Nileworks Inc.

Japan

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Patent
United States - USPTO
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Date
2023 2
2022 7
2021 6
2020 2
IPC Class
B64C 39/02 - Aircraft not otherwise provided for characterised by special use 14
G05D 1/10 - Simultaneous control of position or course in three dimensions 8
G08G 5/00 - Traffic control systems for aircraft 6
A01M 7/00 - Special adaptations or arrangements of liquid-spraying apparatus for purposes covered by this subclass 5
B64D 1/18 - Dropping or releasing powdered, liquid or gaseous matter, e.g. for fire-fighting by spraying, e.g. insecticides 5
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Status
Pending 13
Registered / In Force 4
Found results for  patents

1.

GROWTH ASSESSMENT SYSTEM, GROWTH ASSESSMENT SERVER AND GROWTH ASSESSMENT METHOD

      
Application Number 17797122
Status Pending
Filing Date 2020-02-06
First Publication Date 2023-06-01
Owner NILEWORKS INC. (Japan)
Inventor
  • Wake, Chihiro
  • Yanagishita, Hiroshi
  • Kato, Hiroki

Abstract

Provided are a growth assessment system, growth assessment server and growth assessment method with which it is possible to improve the accuracy of a growth assessment model. A difference determination unit of the growth assessment system compares an estimated growth state value, which is growth state value for a crop that is calculated by a growth assessment model, with a detected growth state value, which is a growth state value for the crop that is calculated based on an image of a field or the crop that is acquired by a camera. A model correction unit corrects the growth assessment model depending on the comparison result from the difference determination unit.

IPC Classes  ?

2.

SURVEY SYSTEM, SURVEY METHOD, AND SURVEY PROGRAM

      
Application Number 17919800
Status Pending
Filing Date 2020-04-20
First Publication Date 2023-05-18
Owner NILEWORKS INC. (Japan)
Inventor
  • Murakumo, Yutaka
  • Wake, Chihiro
  • Kato, Hiroki

Abstract

A survey system for accurately surveying an area includes a coordinate acquisition section that acquires a set of three-dimensional coordinates of a survey point or a base station used for determining sets of coordinates of the area, as a set of measurement coordinates, a comparative coordinate acquisition section that acquires at least a height-direction coordinate value of a set of comparative coordinates indicating a position within a predetermined range from the acquired set of measurement coordinates; and a determining section that calculates a difference between a height-direction coordinate value of the set of measurement coordinates and the height-direction coordinate value of the set of comparative coordinates and determines that at least any one of the set of measurement coordinates and the set of comparative coordinates are incorrect when the difference is larger than a predetermined value.

IPC Classes  ?

  • G01C 15/02 - Means for marking measuring points
  • B64C 39/02 - Aircraft not otherwise provided for characterised by special use
  • B64U 10/00 - Type of UAV

3.

INDUSTRIAL MACHINERY SYSTEM, INDUSTRIAL MACHINE, CONTROL APPARATUS, CONTROL METHOD FOR INDUSTRIAL MACHINERY SYSTEM, AND CONTROL PROGRAM FOR INDUSTRIAL MACHINERY SYSTEM

      
Application Number 17603974
Status Pending
Filing Date 2020-05-20
First Publication Date 2022-06-30
Owner NILEWORKS INC. (Japan)
Inventor
  • Wake, Chihiro
  • Yanagishita, Hiroshi
  • Murakumo, Yutaka

Abstract

There is provided an industrial machinery system including an industrial machine, an area information acquiring device that acquires information on an operation area where the industrial machine is to be caused to perform an operation, and a control apparatus that determines whether to perform the operation by the industrial machine in the operation area, wherein the control apparatus includes a storage section that stores information on a registered area, the information being acquired in advance, and a determining section that determines whether to perform the operation by the industrial machine in accordance with whether an area corresponding to the operation area is identifiable from the registered area stored in the storage section.

IPC Classes  ?

  • A01B 69/04 - Special adaptations of automatic tractor steering, e.g. electric system for contour ploughing
  • G05D 1/10 - Simultaneous control of position or course in three dimensions
  • B64C 39/02 - Aircraft not otherwise provided for characterised by special use

4.

