or plates to one another or to strips or bars parallel to them by means of welds or the like
  • B23K 35/28 - Selection of soldering or welding materials proper with the principal constituent melting at less than 950°C
  • B23K 11/18 - Resistance welding; Severing by resistance heating taking account of the properties of the material to be welded of non-ferrous metals
  • B23K 35/02 - Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape

51.

Wheel flange

      
Application Number 29631254
Grant Number D0853927
Status In Force
Filing Date 2017-12-28
First Publication Date 2019-07-16
Grant Date 2019-07-16
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Sklyut, Henry
  • Peer, Gregory L.
  • Ciccola, Gabriele
  • Degeorge, Grant

52.

Advanced nut and bolt

      
Application Number 16298843
Grant Number 10655669
Status In Force
Filing Date 2019-03-11
First Publication Date 2019-07-04
Grant Date 2020-05-19
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Busby, Donald C.
  • Franklin, Richard
  • Wollard, James L.

Abstract

A fastener including a bolt having an elongated shank having a first end, a second end opposite the first end, and a threaded portion having an external bolt thread, the bolt thread including a bolt pitch. The fastener includes a nut having a first end, a second end opposite the first end of the nut, and an internal nut thread extending between the first and second ends of the nut and adapted to engage threadedly the bolt thread of the bolt. The nut thread includes a nut pitch and a hardness that changes gradationally between the first and second ends of the nut. The bolt pitch of the bolt thread of the bolt is mismatched with the nut pitch of the nut thread of the nut.

IPC Classes  ?

  • F16B 37/00 - Nuts or like thread-engaging members
  • F16B 39/30 - Locking exclusively by special shape of the screw-thread
  • F16B 35/00 - Screw-bolts; Stay bolts; Screw-threaded studs; Screws; Set screws

53.

Fastener locking members

      
Application Number 16268788
Grant Number 10683887
Status In Force
Filing Date 2019-02-06
First Publication Date 2019-06-06
Grant Date 2020-06-16
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Rizza, Gregory
  • Haylock, Luke
  • Pinheiro, Rodrigo

Abstract

A locking member for a fastener, such as a nut or a collar, includes a shank portion and a flanged portion, a bore extending the shank portion and the flanged portion and including a first interior portion located within the shank portion and a containment cavity located within the flanged portion, and an inner wall defining the containment cavity. The containment cavity includes an inner diameter that is greater than an inner diameter of the first interior portion of the bore. The inner wall of the containment cavity includes one or a combination of flat/linear surfaces, concave surfaces, and convex surfaces.

IPC Classes  ?

  • F16B 37/00 - Nuts or like thread-engaging members
  • F16B 39/282 - Locking by means of special shape of work-engaging surfaces, e.g. notched or toothed nuts
  • F16B 5/01 - Joining sheets or plates to one another or to strips or bars parallel to them by means of fastening elements specially adapted for honeycomb panels
  • F16B 19/05 - Bolts fastening by swaged-on collars
  • B64D 45/02 - Lightning protectors; Static dischargers
  • F16B 4/00 - Shrinkage connection, e.g. assembled with the parts at different temperature; Force fits; Non-releasable friction-grip fastenings

54.

RESISTANCE WELDING FASTENER, APPARATUS AND METHODS FOR JOINING SIMILAR AND DISSIMILAR MATERIALS

      
Application Number 16210680
Status Pending
Filing Date 2018-12-05
First Publication Date 2019-05-09
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Spinella, Donald J.
  • Bergstrom, Daniel

Abstract

An apparatus and method for fastening layers of non-ferrous alloys, like aluminum, magnesium and copper utilizes a steel fastener and a spot welding machine. The fastener and metals are stacked and the heat from the welder's electric current softens the lower melting point aluminum allowing the fastener to penetrate the aluminum. A weld zone between the fastener and the various layers creates an internal weld. The fastener has a rough shaft that is coated by the molten weld zone and is hard to withdraw on solidification. Layers of non-conductive materials like plastics and ceramics may also be affixed to a conductive layer using a fastener made from a compatible material that extends through a pilot hole and welds to or penetrates a conductive layer. The fastener may have projections that initially reduce contact area with the stack.

IPC Classes  ?

  • B23K 11/30 - Features relating to electrodes
  • F16B 5/08 - Joining sheets or plates to one another or to strips or bars parallel to them by means of welds or the like
  • B23K 11/00 - Resistance welding; Severing by resistance heating
  • B23K 11/18 - Resistance welding; Severing by resistance heating taking account of the properties of the material to be welded of non-ferrous metals
  • B23K 11/20 - Resistance welding; Severing by resistance heating taking account of the properties of the material to be welded of different metals
  • B23K 35/02 - Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape

55.

Resistance welding fastener, apparatus and methods

      
Application Number 16210599
Grant Number 11196185
Status In Force
Filing Date 2018-12-05
First Publication Date 2019-04-11
Grant Date 2021-12-07
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Spinella, Donald J.
  • Bergstrom, Daniel

Abstract

An apparatus and method for fastening dissimilar materials like steel, plastic and aluminum. A resistance welding fastener having multiple layers may be used with or without a sealant. The fastener may be used to form an aluminum covered steel laminate via a hemming pattern of attachment. The fastener may have a solid shaft or have an extended reach and have features for interacting with the welding electrode. A variety of electrode tips may be employed to cooperate with the fastener.

IPC Classes  ?

  • B23K 11/11 - Spot welding
  • H01R 4/02 - Soldered or welded connections
  • B23K 11/20 - Resistance welding; Severing by resistance heating taking account of the properties of the material to be welded of different metals
  • B23K 35/02 - Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape
  • H01R 43/02 - Apparatus or processes specially adapted for manufacturing, assembling, maintaining, or repairing of line connectors or current collectors or for joining electric conductors for soldered or welded connections
  • F16B 37/06 - Devices for fastening nuts to surfaces, e.g. sheets, plates by means of welding or riveting
  • H01R 4/62 - Connections between conductors of different materials; Connections between or with aluminium or steel-core aluminium conductors
  • B23K 103/20 - Ferrous alloys and aluminium or alloys thereof
  • F16B 5/08 - Joining sheets or plates to one another or to strips or bars parallel to them by means of welds or the like

56.

Ribbed wheel

      
Application Number 29631467
Grant Number D0836522
Status In Force
Filing Date 2017-12-29
First Publication Date 2018-12-25
Grant Date 2018-12-25
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Prasad, Santosh
  • Sklyut, Henry
  • Ciccola, Gabriele F.
  • Degeorge, Grant
  • Fulton, Erin
  • Pacek, Michael A.
  • Burg, James T.
  • Rovito, Anton J.
  • Carraher, Courtney
  • Au, Christopher

57.

Ribbed wheel

      
Application Number 29631449
Grant Number D0836056
Status In Force
Filing Date 2017-12-29
First Publication Date 2018-12-18
Grant Date 2018-12-18
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Prasad, Santosh
  • Skylut, Henry
  • Ciccola, Gabriele F.
  • Degeorge, Grant
  • Fulton, Erin
  • Pacek, Michael A.
  • Burg, James T.
  • Rovito, Anton J.
  • Carraher, Courtney
  • Au, Christopher

58.

Ribbed wheel

      
Application Number 29631455
Grant Number D0836057
Status In Force
Filing Date 2017-12-29
First Publication Date 2018-12-18
Grant Date 2018-12-18
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Prasad, Santosh
  • Sklyut, Henry
  • Ciccola, Gabriele F.
  • Degeorge, Grant
  • Fulton, Erin
  • Pacek, Michael A.
  • Burg, James T.
  • Rovito, Anton J.
  • Carraher, Courtney
  • Au, Christopher

59.

