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WO/2020/107465A1 |
Disclosed are a control method, an unmanned aerial vehicle and a computer-readable storage medium. When a main power source is in a power-down state, a backup power source can be used to supply power to an unmanned aerial vehicle so as t...
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WO/2020/107373A1 |
A power assembly, a power system and an unmanned aerial vehicle. The power assembly comprises: an engine, a transmission mechanism, an electrical generator and a battery, the transmission mechanism comprising a first drive shaft and a se...
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WO/2020/107533A1 |
Disclosed is a backup statically indeterminate hanging structure of an aircraft, the structure comprising a left wall plate, a right wall plate, a hanging middle connector tab, and a lateral connecting rod. A side wall plate tab and a sh...
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WO/2020/108341A1 |
Disclosed is an aircraft landing gear comprising a landing gear bracket (1), a landing gear wheel (2) and an electric motor (3). The electric motor (3) is provided on the landing gear bracket (1).When the aircraft starts to taxi and take...
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WO/2020/107551A1 |
Provided are a protective shell (500), a motor assembly, an arm assembly and an unmanned aerial vehicle (100), wherein, the protective shell (500) is used to protect a motor (300), comprising: a buffer (510) for absorbing shock or vibrat...
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WO/2020/107407A1 |
A motor mount (400), a motor assembly, an arm assembly, and an unmanned aerial vehicle (100). The motor mount is used for connecting a motor (500) and an arm (300) of the unmanned aerial vehicle, and comprises: a mounting structure (410)...
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WO/2020/111096A1 |
[Problem] To obtain a work planning device which, on the basis of a proposed travel route along which a mobile device moves, can estimate, in advance, a plan to replenish a resource and notify a user of the same. [Solution] A work planni...
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WO/2020/104460A1 |
The invention relates to a propulsion system (10) intended to be mounted on an aircraft comprising a main body, said propulsion system (10) comprising: - a first rotating propulsive member (11) and a second rotating propulsive member (12...
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WO/2020/105337A1 |
The present invention addresses the problem of making it easy to continue control of a motor. A motor control system (10) is provided with a motor (1) and a motor control device (2). The motor control device (2) has an acquisition unit (...
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WO/2020/099138A1 |
There is provided a fitting (10) for connecting a first aircraft (20) structure to a second aircraft structure (27). The fitting (10) comprises a first substantially planar surface (11), a second substantially planar surface (12), a body...
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WO/2020/096790A1 |
In an embodiment, an apparatus includes a plurality of electrical contacts, wherein first and second electrical contacts of the plurality of electrical contacts electrically couple with a charging device; one or more rechargeable batteri...
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WO/2020/094617A1 |
The invention relates to an automated method for influencing a gust load of an aircraft (6), wherein the torque (MI) at least of an electromotive thrust generating unit (1) arranged on a wing (4) of the aircraft (6) is modified such that...
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WO/2020/097367A1 |
Devices and systems of the inventive concept provide a durable, all-weather manned or unmanned aircraft that is capable of vertical flight and provides improved stability upon payload launch or delivery. The payload bay is positioned alo...
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WO/2020/096254A1 |
A vertical takeoff and landing aircraft using a hybrid electric propulsion system and a control method therefor according to an embodiment of the present invention can: perform control such that, during vertical takeoff and landing of an...
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WO/2020/089544A1 |
In an aircraft propelled by at least one turbojet engine from which power can be drawn or into which power can be injected via a high-pressure (100, 120) and/or low-pressure (102, 122) turbine shaft and comprising at least one gas turbin...
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WO/2020/090879A1 |
[Problem] To provide a drone that operates using a fuel cell as a power source and can remain highly safe even during autonomous flight. [Solution] The present invention comprises: a flight control unit 21 that generates thrust by operat...
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WO/2020/086568A1 |
By manipulating the fluid flow in the proximity of an object such as a fuselage, a wing, or the hull of ship, the wave drag associated with this object can be substantially reduced. This can be accomplished by locally changing both the f...
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WO/2020/079935A1 |
Provided is a flying body comprising: an antenna for forming a terrestrial communication area and providing wireless communication services to user terminals in the communication area; and an attachment/detachment unit that physically at...
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WO/2020/079369A1 |
The invention relates to an engine (100) provided with a powertrain which comprises a heat engine (1) and an output shaft (A1), an electric motor (2), a battery (40) for supplying the electric motor (2) and a propeller propulsion system ...
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WO/2020/079419A1 |
The present invention relates to a multi-source aircraft propulsion arrangement comprising a cryogenic propulsion source and a combustion propulsion source wherein the cryogenic propulsion source and the combustion propulsion source may ...
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WO/2020/079934A1 |
Provided is a control apparatus controlling a plurality of flying bodies including a first flying body which forms communication area by using a beam radiated to the ground, and includes an antenna for providing a radio communication ser...
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WO/2020/079792A1 |
A propeller aircraft 1 comprising: a plurality of propellers 10a, 10b formed from fixed pitch propellers; an internal combustion engine 20 capable of generating a rotary force; an electric motor 30 capable of generating rotary force and/...
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WO/2020/074811A1 |
The invention concerns a suspension assembly (7) for a turbine engine, comprising a beam (10) intended to be attached to a pylon of an aircraft, and a cylindrical part (15) hinged to a ball-joint housing, the ball-joint housing comprisin...
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WO/2020/074812A1 |
The present invention concerns a system for supplying power to at least one electrical load of an aircraft, this system comprising a main power source (16) connected to at least one electrical load (12) via an electrical network (14), th...