DRONE CONTROLLER AND CONTROL PROGRAM

      
Application Number 17432242
Status Pending
Filing Date 2020-02-21
First Publication Date 2022-06-16
Owner NILEWORKS INC. (Japan)
Inventor
  • Miyagi, Ryo
  • Wake, Chihiro
  • Yanagishita, Hiroshi

Abstract

Provided are a controller for controlling a drone that performs autonomous flight under computer control and a control program that runs on a tablet terminal. On a screen of the controller or the program, map information on an agricultural field over which the drone is to fly, route information on a route along which the drone is to fly, and an emergency stop button of the drone are displayed. A button for performing fine adjustment on an altitude may be displayed. It is desirable that the emergency stop button be translucent and be displayed such that the button is superimposed on the map information. It is desirable that emergency stop be performed only when a predetermined operation is performed on the emergency stop button a predetermined number of times or more within a predetermined time period.

IPC Classes  ?

  • B64C 13/22 - Initiating means actuated automatically, e.g. responsive to gust detectors readily revertible to personal control
  • B64C 39/02 - Aircraft not otherwise provided for characterised by special use
  • G08G 5/00 - Traffic control systems for aircraft
  • B64C 13/20 - Initiating means actuated automatically, e.g. responsive to gust detectors using radiated signals
  • G05D 1/00 - Control of position, course, altitude, or attitude of land, water, air, or space vehicles, e.g. automatic pilot

5.

DRONE SYSTEM, DRONE, MOVABLE BODY, DEMARCATING MEMBER, CONTROL METHOD FOR DRONE SYSTEM, AND DRONE SYSTEM CONTROL PROGRAM

      
Application Number 17423123
Status Pending
Filing Date 2020-01-15
First Publication Date 2022-05-05
Owner NILEWORKS INC. (Japan)
Inventor
  • Wake, Chihiro
  • Yanagishita, Hiroshi

Abstract

There is provided a drone system in which a drone and a movable body operate in coordination with each other, the movable body being capable of moving with the drone aboard and allowing the drone to make a takeoff and a landing, the drone system includes a demarcating member that demarcates an operation area and detects an intruder into the operation area, the operation area being an area where at least one of the drone and the movable body performs an operation, the movable body includes a movement control section that stops movement of the movable body based on the detection of the intruder by the demarcating member, and the drone includes a landing position determining section that determines a landing position based on a stop position of the movable body.

IPC Classes  ?

  • G05D 1/06 - Rate of change of altitude or depth
  • B64D 45/04 - Landing aids; Safety measures to prevent collision with earth's surface
  • G05D 1/00 - Control of position, course, altitude, or attitude of land, water, air, or space vehicles, e.g. automatic pilot
  • B64C 39/02 - Aircraft not otherwise provided for characterised by special use

6.

Drone system, drone, plan management apparatus, plan management method for drone system, and plan management program for drone system

      
Application Number 17423937
Grant Number 11868144
Status In Force
Filing Date 2020-01-21
First Publication Date 2022-03-24
Grant Date 2024-01-09
Owner NILEWORKS INC. (Japan)
Inventor
  • Wake, Chihiro
  • Yanagishita, Hiroshi

Abstract

In a drone system in which a drone and a movable body operate in coordination with each other, the drone performing a predetermined operation in an agricultural field, the movable body being capable of moving with the drone aboard and allowing the drone to make a takeoff and a landing, the plan determining section determines a flight plan for the drone and a movement plan for the movable body in accordance with the flight plan, and the instructing section instructs the drone to execute an operation in accordance with the flight plan and instructs the movable body to move or to be on standby in accordance with the movement plan.

IPC Classes  ?

  • G05D 1/10 - Simultaneous control of position or course in three dimensions
  • B60L 58/12 - Methods or circuit arrangements for monitoring or controlling batteries or fuel cells, specially adapted for electric vehicles for monitoring or controlling batteries responding to state of charge [SoC]
  • B64C 39/02 - Aircraft not otherwise provided for characterised by special use
  • B64D 1/16 - Dropping or releasing powdered, liquid or gaseous matter, e.g. for fire-fighting
  • G08G 5/00 - Traffic control systems for aircraft
  • G08G 5/02 - Automatic landing aids, i.e. systems in which flight data of incoming planes are processed to provide landing data
  • A01C 7/08 - Broadcast seeders; Seeders depositing seeds in rows
  • A01C 23/04 - Distributing under pressure; Distributing mud; Adaptation of watering systems for fertilising-liquids
  • A01M 7/00 - Special adaptations or arrangements of liquid-spraying apparatus for purposes covered by this subclass
  • A01M 9/00 - Special adaptations or arrangements of powder-spraying apparatus for purposes covered by this subclass
  • B64U 10/13 - Flying platforms
  • B64U 101/00 - UAVs specially adapted for particular uses or applications

7.