Single piece heavy duty wheel

      
Application Number 29572286
Grant Number D0834482
Status In Force
Filing Date 2016-07-26
First Publication Date 2018-11-27
Grant Date 2018-11-27
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Zehnder, Craig
  • Ciccola, Gabriele F.
  • Degeorge, Grant
  • Prasad, Santosh
  • Sklyut, Henry
  • Rovito, Anton J.
  • Tan, Christopher J.

60.

Wheel

      
Application Number 29621979
Grant Number D0830929
Status In Force
Filing Date 2017-10-12
First Publication Date 2018-10-16
Grant Date 2018-10-16
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Sklyut, Henry
  • Peer, Gregory L.
  • Ciccola, Gabriele
  • Degeorge, Grant

61.

Blind fasteners

      
Application Number 16002679
Grant Number 10704582
Status In Force
Filing Date 2018-06-07
First Publication Date 2018-10-04
Grant Date 2020-07-07
Owner Howmet Aerospace Inc. (USA)
Inventor
  • Hufnagl, Gerhart
  • Desalvo, Douglas
  • Torrence, Randy

Abstract

A fastener includes a sleeve, a core bolt, and an insert. The sleeve includes a first portion having a first inner diameter, a second portion having a second inner diameter, and a step intermediate the first and second portions. The core bolt includes a cylindrical portion having a first diameter, a threaded portion having a major diameter, and a thread run-out intermediate the cylindrical and threaded portions. The insert is disposed within the sleeve and is sized and shaped to be retained between the step of the sleeve and the thread run-out of the core bolt when the fastener is in a pre-installation position. The fastener compresses the insert between the step of the sleeve and the thread run-out of the core bolt by an installation motion of the core bolt. The insert deforms away from the core bolt to initiate formation of a bulb in response to the compression.

IPC Classes  ?

  • F16B 13/06 - Dowels or other devices fastened in walls or the like by inserting them in holes made therein for that purpose with parts gripping in the hole or behind the reverse side of the wall after inserting from the front combined with expanding sleeve
  • F16B 5/04 - Joining sheets or plates to one another or to strips or bars parallel to them by means of riveting
  • F16B 19/10 - Hollow rivets; Multi-part rivets fastened by expanding mechanically
  • 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

62.

Asymmetric fastener recess and key

      
Application Number 15972455
Grant Number 10907677
Status In Force
Filing Date 2018-05-07
First Publication Date 2018-09-06
Grant Date 2021-02-02
Owner Howmet Aerospace Inc. (USA)
Inventor
  • Pinheiro, Rodrigo
  • Haylock, Luke

Abstract

A fastening system including a pin member and a key for engaging the pin member. The pin member includes a shank portion and a recess formed within an end face of the shank portion. The recess includes a plurality of splines and recesses that form first and second bearing surfaces oriented at angles. The key includes a key head having a plurality of splines and grooves that form first and second bearing surfaces oriented at angles. The plurality of splines and recesses of the pin member and the plurality of splines and recesses of the key are adapted to communicate with each other when tightening and loosening the pin member.

IPC Classes  ?

  • F16B 23/00 - Specially-shaped heads of bolts or screws for rotations by a tool
  • 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

63.

Titanium alloy having good oxidation resistance and high strength at elevated temperatures

      
Application Number 15903545
Grant Number 11041402
Status In Force
Filing Date 2018-02-23
First Publication Date 2018-08-30
Grant Date 2021-06-22
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Sun, Fusheng
  • Crist, Ernest M.
  • Yu, Kuang-O

Abstract

A titanium alloy may be characterized by a good oxidation resistance, high strength and creep resistance at elevated temperatures up to 750° C., and good cold/hot forming ability, good superplastic forming performance, and good weldability. The alloy may contain, in weight percent, aluminum 4.5 to 7.5, tin 2.0 to 8.0, niobium 1.5 to 6.5, molybdenum 0.1 to 2.5, silicon 0.1 to 0.6, oxygen up to 0.20, carbon up to 0.10, and balance titanium with incidental impurities.

IPC Classes  ?

  • C22C 14/00 - Alloys based on titanium
  • F01D 25/00 - Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
  • C22C 1/02 - Making non-ferrous alloys by melting
  • C22F 1/18 - High-melting or refractory metals or alloys based thereon
  • F01D 5/28 - Selecting particular materials; Measures against erosion or corrosion

64.

Reduced electromagnetic signature of conforming conical seal fastener systems

      
Application Number 15836296
Grant Number 10457414
Status In Force
Filing Date 2017-12-08
First Publication Date 2018-06-14
Grant Date 2019-10-29
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Liebscher, Andreas
  • Prachumsri, Wudhidham
  • Lea, Curtis
  • Haylock, Luke

Abstract

A fastener including a sleeve having an elongated portion, a head with a bearing surface, and an internal threaded portion, a core bolt disposed within the sleeve and having a head and a shank portion having an external threaded portion engageable threadedly with the threaded portion of the sleeve. An insert is disposed within the sleeve and surrounds a portion of the core bolt. A seal element is attached to the sleeve and juxtaposed with the bearing surface of the head of the sleeve. The fastener is adapted to be installed in a structure. The electrical contact of the fastener reduces the potential difference between it and the structure, which provides a direct path for continuous propagation of electromagnetic waves, reducing electromagnetic wave scattering and minimizing the electromagnetic signature.

IPC Classes  ?

  • F16B 5/06 - Joining sheets or plates to one another or to strips or bars parallel to them by means of clamps or clips
  • B64D 45/02 - Lightning protectors; Static dischargers
  • F16B 43/00 - Washers or equivalent devices; Other devices for supporting bolt-heads or nuts
  • F16B 35/06 - Specially-shaped heads
  • F16B 33/00 - Features common to bolt and nut
  • F16B 1/00 - Devices for securing together, or preventing relative movement between, constructional elements or machine parts
  • B64C 1/00 - Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like

65.

Fastener and fastening system

      
Application Number 15785526
Grant Number 10710146
Status In Force
Filing Date 2017-10-17
First Publication Date 2018-04-26
Grant Date 2020-07-14
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Corbett, Robert J.
  • Leavelle, Joseph Z.

Abstract

A fastening system includes a fastener having a bolt with a pull portion having at least one pull groove, and an outer sleeve having a head with an inner face, the bolt being inserted within the sleeve. The fastening system includes a fastener installation tool having a puller with at least one tooth and a front face. The inner face of the head of the sleeve is angled at an included angle measured transverse to a longitudinal axis of the fastener, while the front face of the puller of the fastener installation tool is angled at an included angle measured transverse to a longitudinal axis of the puller. The included angles are chosen to match or be substantially the same. The front face of the puller of the fastener installation tool is adapted to engage the inner face of the outer sleeve of the fastener when the fastener installation tool engages the fastener, and the inner face of the outer sleeve facilitates the receipt of the front face of the puller and the alignment of the at least one tooth of the puller with the at least one pull groove of the bolt by allowing the puller to shift forward or backward to facilitate such alignment.

IPC Classes  ?

  • 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
  • B21J 15/04 - Riveting hollow rivets mechanically
  • B21J 15/02 - Riveting procedures
  • F16B 19/10 - Hollow rivets; Multi-part rivets fastened by expanding mechanically

66.

Wheel

      
Application Number 29541115
Grant Number D0810645
Status In Force
Filing Date 2015-09-30
First Publication Date 2018-02-20
Grant Date 2018-02-20
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Sklyut, Henry
  • Peer, Gregory L.
  • Ciccola, Gabriele
  • Degeorge, Grant

67.

Rotary latch system

      
Application Number 15620283
Grant Number 10676971
Status In Force
Filing Date 2017-06-12
First Publication Date 2017-12-14
Grant Date 2020-06-09
Owner HOWMET AEROSPACE INC. (USA)
Inventor Do, Thai

Abstract

A latch includes a base having a bore extending therethrough defining an axis, a plunger positioned within the bore and rotatable about the axis, a drive shaft positioned adjacent the base and engaged with the plunger such that rotation of the plunger about the axis causes corresponding rotation of the drive shaft about the axis, a bracket positioned adjacent the base and the drive shaft and engaged with the drive shaft such that rotation of the drive shaft about the axis causes movement of the bracket, and a closure element coupled to the bracket such that movement of the bracket causes the closure element to move between a position wherein the closure element allows a structure to move with respect to an adjacent structure and a position in which the closure element prevents the structure from moving with respect to the adjacent structure.

IPC Classes  ?

  • E05C 3/12 - Fastening devices with bolts moving pivotally or rotatively with latching action
  • E05B 35/00 - Locks for use with special keys or a plurality of keys
  • E05B 17/20 - Means independent of the locking mechanism for preventing unauthorised opening, e.g. for securing the bolt in the fastening position
  • E05B 15/00 - Other details of locks; Parts for engagement by bolts of fastening devices
  • B64D 29/06 - Attaching of nacelles, fairings, or cowlings
  • E05B 41/00 - Locks with visible indication as to whether the lock is locked or unlocked
  • E05C 3/10 - Fastening devices with bolts moving pivotally or rotatively without latching action with operating handle or equivalent member moving otherwise than rigidly with the bolt the handle or member moving essentially in a plane substantially parallel to the wing
  • E05B 63/00 - Locks with special structural characteristics

68.

Resistance welding fasteners, apparatus and methods for joining dissimilar materials and assessing joints made thereby

      
Application Number 15469161
Grant Number 10593034
Status In Force
Filing Date 2017-03-24
First Publication Date 2017-11-02
Grant Date 2020-03-17
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Spinella, Donald J.
  • Bergstrom, Daniel
  • Wojciechowski, Stanley E.
  • Wilcox, Robert
  • Williams, Justin K.

Abstract

An apparatus and method for method for joining materials includes a rivet that may extend through a first sheet to be resistance welded to a second sheet. The head of the rivet has a cavity and vents allowing adhesive extruded from a pilot hole to be received in the cavity and vented in a direction parallel to the first sheet. The rivet is deformed to an hourglass shape that fills the pilot hole and displaces the first sheet into the cavity. Rivet dimension allow for holding with a robotic gripper that can be withdrawn before welding. Methods of monitoring joint quality include comparing welding parameter profiles and images of good and discrepant joints.

IPC Classes  ?

  • B21J 15/02 - Riveting procedures
  • B23K 11/20 - Resistance welding; Severing by resistance heating taking account of the properties of the material to be welded of different metals
  • G06T 7/00 - Image analysis
  • B21J 15/28 - Control devices specially adapted to riveting machines not restricted to one of the preceding subgroups
  • B21J 15/32 - Devices for inserting or holding rivets in position with or without feeding arrangements
  • G01B 11/24 - Measuring arrangements characterised by the use of optical techniques for measuring contours or curvatures
  • B23K 11/00 - Resistance welding; Severing by resistance heating
  • B23K 103/04 - Steel alloys
  • B23K 103/00 - Materials to be soldered, welded or cut
  • B23K 103/18 - Dissimilar materials
  • B23K 103/08 - Non-ferrous metals or alloys
  • B23K 103/20 - Ferrous alloys and aluminium or alloys thereof
  • B23K 103/16 - Composite materials

69.

Lockbolt fastening system

      
Application Number 15478785
Grant Number 10260547
Status In Force
Filing Date 2017-04-04
First Publication Date 2017-10-05
Grant Date 2019-04-16
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Smith, James T.
  • Corbett, Robert J.

Abstract

A swage collar includes a shank, a flange, and a through bore. The shank includes a first end, a second end opposite the first end, an outside diameter, and an overall length between the first end and the second end. The flange extends from the first end of the shank. The through bore extends longitudinally through the shank from the first end of the shank to the second end of the shank. The through bore defines an inside diameter. The inside diameter and the outside diameter together define a wall thickness of the shank. The wall thickness of the shank is in a range of about 0.1 times the overall length of the shank to about 0.16 times the overall length of the shank.

IPC Classes  ?

  • F16B 19/05 - Bolts fastening by swaged-on collars
  • B21J 15/02 - Riveting procedures
  • F16B 5/04 - Joining sheets or plates to one another or to strips or bars parallel to them by means of riveting

70.

Fasteners with conforming sleeves

      
Application Number 15412906
Grant Number 10451099
Status In Force
Filing Date 2017-01-23
First Publication Date 2017-07-27
Grant Date 2019-10-22
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Haylock, Luke
  • Mulazimoglu, Hasim
  • Zeng, Liang

Abstract

A sleeve interference fastener including a conformable sleeve, wherein the conformable sleeve is comprised of at least one first material having a hardness of X, and a pin member, wherein the pin member is comprised of at least one second material having a hardness of Y, wherein X is sufficiently less than Y so that, in an installed position of an interference fit, at least a portion of the at least one first material of the conformable sleeve conforms to a contour of an inner surface of a hole of a composite structure so as to create a continuous electrical contact at an interface between the inner surface of the hole of the composite structure and the conformable sleeve.

IPC Classes  ?

  • F16B 19/02 - Bolts or sleeves for positioning of machine parts, e.g. notched taper pins, fitting pins, sleeves, eccentric positioning rings
  • F16B 4/00 - Shrinkage connection, e.g. assembled with the parts at different temperature; Force fits; Non-releasable friction-grip fastenings
  • 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
  • B64D 45/02 - Lightning protectors; Static dischargers
  • F16B 1/00 - Devices for securing together, or preventing relative movement between, constructional elements or machine parts

71.

Methods for producing forged products and other worked products

      
Application Number 15406306
Grant Number 11554443
Status In Force
Filing Date 2017-01-13
First Publication Date 2017-07-20
Grant Date 2023-01-17
Owner Howmet Aerospace Inc. (USA)
Inventor
  • Satoh, Gen
  • Myers, Daniel M.
  • Bodily, Brandon H.

Abstract

The present disclosure is directed towards different embodiments of additively manufacturing and smoothing an AM preform to configure an AM preform for downstream processing (working, forging, and the like).

IPC Classes  ?

  • B23K 26/00 - Working by laser beam, e.g. welding, cutting or boring
  • B23K 15/00 - Electron-beam welding or cutting
  • B23K 15/08 - Removing material, e.g. by cutting, by hole drilling
  • B23K 26/352 - Working by laser beam, e.g. welding, cutting or boring for surface treatment
  • B21J 5/00 - Methods for forging, hammering, or pressing; Special equipment or accessories therefor
  • B23K 26/361 - Removing material for deburring or mechanical trimming
  • B33Y 10/00 - Processes of additive manufacturing
  • B23K 26/342 - Build-up welding
  • B23K 26/354 - Working by laser beam, e.g. welding, cutting or boring for surface treatment by melting
  • B23K 26/36 - Removing material
  • B23K 103/14 - Titanium or alloys thereof

72.

Blind fastener

      
Application Number 15353126
Grant Number 10215210
Status In Force
Filing Date 2016-11-16
First Publication Date 2017-05-18
Grant Date 2019-02-26
Owner HOWMET AEROSPACE INC. (USA)
Inventor Busby, Donald C.

Abstract

A fastener including a bolt having a head, a shank portion, and an annular groove located intermediate the head and the shank portion, and a sleeve having a head, a shank portion, an inner cavity, a recess located in the head of the sleeve, and an annular tab located at a bottom of the recess and proximate to the shank portion of the sleeve. The sleeve receives the bolt such that the shank portion of the bolt is positioned within the inner cavity of the sleeve and the head of the bolt is positioned within the recess of the head of the sleeve. When the bolt is in an installed position within the sleeve, the annular tab of the sleeve is deformed and engages the annular groove of the bolt.

IPC Classes  ?