UNMANNED AERIAL VEHICLE AND MOVING BODY

      
Application Number 17276581
Status Pending
Filing Date 2019-02-28
First Publication Date 2022-02-17
Owner NILEWORKS INC. (Japan)
Inventor
  • Wake, Chihiro
  • Yanagishita, Hiroshi

Abstract

An unmanned aerial vehicle that can be disabled when it detects a phenomenon causing a malfunction of a battery is provided. The unmanned aerial vehicle is capable of carrying a detachable battery and has a battery pack, sensors detecting a phenomenon causing a malfunction of the battery pack, a memory storing the detection signal of the sensors, and cutoff circuits cutting off a power supply line from the battery pack by the detection signal. The sensor is an aerial vehicle side sensor equipped outside of the battery and on an unmanned aerial vehicle side. The memory is equipped in the battery and stores the detection signal of the aerial vehicle side sensor received through a connector connecting the battery and the unmanned aerial vehicle. The cutoff circuit is equipped on the unmanned aerial vehicle side and cuts off the power supply line from the battery pack.

IPC Classes  ?

  • B64C 39/02 - Aircraft not otherwise provided for characterised by special use
  • H01M 10/48 - Accumulators combined with arrangements for measuring, testing or indicating the condition of cells, e.g. the level or density of the electrolyte
  • H02J 7/00 - Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
  • H02H 7/18 - Emergency protective circuit arrangements specially adapted for specific types of electric machines or apparatus or for sectionalised protection of cable or line systems, and effecting automatic switching in the event of an undesired change from norm for accumulators

8.

DRONE SYSTEM, DRONE, MOVABLE BODY, DRONE SYSTEM CONTROL METHOD, AND DRONE SYSTEM CONTROL PROGRAM

      
Application Number 17299033
Status Pending
Filing Date 2019-12-02
First Publication Date 2022-01-27
Owner NILEWORKS INC. (Japan)
Inventor
  • Wake, Chihiro
  • Yanagishita, Hiroshi

Abstract

A drone system that includes a drone and a movable body which is movable with loading the drone and where the drone can take off and land, cooperate to operate and that is able to maintain a high level of safety even during autonomous flight, is provided. The drone has a flight controller controlling a flight of the drone, and a drone transmitter transmitting an information possible to distinguish whether the drone is in flight. The movable body has a take-off and landing area where the drone is loaded, takes off and lands, a movement controller loading the drone on the take-off and landing area and moving the movable body with the drone, a movable body receiver receiving an information from the drone, and a display unit.

IPC Classes  ?

  • B64C 39/02 - Aircraft not otherwise provided for characterised by special use
  • G08G 5/00 - Traffic control systems for aircraft
  • G08G 5/04 - Anti-collision systems
  • G05D 1/00 - Control of position, course, altitude, or attitude of land, water, air, or space vehicles, e.g. automatic pilot
  • G05D 1/10 - Simultaneous control of position or course in three dimensions

9.

Drone system, drone, movable body, drone system control method, and drone system control program

      
Application Number 17299956
Grant Number 11873100
Status In Force
Filing Date 2019-12-04
First Publication Date 2022-01-27
Grant Date 2024-01-16
Owner NILEWORKS INC. (Japan)
Inventor
  • Wake, Chihiro
  • Yanagishita, Hiroshi

Abstract

There is provided a drone system in which a drone and a movable body operate in coordination with each other, the movable body being capable of moving with the drone aboard and allowing the drone to make a takeoff and a landing, the movable body including: a takeoff-landing area on which the drone can be placed and that serves as a takeoff-landing point from and on which the drone takes off and lands; a movement control section capable of moving the movable body together with the drone aboard; and a movable body transmission section that sends information on the movable body, the drone including: a flight control section that causes the drone to fly; and a drone reception section that receives information on the movable body, wherein the drone sends, to the movable body, a position of a takeoff-landing point at a time when the drone takes off.

IPC Classes  ?

  • B64D 1/18 - Dropping or releasing powdered, liquid or gaseous matter, e.g. for fire-fighting by spraying, e.g. insecticides
  • B60L 50/60 - Electric propulsion with power supplied within the vehicle using propulsion power supplied by batteries or fuel cells using power supplied by batteries
  • B60L 58/12 - Methods or circuit arrangements for monitoring or controlling batteries or fuel cells, specially adapted for electric vehicles for monitoring or controlling batteries responding to state of charge [SoC]
  • B64C 39/02 - Aircraft not otherwise provided for characterised by special use
  • B64D 27/24 - Aircraft characterised by the type or position of power plant using steam, electricity, or spring force
  • B64F 1/36 - Other airport installations
  • G05D 1/10 - Simultaneous control of position or course in three dimensions
  • A01M 7/00 - Special adaptations or arrangements of liquid-spraying apparatus for purposes covered by this subclass
  • B64U 10/13 - Flying platforms
  • B64U 50/19 - Propulsion using electrically powered motors
  • B64U 80/86 - Land vehicles
  • B64U 101/00 - UAVs specially adapted for particular uses or applications

10.

UNMANNED AERIAL VEHICLE

      
Application Number 17041557
Status Pending
Filing Date 2019-03-26
First Publication Date 2021-10-07
Owner NILEWORKS INC. (Japan)
Inventor
  • Wake, Chihiro
  • Yanagishita, Hiroshi

Abstract

An unmanned aerial vehicle and a battery, possible to be disabled when a phenomenon to cause a functional disorder, are provided. The battery includes a battery pack having a battery cell, sensors detecting a phenomenon that impairs a function of the battery pack, a memory storing a detection signal of the sensors, and block circuits blocking output of the battery pack by the detection signal. The unmanned aerial vehicle includes the battery and air frame side sensors, and operates the block circuit, which the battery includes, by the detection signal of the airframe side sensors.

IPC Classes  ?

  • B60L 58/22 - Balancing the charge of battery modules
  • B64C 39/02 - Aircraft not otherwise provided for characterised by special use
  • B64D 27/24 - Aircraft characterised by the type or position of power plant using steam, electricity, or spring force
  • B64D 1/18 - Dropping or releasing powdered, liquid or gaseous matter, e.g. for fire-fighting by spraying, e.g. insecticides
  • B60L 58/13 - Maintaining the SoC within a determined range

11.

TRAVELING ROUTE GENERATING SYSTEM, TRAVELING ROUTE GENERATING METHOD, TRAVELING ROUTE GENERATING PROGRAM, COORDINATE MEASURING SYSTEM, AND DRONE

      
Application Number 17236005
Status Pending
Filing Date 2021-04-21
First Publication Date 2021-08-19
Owner NILEWORKS INC. (Japan)
Inventor
  • Wake, Chihiro
  • Yanagishita, Hiroshi
  • Murakumo, Yutaka

Abstract

There is provided a traveling route generating system for generating a traveling route for a movable device in a target area, the traveling route generating system includes: a target area information acquiring section that acquires sets of measurement-point coordinates on edges of the target area; and a movable area generating section that determines appropriateness of the sets of measurement-point coordinates, in a case where any of the plurality of sets of measurement-point coordinates is determined to be inappropriate by the determination, does not generate a movable area where the movable device can move or does not use a set of measurement-point coordinates determined to be inappropriate for generating the movable area, and in a case where the plurality of sets of measurement-point coordinates are determined to be appropriate by the determination, generates the movable area based on the plurality of sets of measurement-point coordinates.

IPC Classes  ?

  • G01C 21/20 - Instruments for performing navigational calculations
  • G05D 1/10 - Simultaneous control of position or course in three dimensions
  • G08G 5/00 - Traffic control systems for aircraft

12.