  • F16B 13/06 - Dowels or other devices fastened in walls or the like by inserting them in holes made therein for that purpose with parts gripping in the hole or behind the reverse side of the wall after inserting from the front combined with expanding sleeve
  • F16B 19/10 - Hollow rivets; Multi-part rivets fastened by expanding mechanically
  • F16B 39/22 - Locking of screws, bolts, or nuts in which the locking takes place during screwing down or tightening
  • F16B 29/00 - Screwed connection with deformation of nut or auxiliary member while fastening

73.

Pressure relief latch

      
Application Number 15337232
Grant Number 10378256
Status In Force
Filing Date 2016-10-28
First Publication Date 2017-05-04
Grant Date 2019-08-13
Owner HOWMET AEROSPACE INC. (USA)
Inventor Do, Thai

Abstract

A latch having a housing and a latch mechanism located within an interior portion of the housing. The latch mechanism includes an arm, a pair of socket screws, a pair of torsion springs, each of which is connected rotatably to the arm and engages a corresponding one of the pair of socket screws, a bolt mechanism attached rotatably to the housing, and a link attached pivotally to the arm and attached to the bolt mechanism. The socket screws are utilized to adjust loads on the springs. The bolt mechanism is movable between a first position, in which the arm and the link are toggled with one another under the loads of the springs and the bolt mechanism is adapted to engage an external structure, and a second position, in which the link and the arm are untoggled with one another and the bolt mechanism is disengaged with the external structure.

IPC Classes  ?

  • E05C 19/02 - Automatic catches, i.e. released by pull or pressure on the wing
  • B64D 29/08 - Inspection panels for power plants
  • B64D 29/00 - Power-plant nacelles, fairings, or cowlings
  • E05B 15/04 - Spring arrangements in locks
  • E05B 51/02 - Operating or controlling locks or other fastening devices by other non-mechanical means by pneumatic or hydraulic means
  • E05B 63/00 - Locks with special structural characteristics
  • E05B 85/02 - Lock casings

74.

Pressure relief door

      
Application Number 15278370
Grant Number 10240389
Status In Force
Filing Date 2016-09-28
First Publication Date 2017-03-30
Grant Date 2019-03-26
Owner HOWMET AEROSPACE INC. (USA)
Inventor Do, Thai

Abstract

A pressure relief door having a panel with an exterior side and an interior side, a pair of pressure relief latches mounted to the interior side of the panel, and a pair of hinges mounted to the panel and each including a lock mechanism mounted thereto. Each of the lock mechanisms includes a mounting bracket. The door is adapted to be installed within a structure and moveable between a closed position, such that the exterior side of the panel is substantially flush with an exterior surface of the structure, the lock mechanisms are engaged with an interior surface of the structure, and the pressure relief latches are engaged with the interior surface of the structure, and an open position, such that the pressure relief latches are disengaged with the interior surface of the structure, while the lock mechanisms remain engaged with the interior surface of the structure.

IPC Classes  ?

  • B64C 1/14 - Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens
  • E06B 5/12 - Doors, windows, or like closures for special purposes; Border constructions therefor for other protective purposes against air pressure, explosion, or gas
  • E05C 19/02 - Automatic catches, i.e. released by pull or pressure on the wing
  • E05D 11/10 - Devices for preventing movement between relatively-movable hinge parts

75.

Rivet feeding apparatus

      
Application Number 15266331
Grant Number 10507514
Status In Force
Filing Date 2016-09-15
First Publication Date 2017-03-16
Grant Date 2019-12-17
Owner HOWMET AEROSPACE INC. (USA)
Inventor Wilcox, Robert

Abstract

A fastener feed apparatus includes a mounting portion and a feed portion attached movably thereto. The feed portion includes a feed body having first and second ends and an internal track extending therethrough. The internal track is sized and shaped to convey a fastener through the feed body. The feed portion also includes a feeding block attached to the second end of the feed body and including a body and a pair of feed fingers, each of which includes a first end attached to the body and a second end. A track is formed between the feed fingers, is sized and shaped to convey the fastener from its first end to its second end, and is contiguous with the internal track of the feed body. The second end of the track includes a retention point. The feed fingers are sized and shaped to retain the fastener at the retention point.

IPC Classes  ?

  • B21J 15/32 - Devices for inserting or holding rivets in position with or without feeding arrangements
  • B23K 11/00 - Resistance welding; Severing by resistance heating
  • B23P 19/00 - Machines for simply fitting together or separating metal parts or objects, or metal and non-metal parts, whether or not involving some deformation; Tools or devices therefor so far as not provided for in other classes
  • B23K 11/11 - Spot welding
  • B23K 11/36 - Auxiliary equipment
  • B23K 103/04 - Steel alloys
  • B23K 103/10 - Aluminium or alloys thereof
  • B23K 103/16 - Composite materials

76.

Fastener locking members

      
Application Number 15239206
Grant Number 10215218
Status In Force
Filing Date 2016-08-17
First Publication Date 2017-03-02
Grant Date 2019-02-26
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Rizza, Gregory
  • Haylock, Luke
  • Pinheiro, Rodrigo
  • Mulazimoglu, Hasim
  • Liebscher, Andreas
  • Kamal, Manish

Abstract

A locking member for a fastener, such as a nut or a collar, includes a shank portion and a flanged portion, a bore extending the shank portion and the flanged portion and including a first interior portion located within the shank portion and a containment cavity located within the flanged portion, and an inner wall defining the containment cavity. The containment cavity includes an inner diameter that is greater than an inner diameter of the first interior portion of the bore. The inner wall of the containment cavity includes one or a combination of flat/linear surfaces, concave surfaces, and convex surfaces.

IPC Classes  ?

  • F16B 37/00 - Nuts or like thread-engaging members
  • F16B 39/282 - Locking by means of special shape of work-engaging surfaces, e.g. notched or toothed nuts
  • F16B 5/01 - Joining sheets or plates to one another or to strips or bars parallel to them by means of fastening elements specially adapted for honeycomb panels
  • B64D 45/02 - Lightning protectors; Static dischargers
  • F16B 4/00 - Shrinkage connection, e.g. assembled with the parts at different temperature; Force fits; Non-releasable friction-grip fastenings

77.

Adjustable pressure relief latch

      
Application Number 15245332
Grant Number 10435929
Status In Force
Filing Date 2016-08-24
First Publication Date 2017-03-02
Grant Date 2019-10-08
Owner HOWMET AEROSPACE INC. (USA)
Inventor Do, Thai

Abstract

A latch including a housing having side members each having an elongated slot, a bolt mounted rotatably to the housing and positioned between the side members of the housing, an adjustment mechanism, and a pin and roller positioned slidably within the elongated slots of the side members of the housing. The adjustment mechanism includes a compression spring, a central cap for receiving the pin and roller therethrough, and a nut for adjusting the load on the compression spring. The bolt is moveable between a first, closed position, in which the pin and roller are engaged with the bolt, and a second open position, in which the pin and roller are disengaged from the bolt. The latch can be opened automatically when a defined load, as adjusted by the adjustment mechanism, is provided on the bolt to disengage the pin and roller from the bolt.

IPC Classes  ?

  • E05C 19/04 - Ball or roller catches
  • E05B 15/04 - Spring arrangements in locks
  • E05B 51/02 - Operating or controlling locks or other fastening devices by other non-mechanical means by pneumatic or hydraulic means
  • B64D 29/06 - Attaching of nacelles, fairings, or cowlings
  • E05B 63/00 - Locks with special structural characteristics
  • E05C 19/06 - Other devices specially designed for securing wings in which the securing part is formed or carried by a spring and moves only by distortion of the spring, e.g. snaps

78.