DRONE SYSTEM, DRONE, STEERING DEVICE, DRONE SYSTEM CONTROL METHOD, AND DRONE SYSTEM CONTROL PROGRAM

      
Application Number 15734245
Status Pending
Filing Date 2019-06-03
First Publication Date 2021-07-15
Owner NILEWORKS INC. (Japan)
Inventor
  • Wake, Chihiro
  • Yanagishita, Hiroshi

Abstract

A highly safe drone is provided. A remote controller and a drone are connected to each other through a network and cooperate to operate. The drone includes a flight control unit, a flight start command reception unit receiving a flight start command from a user, a drone determination unit determining a configuration of the drone itself, an external environment determination unit determining an external environment of the drone. The drone system has a plurality of states including a takeoff diagnosis state and satisfies a condition transitioning to another state. The takeoff diagnosis state includes a drone determination state where the drone determination unit determines the configuration of the drone itself and an external environment determination state where the external environment determination unit determines the external environment. The drone system makes the drone to takeoff after transitioning to the takeoff diagnosis state upon receiving the flight start command.

IPC Classes  ?

  • G05D 1/10 - Simultaneous control of position or course in three dimensions
  • G08G 5/00 - Traffic control systems for aircraft
  • B64C 39/02 - Aircraft not otherwise provided for characterised by special use

13.

DRONE, CONTROL METHOD THEREOF, AND PROGRAM

      
Application Number 17047733
Status Pending
Filing Date 2019-02-27
First Publication Date 2021-06-03
Owner NILEWORKS INC. (Japan)
Inventor
  • Wake, Chihiro
  • Yanagishita, Hiroshi

Abstract

An agricultural chemical spraying drone with improved safety is provided. The drone includes an altitude measurement sensor and a speed measurement sensor and controls not to exceed an altitude restriction and a speed restriction of an airframe by using a flight controller. The sensors are desirable be combination of multiple types. Particularly, the altitude is desirably measured by a GPS during take-off and by a sonar during chemical spraying. Weight of the airframe is measured from time to time, and the altitude restriction and the speed restriction may be adjusted according to the weight.

IPC Classes  ?

  • B64D 1/18 - Dropping or releasing powdered, liquid or gaseous matter, e.g. for fire-fighting by spraying, e.g. insecticides
  • B64C 39/02 - Aircraft not otherwise provided for characterised by special use
  • A01M 7/00 - Special adaptations or arrangements of liquid-spraying apparatus for purposes covered by this subclass
  • G05D 1/04 - Control of altitude or depth

14.

Unmanned aerial vehicle, control system thereof and control program

      
Application Number 17041552
Grant Number 11797000
Status In Force
Filing Date 2019-03-26
First Publication Date 2021-04-22
Grant Date 2023-10-24
Owner NILEWORKS INC. (Japan)
Inventor
  • Wake, Chihiro
  • Yanagishita, Hiroshi
  • Saito, Atsunori

Abstract

Being unable to restart when it collides with an object or crashes, an unmanned aerial vehicle, control system thereof and control program, for preventing damage caused by uncontrollable restarts and crashes is provided. The unmanned aerial vehicle includes a plurality of rotating bodies, a plurality of motors individually driving and rotating the plurality of rotating bodies, and a flight controller individually controlling the plurality of motors. The flight controller includes a collision/crash detection unit detecting collision or crash on the basis of a signal from a sensor, and a power cut-off command unit cutting off a power supply on the basis of a detection signal from the collision/crash detection unit.

IPC Classes  ?

  • G05D 1/00 - Control of position, course, altitude, or attitude of land, water, air, or space vehicles, e.g. automatic pilot
  • A01M 7/00 - Special adaptations or arrangements of liquid-spraying apparatus for purposes covered by this subclass
  • B64C 39/02 - Aircraft not otherwise provided for characterised by special use
  • B64D 1/18 - Dropping or releasing powdered, liquid or gaseous matter, e.g. for fire-fighting by spraying, e.g. insecticides
  • B64D 45/00 - Aircraft indicators or protectors not otherwise provided for
  • B64U 30/20 - Rotors; Rotor supports
  • B64U 50/19 - Propulsion using electrically powered motors

15.

AGRICULTURAL DRONE HAVING IMPROVED FOOLPROOF

      
Application Number 17047736
Status Pending
Filing Date 2019-02-28
First Publication Date 2021-04-15
Owner NILEWORKS INC. (Japan)
Inventor
  • Wake, Chihiro
  • Yanagishita, Hiroshi

Abstract

A drone (an aerial vehicle), able to maintain improved safety for operation by non-specialists, is provided. A farm field data stored in a cloud at take-off is compared to an environment data read by a sensor, and a control to prohibit take-off is performed if any danger is considered. In particular, it is desirable to prohibit if there is a traffic, where people and cars may pass, between the farm field and a current location, and if a direction of the drone, installed, does not point to a direction of an intrusion pathway to the target farm field. Furthermore, it is desirable to prohibit take-off if a predetermined maintenance is not performed by referring to a maintenance history.

IPC Classes  ?

  • G08G 5/00 - Traffic control systems for aircraft
  • B64C 39/02 - Aircraft not otherwise provided for characterised by special use
  • G08G 5/04 - Anti-collision systems
  • G05D 1/10 - Simultaneous control of position or course in three dimensions

16.

AGRICULTURAL DRONE HAVING IMPROVED SAFETY

      
Application Number 16962869
Status Pending
Filing Date 2019-02-28
First Publication Date 2020-11-05
Owner NILEWORKS INC. (Japan)
Inventor
  • Wake, Chihiro
  • Yanagishita, Hiroshi

Abstract

Provide is an agricultural chemical spraying drone with improved safety. An acceleration sensor and a contact detection sensor are combined to detect contact of a drone with an obstacle. In a case where the contact is detected, a retreat action such as hovering is taken. In addition, a message may be displayed on a control terminal, a warning sound may be generated, and a warning light may be turned on. Further, a structure capable of minimizing finger insertion accidents and minimizing interference with a rotor even in collision is adopted as a propeller guard.

IPC Classes  ?

  • G05D 1/10 - Simultaneous control of position or course in three dimensions
  • B64C 39/02 - Aircraft not otherwise provided for characterised by special use
  • B64D 27/24 - Aircraft characterised by the type or position of power plant using steam, electricity, or spring force
  • B64D 1/18 - Dropping or releasing powdered, liquid or gaseous matter, e.g. for fire-fighting by spraying, e.g. insecticides
  • B64C 27/00 - Rotorcraft; Rotors peculiar thereto
  • B64D 45/00 - Aircraft indicators or protectors not otherwise provided for
  • A01M 7/00 - Special adaptations or arrangements of liquid-spraying apparatus for purposes covered by this subclass

17.

Battery mounting unit, electric device, and power supply unit

      
Application Number 16644767
Grant Number 11309611
Status In Force
Filing Date 2018-10-09
First Publication Date 2020-09-17
Grant Date 2022-04-19
Owner
  • THE FURUKAWA BATTERY CO., LTD. (Japan)
  • NILEWORKS INC. (Japan)
Inventor
  • Onishi, Yuta
  • Isa, Akino
  • Watanabe, Hitoshi
  • Yamakata, Masanori
  • Yanagishita, Hiroshi
  • Wake, Chihiro

Abstract

A battery mount from which a battery device is attachable and detachable results in a configuration that enables easy attachment and detachment of a battery having various shapes. The battery mount includes: connection terminals configured to fit to external terminals of the battery and having a shape along which the external terminals are slidable in at least one direction; and a lever rotatable about a fulcrum and located at a side at which the connection terminals are located when seen from the battery in a state where the external terminals are fitted to the connection terminals. The external terminals are configured to be elastically deformable to fit to the connection terminals by sandwiching the connection terminals therein.

IPC Classes  ?

  • H01M 50/244 - Secondary casings; Racks; Suspension devices; Carrying devices; Holders characterised by their mounting method
  • B60L 50/64 - Constructional details of batteries specially adapted for electric vehicles
  • B60L 53/80 - Exchanging energy storage elements, e.g. removable batteries
  • H01M 50/20 - Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders
  • H01M 50/209 - Racks, modules or packs for multiple batteries or multiple cells characterised by their shape adapted for prismatic or rectangular cells
  • H01M 50/249 - Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders specially adapted for aircraft or vehicles, e.g. cars or trains
  • H01M 50/543 - Terminals
  • H01M 50/296 - Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders characterised by terminals of battery packs