Adjustable hook latch

      
Application Number 15251535
Grant Number 10760304
Status In Force
Filing Date 2016-08-30
First Publication Date 2017-03-02
Grant Date 2020-09-01
Owner Howmet Aerospace Inc. (USA)
Inventor Do, Thai

Abstract

A latch including a housing having a cylinder, a compression spring positioned within the cylinder, and a ball positioned at one end of the compression spring, a hook positioned slidably within the housing, and a star wheel positioned around the hook and having a plurality of holes formed therein. The ball under load from the spring aligns with and engages one of the holes of the star wheel to retain it in place. The star wheel is moveable rotatably such that the ball disengages the one of the holes of the star wheel to enable the hook to move axially and be adjusted relative to the housing, and the ball is adapted to engage another of the holes of the star wheel to retain the star wheel and prevent inadvertent rotation.

IPC Classes  ?

  • E05B 63/06 - Locks with special structural characteristics with lengthwise-adjustable bolts
  • E05C 19/10 - Hook fastenings; Fastenings in which a link engages a fixed hook-like member
  • E05C 19/14 - Hook fastenings; Fastenings in which a link engages a fixed hook-like member pivotally mounted with toggle action

79.

Pressure relief latch

      
Application Number 15224026
Grant Number 10604977
Status In Force
Filing Date 2016-07-29
First Publication Date 2017-02-09
Grant Date 2020-03-31
Owner HOWMET AEROSPACE INC. (USA)
Inventor Do, Thai

Abstract

A latch including a housing having side members each having an elongated slot, a bolt mounted rotatably to the housing and positioned between the side members of the housing, a trigger mounted rotatably to the housing, and a pin and roller positioned slidably within the elongated slots of the side members of the housing. The bolt is moveable between a first, closed position and a second open position. The trigger is moveable between a first position, in which the pin and roller are engaged with the bolt when the bolt is in its first position, and a second position, in which the pin and roller are disengaged from the bolt. The latch can be opened automatically when a defined load is provided on the bolt, or manually by depressing the trigger to disengage the pin and roller from the bolt.

IPC Classes  ?

  • E05C 19/02 - Automatic catches, i.e. released by pull or pressure on the wing
  • B64D 29/06 - Attaching of nacelles, fairings, or cowlings
  • E05B 15/04 - Spring arrangements in locks
  • E05B 51/02 - Operating or controlling locks or other fastening devices by other non-mechanical means by pneumatic or hydraulic means
  • E05C 3/24 - Fastening devices with bolts moving pivotally or rotatively with latching action with operating handle or equivalent member moving otherwise than rigidly with the latch the bolt being spring-controlled in the form of a bifurcated member

80.

Fastener and fastener installation tool

      
Application Number 15282425
Grant Number 10087972
Status In Force
Filing Date 2016-09-30
First Publication Date 2017-01-19
Grant Date 2018-10-02
Owner HOWMET AEROSPACE INC. (USA)
Inventor Corbett, Robert J.

Abstract

A fastening system including a fastener and a fastener installation tool. The fastener includes a pin member having an elongated shank portion with a threaded portion, a stop shoulder located at an end of the threaded portion, and a pull portion extending from the stop shoulder. The stop shoulder includes an outer rim and an inner annular wall. The inner annular wall and the inner face form an annular recess. The fastener installation tool includes a puller having a front face. The recess of the fastener is adapted to receive the front face of the fastener installation tool when the puller engages the pull portion of the pin member and facilitates alignment of teeth of the installation tool and pull grooves of the pin member.

IPC Classes  ?

  • 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
  • B21J 15/02 - Riveting procedures
  • B21J 15/04 - Riveting hollow rivets mechanically
  • F16B 19/10 - Hollow rivets; Multi-part rivets fastened by expanding mechanically
  • F16B 19/05 - Bolts fastening by swaged-on collars

81.

Handle mechanisms

      
Application Number 15204120
Grant Number 10337218
Status In Force
Filing Date 2016-07-07
First Publication Date 2017-01-12
Grant Date 2019-07-02
Owner HOWMET AEROSPACE INC. (USA)
Inventor Do, Thai

Abstract

A handle mechanism includes a gear drive having an interior end and an exterior end; an inside handle fixed to the interior end; a button; a finger; a handle drive; an outside handle; and a spring. The button has an interior end and an exterior end, which is positioned within the exterior end of the gear drive. The handle drive is positioned within the exterior end of the gear drive and is rotatable relative thereto. The outside handle and the handle drive rotate together. The outside handle moves between a first position, wherein it is constrained from rotation, and a second position. The finger is fixed to the exterior end of the button, which moves between a first position, wherein the finger causes the gear drive and the handle drive to rotate together, and a second position. The spring biases the button and the outside handle toward their first positions.

IPC Classes  ?

  • E05B 13/00 - Devices preventing the key or the handle or both from being used
  • E05B 5/02 - Handles completely let into the surface of the wing able to be turned outwards before operation
  • E05C 5/02 - Fastening devices with bolts moving otherwise than only rectilinearly and only pivotally or rotatively both moving axially and turning about their axes to secure the wing
  • E05C 3/00 - Fastening devices with bolts moving pivotally or rotatively
  • E05C 3/12 - Fastening devices with bolts moving pivotally or rotatively with latching action
  • E05C 3/14 - Fastening devices with bolts moving pivotally or rotatively with latching action with operating handle or equivalent member rigid with the latch
  • E05C 1/06 - Fastening devices with bolts moving rectilinearly without latching action with operating handle or equivalent member moving otherwise than rigidly with the bolt
  • E05B 1/00 - Knobs or handles for wings; Knobs, handles, or press buttons for locks or latches on wings
  • B64C 1/14 - Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens

82.

Wheel

      
Application Number 29531940
Grant Number D0773974
Status In Force
Filing Date 2015-06-30
First Publication Date 2016-12-13
Grant Date 2016-12-13
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Degeorge, Grant
  • Peer, Gregory L.
  • Sklyut, Henry
  • Ciccola, Gabriele

83.

6XXX aluminum alloys, and methods for producing the same

      
Application Number 15224918
Grant Number 10590515
Status In Force
Filing Date 2016-08-01
First Publication Date 2016-11-24
Grant Date 2020-03-17
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Lin, Jen C.
  • Rovito, Anton J.
  • Doyle, Timothy P.
  • Sullivan, Shawn P.
  • Ciccola, Gabriele F.
  • Tan, Christopher J.

Abstract

New 6xxx aluminum alloys are disclosed. The new 6xxx aluminum alloys may include 1.05-1.50 wt. Mg, 0.60-0.95 wt. % Si, where the (wt. % Mg)/(wt. % Si) is from 1.30 to 1.90, 0.275-0.50 wt. % Cu, and from 0.05 to 1.0 wt. % of at least one secondary element, wherein the secondary element is selected from the group consisting of V, Fe, Cr, Mn, Zr, Ti, and combinations thereof.

IPC Classes  ?

  • C22C 21/08 - Alloys based on aluminium with magnesium as the next major constituent with silicon
  • C22C 21/02 - Alloys based on aluminium with silicon as the next major constituent
  • C22C 21/14 - Alloys based on aluminium with copper as the next major constituent with silicon
  • C22C 21/16 - Alloys based on aluminium with copper as the next major constituent with magnesium
  • C22F 1/047 - 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 of alloys with magnesium as the next major constituent
  • C22F 1/05 - 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 of alloys of the Al-Si-Mg type, i.e. containing silicon and magnesium in approximately equal proportions

84.

Latch having tool recess in trigger

      
Application Number 15084660
Grant Number 11041331
Status In Force
Filing Date 2016-03-30
First Publication Date 2016-10-06
Grant Date 2021-06-22
Owner HOWMET AEROSPACE INC. (USA)
Inventor Do, Thai

Abstract

A latch including a body and an engagement member adapted to engage releasably a clevis, and a handle with a trigger attached pivotally and is pivotable between a first position, in which the trigger is engaged releasably with the clevis, and a second position, in which the trigger is disengaged from the clevis. The trigger includes a recess that receives a tool to facilitate pivoting the trigger from its first position to its second position. The latch may include a drive and the trigger includes a socket adapted to receive a key that facilitates moving a drive to clear the handle and disengaging the trigger with the clevis to open the handle.

IPC Classes  ?

  • E05B 13/00 - Devices preventing the key or the handle or both from being used
  • E05B 85/26 - Cooperation between bolts and detents
  • E05C 19/12 - Hook fastenings; Fastenings in which a link engages a fixed hook-like member pivotally mounted
  • E05C 19/14 - Hook fastenings; Fastenings in which a link engages a fixed hook-like member pivotally mounted with toggle action
  • E05B 35/00 - Locks for use with special keys or a plurality of keys
  • E05C 3/16 - Fastening devices with bolts moving pivotally or rotatively with latching action with operating handle or equivalent member moving otherwise than rigidly with the latch
  • E05C 3/30 - Fastening devices with bolts moving pivotally or rotatively with latching action with operating handle or equivalent member moving otherwise than rigidly with the latch the bolt being spring-controlled in the form of a hook

85.

Coated fasteners with conforming seals

      
Application Number 15059608
Grant Number 09939004
Status In Force
Filing Date 2016-03-03
First Publication Date 2016-09-29
Grant Date 2018-04-10
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Kamal, Manish
  • Haylock, Luke
  • Mulazimoglu, Hasim
  • Liebscher, Andreas
  • Rizza, Gregory
  • Pinheiro, Rodrigo
  • Prachumsri, Wudhidham

Abstract

A pin member for a fastener includes an elongated shank having a first end, a second end opposite the first end, a cylindrical shank portion having an outer surface, a head located at the first end of the elongated shank, the head including a bearing surface located on the bearing surface of the head, and a threaded portion located at the second end of the elongated shank. The pin member can be fully coated with a coating. A conformable seal element is attached to the pin member, which is adapted to fill the microscopic voids between the bearing surface of the head of the pin member and the surrounding structure under the axial load exerted by the fastener during installation. The seal element can be separate and distinct from the pin member. The seal element can be attached to the pin member for the sake of convenience, but the seal element can deform independently of the pin member and the surrounding structure in response to the forces exerted by the fastener.

IPC Classes  ?

  • F16B 43/00 - Washers or equivalent devices; Other devices for supporting bolt-heads or nuts
  • F16B 33/00 - Features common to bolt and nut
  • F16B 33/06 - Surface treatment of parts furnished with screw-thread, e.g. for preventing seizure
  • F16B 35/06 - Specially-shaped heads
  • B64D 45/02 - Lightning protectors; Static dischargers
  • C23C 30/00 - Coating with metallic material characterised only by the composition of the metallic material, i.e. not characterised by the coating process
  • F16B 19/04 - Rivets; Spigots or the like fastened by riveting

86.

Dual piston close clearance fastening tool

      
Application Number 15074514
Grant Number 09550228
Status In Force
Filing Date 2016-03-18
First Publication Date 2016-09-22
Grant Date 2017-01-24
Owner HOWMET AEROSPACE INC. (USA)
Inventor Wilcox, Robert

Abstract

A fastener installation tool includes a nose assembly, first and second cylinders, first and second pistons, and a yoke. The nose assembly is adapted to apply an axial load to a fastener along a longitudinal axis of the nose assembly. The first and second cylinders are diametrically opposed to one another with respect to the longitudinal axis of the nose assembly. The first piston is disposed within the first cylinder and is movable along a longitudinal axis thereof. The second piston is disposed within the second cylinder and is movable along a longitudinal axis thereof. The yoke connects the first piston, the second piston, and the nose assembly such that motion of one of the pistons along its corresponding longitudinal axis causes motion of the other one of the pistons along its corresponding longitudinal axis and motion of at least a portion of the nose assembly along its longitudinal axis.

IPC Classes  ?

  • B21J 15/10 - Riveting machines
  • B21J 15/20 - Drives for riveting machines; Transmission means therefor operated by hydraulic or liquid pressure
  • B21J 15/02 - Riveting procedures
  • B21J 15/04 - Riveting hollow rivets mechanically
  • B21J 15/18 - Drives for riveting machines; Transmission means therefor operated by air pressure or other gas pressure, e.g. explosion pressure
  • F15B 15/14 - Fluid-actuated devices for displacing a member from one position to another; Gearing associated therewith characterised by the construction of the motor unit of the straight-cylinder type
  • B21J 15/32 - Devices for inserting or holding rivets in position with or without feeding arrangements

87.

Blind fasteners

      
Application Number 15001979
Grant Number 10006478
Status In Force
Filing Date 2016-01-20
First Publication Date 2016-07-28
Grant Date 2018-06-26
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Hufnagl, Gerhart
  • Desalvo, Douglas
  • Torrence, Randy

Abstract

A fastener includes a sleeve, a core bolt, and an insert. The sleeve includes a first portion having a first inner diameter, a second portion having a second inner diameter, and a step intermediate the first and second portions. The core bolt includes a cylindrical portion having a first diameter, a threaded portion having a major diameter, and a thread run-out intermediate the cylindrical and threaded portions. The insert is disposed within the sleeve and is sized and shaped to be retained between the step of the sleeve and the thread run-out of the core bolt when the fastener is in a pre-installation position. The fastener compresses the insert between the step of the sleeve and the thread run-out of the core bolt by an installation motion of the core bolt. The insert deforms away from the core bolt to initiate formation of a bulb in response to the compression.

IPC Classes  ?

  • F16B 13/06 - Dowels or other devices fastened in walls or the like by inserting them in holes made therein for that purpose with parts gripping in the hole or behind the reverse side of the wall after inserting from the front combined with expanding sleeve
  • F16B 19/10 - Hollow rivets; Multi-part rivets fastened by expanding mechanically
  • F16B 5/04 - Joining sheets or plates to one another or to strips or bars parallel to them by means of riveting
  • 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

88.

Methods for producing forged products and other worked products

      
Application Number 15083007
Grant Number 10220434
Status In Force
Filing Date 2016-03-28
First Publication Date 2016-07-21
Grant Date 2019-03-05
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Bush, Dustin M.
  • Roegner, Eric V.
  • Colvin, Edward L.
  • Mueller, Larry N.
  • Bodily, Brandon Hendrickson
  • Rioja, Roberto J.

Abstract

Methods for producing forged products and other worked products are disclosed. In one embodiment, a method comprises using additive manufacturing to produce a metal shaped-preform and, after the using step, forging the metal shaped-preform into a final forged product. The final forged product may optionally be annealed.

IPC Classes  ?

  • B21J 5/02 - Die forging; Trimming by making use of special dies
  • C22F 1/18 - High-melting or refractory metals or alloys based thereon
  • F01D 5/28 - Selecting particular materials; Measures against erosion or corrosion
  • C23C 4/12 - Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the method of spraying
  • C23C 4/08 - Metallic material containing only metal elements
  • B21J 1/00 - Preparing metal stock
  • B21J 1/06 - Heating or cooling methods or arrangements specially adapted for performing forging or pressing operations
  • C23C 4/01 - Selective coating, e.g. pattern coating, without pre-treatment of the material to be coated
  • B23P 15/02 - Making specific metal objects by operations not covered by a single other subclass or a group in this subclass turbine or like blades from one piece
  • B22F 3/105 - Sintering only by using electric current, laser radiation or plasma
  • B22F 5/04 - Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product of turbine blades
  • B21J 5/00 - Methods for forging, hammering, or pressing; Special equipment or accessories therefor
  • C22C 1/04 - Making non-ferrous alloys by powder metallurgy

89.

Methods for producing forged products and other worked products

      
Application Number 15069686
Grant Number 10307814
Status In Force
Filing Date 2016-03-14
First Publication Date 2016-07-07
Grant Date 2019-06-04
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Bush, Dustin M.
  • Roegner, Eric V.
  • Colvin, Edward L.
  • Mueller, Larry N.
  • Bodily, Brandon Hendrickson

Abstract

Methods for producing forged products and other worked products are disclosed. In one embodiment, a method comprises using additive manufacturing to produce a metal shaped-preform and, after the using step, forging the metal shaped-preform into a final forged product. The final forged product may optionally be annealed.

IPC Classes  ?

  • B21J 1/00 - Preparing metal stock
  • B21J 5/02 - Die forging; Trimming by making use of special dies
  • C22F 1/18 - High-melting or refractory metals or alloys based thereon
  • F01D 5/28 - Selecting particular materials; Measures against erosion or corrosion
  • C23C 4/12 - Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the method of spraying
  • C23C 4/08 - Metallic material containing only metal elements
  • B21J 1/06 - Heating or cooling methods or arrangements specially adapted for performing forging or pressing operations
  • C23C 4/01 - Selective coating, e.g. pattern coating, without pre-treatment of the material to be coated
  • B23P 15/02 - Making specific metal objects by operations not covered by a single other subclass or a group in this subclass turbine or like blades from one piece
  • B22F 3/105 - Sintering only by using electric current, laser radiation or plasma
  • B22F 5/04 - Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product of turbine blades
  • B21J 5/00 - Methods for forging, hammering, or pressing; Special equipment or accessories therefor
  • C22C 1/04 - Making non-ferrous alloys by powder metallurgy

90.

Resistance welding fastener, apparatus and methods for joining similar and dissimilar materials

      
Application Number 14967777
Grant Number 10384296
Status In Force
Filing Date 2015-12-14
First Publication Date 2016-06-16
Grant Date 2019-08-20
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Spinella, Donald J.
  • Bergstrom, Daniel

Abstract

An apparatus and method for fastening layers of non-ferrous alloys, like aluminum, magnesium and copper utilizes a steel fastener and a spot welding machine. The fastener and metals are stacked and the heat from the welder's electric current softens the lower melting point aluminum allowing the fastener to penetrate the aluminum. A weld zone between the fastener and the various layers creates an internal weld. The fastener has a rough shaft that is coated by the molten weld zone and is hard to withdraw on solidification. Layers of non-conductive materials like plastics and ceramics may also be affixed to a conductive layer using a fastener made from a compatible material that extends through a pilot hole and welds to or penetrates a conductive layer. The fastener may have projections that initially reduce contact area with the stack.

IPC Classes  ?

  • B23K 11/30 - Features relating to electrodes
  • B23K 11/18 - Resistance welding; Severing by resistance heating taking account of the properties of the material to be welded of non-ferrous metals
  • B23K 11/20 - Resistance welding; Severing by resistance heating taking account of the properties of the material to be welded of different metals
  • F16B 5/08 - Joining sheets or plates to one another or to strips or bars parallel to them by means of welds or the like
  • B23K 11/00 - Resistance welding; Severing by resistance heating
  • B23K 35/02 - Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape
  • B23K 101/38 - Conductors
  • B23K 103/10 - Aluminium or alloys thereof
  • B23K 103/12 - Copper or alloys thereof
  • B23K 103/08 - Non-ferrous metals or alloys
  • B23K 103/18 - Dissimilar materials

91.

Fasteners with coated and textured pin members

      
Application Number 14854223
Grant Number 09638236
Status In Force
Filing Date 2015-09-15
First Publication Date 2016-03-17
Grant Date 2017-05-02
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Kamal, Manish
  • Haylock, Luke
  • Mulazimoglu, Hasim
  • Liebscher, Andreas
  • Rizza, Gregory
  • Pinheiro, Rodrigo

Abstract

A pin member for a fastener includes an elongated shank having a first end, a second end opposite the first end, a cylindrical shank portion having an outer surface, a head located at the first end of the elongated shank, the head including a bearing surface located on the bearing surface of the head, and a threaded portion located at the second end of the elongated shank. Either or both of the bearing surface of the head or the outer surface of the cylindrical shank portion is coated with a coating and/or is textured. The coating may be tungsten, molybdenum, copper, or a refractory ceramic. The textured surfaces may include a surface roughness greater than 0.5 micron.

IPC Classes  ?

  • 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
  • F16B 33/00 - Features common to bolt and nut
  • B64D 45/02 - Lightning protectors; Static dischargers
  • F16B 33/06 - Surface treatment of parts furnished with screw-thread, e.g. for preventing seizure
  • F16B 35/06 - Specially-shaped heads
  • F16B 19/04 - Rivets; Spigots or the like fastened by riveting

92.

Fasteners with conforming sleeves

      
Application Number 13618419
Grant Number 09562556
Status In Force
Filing Date 2012-09-14
First Publication Date 2016-02-25
Grant Date 2017-02-07
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Haylock, Luke
  • Mulazimoglu, Hasim
  • Zeng, Liang

Abstract

A sleeve interference fastener including a conformable sleeve, wherein the conformable sleeve is comprised of at least one first material having a hardness of X, and a pin member, wherein the pin member is comprised of at least one second material having a hardness of Y, wherein X is sufficiently less than Y so that, in an installed position of an interference fit, at least a portion of the at least one first material of the conformable sleeve conforms to a contour of an inner surface of a hole of a composite structure so as to create a continuous electrical contact at an interface between the inner surface of the hole of the composite structure and the conformable sleeve.

IPC Classes  ?

  • F16B 19/02 - Bolts or sleeves for positioning of machine parts, e.g. notched taper pins, fitting pins, sleeves, eccentric positioning rings
  • F16B 4/00 - Shrinkage connection, e.g. assembled with the parts at different temperature; Force fits; Non-releasable friction-grip fastenings
  • 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
  • B64D 45/02 - Lightning protectors; Static dischargers
  • F16B 1/00 - Devices for securing together, or preventing relative movement between, constructional elements or machine parts

93.

Textured sleeves for fasteners

      
Application Number 14833885
Grant Number 09759246
Status In Force
Filing Date 2015-08-24
First Publication Date 2016-02-25
Grant Date 2017-09-12
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Haylock, Luke
  • Mulazimoglu, Hasim

Abstract

A fastener adapted to be installed in a hole of a composite structure includes a sleeve, a pin member, and a locking member. The sleeve has an outer surface having an outer diameter. The outer surface of the sleeve is textured. The outer diameter of the tubular portion is less than an inner diameter of the hole of the structure. The pin member has a shank portion. The sleeve is adapted to expand radially over the shank portion of the pin member to form an interference fit between the outer surface of the sleeve and the hole of the structure so as to provide an installed position of the fastener. When the fastener is in the installed position, the texture of the outer surface of the tubular portion deforms to engage with voids of the composite material present on the inner surface of the hole.

IPC Classes  ?

  • 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
  • B64D 45/02 - Lightning protectors; Static dischargers
  • F16B 19/00 - Bolts without screw-thread; Pins, including deformable elements; Rivets
  • F16B 19/05 - Bolts fastening by swaged-on collars

94.

High strength forged aluminum alloy products

      
Application Number 14847303
Grant Number 10119184
Status In Force
Filing Date 2015-09-08
First Publication Date 2015-12-31
Grant Date 2018-11-06
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Bush, Dustin M.
  • Colvin, Edward L.
  • Rioja, Roberto J.
  • Sawtell, Ralph R.

Abstract

High strength forged aluminum alloys and methods for producing the same are disclosed. The forged aluminum alloy products may have grains having a high aspect ratio in at least two planes, generally the L-ST and the LT-ST planes. The forged aluminum alloy products may also have a high amount of texture. The forged products may realize increased strength relative to conventionally prepared forged products of comparable product form, composition and temper.

IPC Classes  ?

  • C22C 21/12 - Alloys based on aluminium with copper as the next major constituent
  • C22C 21/16 - Alloys based on aluminium with copper as the next major constituent with magnesium
  • C22C 21/10 - Alloys based on aluminium with zinc as the next major constituent
  • C22F 1/053 - 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 of alloys with zinc as the next major constituent
  • 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
  • C22C 21/14 - Alloys based on aluminium with copper as the next major constituent with silicon
  • C22F 1/057 - 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 of alloys with copper as the next major constituent

95.

Fastener installation tool with internal concentric sleeves

      
Application Number 14631085
Grant Number 09192982
Status In Force
Filing Date 2015-02-25
First Publication Date 2015-08-27
Grant Date 2015-11-24
Owner HOWMET AEROSPACE INC. (USA)
Inventor Wilcox, Robert

Abstract

A fastener installation tool including a cylinder assembly having a housing and a handle/sleeve assembly attached to the housing. The handle/sleeve assembly includes a handle having a bore and an inner wall defined by the bore. The handle/sleeve assembly further includes an outer sleeve having an outer wall and an inner wall, and an inner sleeve having an outer wall and an inner wall. The outer sleeve is positioned within the bore of the handle, while the inner sleeve is positioned concentrically within the outer sleeve to form an annular space between the outer wall of the inner sleeve and the inner wall of the outer sleeve. The annular space is utilized to conduct hydraulic fluid.

IPC Classes  ?

  • B21J 15/34 - Devices for inserting or holding rivets in position with or without feeding arrangements for installing tubular rivets
  • B21J 15/10 - Riveting machines
  • B21J 15/16 - Drives for riveting machines; Transmission means therefor
  • B21J 15/22 - Drives for riveting machines; Transmission means therefor operated by both hydraulic or liquid pressure and gas pressure

96.

Wheel assembly

      
Application Number 14613736
Grant Number 09604498
Status In Force
Filing Date 2015-02-04
First Publication Date 2015-08-06
Grant Date 2017-03-28
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Zehnder, Craig M.
  • Peer, Greg
  • Burg, James
  • Leonard, Stephen
  • Sklyut, Henry
  • Cobes, John
  • Rovito, Anton
  • Ciccola, Gabriele
  • Weiler, Kelly
  • Kulak, Michael
  • Black, James
  • Jarvis, Glenn
  • Lee, Wilson
  • Degeorge, Grant

Abstract

A wheel for a pneumatic tire has a rim with one monolithic bead seat and a removable beat seat. The removable bead seat has two halves that embrace the rim and engage a groove to retain the tire. The removable bead seat may have a second lip either monolithically formed or as a part of a separate retainer that bolts to the bead seat. The wheel may be made from aluminum alloy.

IPC Classes  ?

  • B60B 25/00 - Rims built-up of several main parts
  • B60B 25/12 - Seat rings for the tyre bead part, e.g. split with integral flange part
  • B60B 11/02 - Units of separate wheels mounted for independent or coupled rotation
  • B60B 25/18 - Arrangement of split rings
  • B60B 25/20 - Arrangement of screw, bolts, or shouldered pins

97.

Resistance welding fastener, apparatus and methods

      
Application Number 14611555
Grant Number 10903587
Status In Force
Filing Date 2015-02-02
First Publication Date 2015-08-06
Grant Date 2021-01-26
Owner Howmet Aerospace Inc. (USA)
Inventor
  • Spinella, Donald J.
  • Bergstrom, Daniel

Abstract

An apparatus and method for fastening dissimilar materials like steel, plastic and aluminum. A resistance welding fastener having multiple layers may be used with or without a sealant. The fastener may be used to form an aluminum covered steel laminate via a hemming pattern of attachment. The fastener may have a solid shaft or have an extended reach and have features for interacting with the welding electrode. A variety of electrode tips may be employed to cooperate with the fastener.

IPC Classes  ?

  • B23K 11/11 - Spot welding
  • H01R 4/02 - Soldered or welded connections
  • B23K 11/20 - Resistance welding; Severing by resistance heating taking account of the properties of the material to be welded of different metals
  • B23K 35/02 - Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by mechanical features, e.g. shape
  • H01R 43/02 - Apparatus or processes specially adapted for manufacturing, assembling, maintaining, or repairing of line connectors or current collectors or for joining electric conductors for soldered or welded connections
  • F16B 37/06 - Devices for fastening nuts to surfaces, e.g. sheets, plates by means of welding or riveting
  • H01R 4/62 - Connections between conductors of different materials; Connections between or with aluminium or steel-core aluminium conductors
  • B23K 103/20 - Ferrous alloys and aluminium or alloys thereof
  • F16B 5/08 - Joining sheets or plates to one another or to strips or bars parallel to them by means of welds or the like

98.

Fastener and fastener installation tool

      
Application Number 14601453
Grant Number 09488213
Status In Force
Filing Date 2015-01-21
First Publication Date 2015-07-30
Grant Date 2016-11-08
Owner HOWMET AEROSPACE INC. (USA)
Inventor Corbett, Robert J.

Abstract

A fastening system including a fastener and a fastener installation tool. The fastener includes a pin member having an elongated shank portion with a threaded portion, a stop shoulder located at an end of the threaded portion, and a pull portion extending from the stop shoulder. The stop shoulder includes an inner annular wall extending longitudinally from the end of the threaded portion, and an inner face extending outwardly and obliquely from the shank portion. The inner annular wall and the inner face form an annular receiving area. The fastener installation tool includes a puller having a front face. The receiving area of the fastener is adapted to receive the front face of the fastener installation tool when the puller engages the pull portion of the pin member.

IPC Classes  ?

  • F16B 19/00 - Bolts without screw-thread; Pins, including deformable elements; Rivets
  • 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
  • B21J 15/02 - Riveting procedures
  • F16B 19/10 - Hollow rivets; Multi-part rivets fastened by expanding mechanically
  • B21J 15/04 - Riveting hollow rivets mechanically
  • F16B 19/05 - Bolts fastening by swaged-on collars

99.

Titanium alloy having good oxidation resistance and high strength at elevated temperatures

      
Application Number 13840265
Grant Number 09957836
Status In Force
Filing Date 2013-03-15
First Publication Date 2015-07-09
Grant Date 2018-05-01
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Sun, Fusheng
  • Crist, Ernest M.
  • Yu, Kuang-O

Abstract

A titanium alloy may be characterized by a good oxidation resistance, high strength and creep resistance at elevated temperatures up to 750° C., and good cold/hot forming ability, good superplastic forming performance, and good weldability. The alloy may contain, in weight percent, aluminum 4.5 to 7.5, tin 2.0 to 8.0, niobium 1.5 to 6.5, molybdenum 0.1 to 2.5, silicon 0.1 to 0.6, oxygen up to 0.20, carbon up to 0.10, and balance titanium with incidental impurities.

IPC Classes  ?

  • C22C 1/02 - Making non-ferrous alloys by melting
  • F01D 25/00 - Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
  • C22C 14/00 - Alloys based on titanium
  • C22F 1/18 - High-melting or refractory metals or alloys based thereon
  • F01D 5/28 - Selecting particular materials; Measures against erosion or corrosion

100.

Asymmetric fastener recess and key

      
Application Number 14503582
Grant Number 09970469
Status In Force
Filing Date 2014-10-01
First Publication Date 2015-04-02
Grant Date 2018-05-15
Owner HOWMET AEROSPACE INC. (USA)
Inventor
  • Pinheiro, Rodrigo
  • Haylock, Luke

Abstract

A fastening system including a pin member and a key for engaging the pin member. The pin member includes a shank portion and a recess formed within an end face of the shank portion. The recess includes a plurality of splines and recesses that form first and second bearing surfaces oriented at angles. The key includes a key head having a plurality of splines and grooves that form first and second bearing surfaces oriented at angles. The plurality of splines and recesses of the pin member and the plurality of splines and recesses of the key are adapted to communicate with each other when tightening and loosening the pin member.

IPC Classes  ?

  • F16B 23/00 - Specially-shaped heads of bolts or screws for rotations by a tool
  • 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
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