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WO/2020/074810A1 |
The invention concerns a turbine engine (1) extending along an axis (X), including a high-pressure body comprising a high-pressure compressor (4) coupled to rotate with a high-pressure turbine (6), and a low-pressure body including a low...
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WO/2020/075407A1 |
A flight body 20 comprises a rotary blade 200 that generates lift or propulsion by rotating, and a rotary electric machine unit that rotates the rotary blade 200. The rotary blade 200 receives wind power and rotates when not flying. The ...
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WO/2020/077121A1 |
Aircraft spars with integrated power cells, and associated systems and methods are described. A representative aircraft wing spar includes a spar body extending in a spanwise direction, and having a plurality of apertures also extending ...
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WO/2020/070438A1 |
An aircraft (1) with hybrid thermal/electric propulsion comprising at least one turbomachine (3), at least one first electrical source (12, 31, 32), at least one second electrical source (13, 45) provided with at least one means for stor...
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WO/2020/067026A1 |
[Problem] To provide a drone system that operates using fuel cell for power and that can maintain high safety even when performing autonomous flying. [Solution] In a drone system 500, a control unit 20 mounted to a drone 100 and a fuel c...
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WO/2020/062574A1 |
Provided is a connector (30) for electrically connecting a motor (10) and an electronic governor (20), the connector (30) includes a conductive member (31) and a package body (32), the conductive member (31) is electrically connected to ...
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WO/2020/068002A1 |
The disclosure relates to a vertical take-off and landing (VTOL) aircraft comprising a body with a cockpit and a combustion engine (1), an undercarriage, two wings attached to the body comprising at least one wing support (2) and a stabi...
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WO/2020/060927A1 |
An unmanned aerial vehicle (UAV) includes one or more sources of propulsion, a power source, and communication system. The UAV also includes a controller coupled to the communication system, the power source, and the one or more sources ...
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WO/2020/060488A1 |
The application provides an autonomous refueling vehicle for a hydrogen-electric aircraft, which includes two or more wings. The wings are provided with one or more removable electric propulsion pods. The autonomous refueling vehicle inc...
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WO/2020/053502A2 |
The invention relates to a hybrid propulsion assembly (40) comprising a gas turbine (42) driving a mechanical shaft of an electric generator (44) having n phases at the output and powering an AC distribution bar (46), and a system for co...
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WO/2020/052910A1 |
A hybrid airbreathing rocket engine module (70) comprises an air intake arrangement (62) configured to receive air and a heat exchanger arrangement (63) configured to cool air from the air intake arrangement (62); a compressor (64) confi...
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WO/2020/051688A1 |
A battery-powered pilotless aerial vehicle has a center unit, a plurality of rotor units coupled to the center unit, a plurality of battery assemblies, and a plurality of electrical circuitry components including a central control circui...
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WO/2020/052102A1 |
A fire-fighting drone aiming method comprises: controlling a fire-fighting drone to fly to a fire-hit region; enabling the fire-fighting drone to hover around the fire-hit region; transmitting an image of the fire-hit region back via a g...
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WO/2020/054876A1 |
[Problem] To provide a work management system for easily recording and managing the progress state of a work process. [Solution] This work management system 1 is for managing work having a plurality of steps and has a terminal 407 wearab...
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WO/2020/049604A1 |
The present invention refers to a large multirotor rotary wing drone with the possibility of being connected to other drones of the same type by means of special connectors so as to increase the load capacity and flight time. It has a pr...
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WO/2020/044895A1 |
Provided is a control device for controlling a plurality of flying objects each having: a solar battery panel; a battery for storing power generated by the solar battery panel; and an antenna for forming a communication area on the groun...
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WO/2020/041218A1 |
Briefly, example methods, apparatuses, and/or articles of manufacture are disclosed that may be implemented, in whole or in part, to facilitate and/or support one or more operations and/or techniques for a system controller for a series ...
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WO/2020/039822A1 |
Provided is a control device that controls a flying object having a solar battery panel and an antenna for forming a communication area on the ground by using power generated by the solar battery panel and for providing a wireless commun...
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WO/2020/035042A1 |
A power supply method and device for an aircraft, a flight control system, and an aircraft. Said method comprises: determining the current flight phase of an aircraft (100); and controlling a battery (20), of which the discharge rate cor...
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WO/2020/034148A1 |
A power supply method and device. The power supply method is applied to a host device (100). The host device comprises a power supply circuit. The power supply circuit comprises a first power supply circuit (130) and a second power suppl...
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WO/2020/024423A1 |
An aircraft, a solar cell system (100), a wing (200), and a manufacturing method for the wing (200). the solar cell system (100) comprises a first encapsulation layer (2), a second encapsulation layer (3), and one or a plurality of photo...
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WO/2020/025886A1 |
The invention relates to a turbomachine with a longitudinal axis, comprising two, respectively upstream (122) and downstream, coaxial outer propellers (122), characterised in that at least some of the blades (148) of the upstream propell...
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WO/2020/027140A1 |
Provided is a system comprising a floodlight and a control device, the control device having: a floodlight position information acquisition unit that acquires floodlight position information indicating the position of the floodlight; an ...
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WO/2020/025332A1 |
A method for managing the propulsive power of an aircraft, the aircraft extending longitudinally along an axis X from the rear forwards and comprising at least two lateral propulsion systems (2) each comprising a fan, each lateral propul...
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WO/2020/022264A1 |
[Problem] To obtain a flying body with enhanced flight attitude stability through ingenious modification of the layout of constituent parts. [Solution] This flying body includes: a plurality of propellers 101-1a to 101-4b; a plurality of...
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WO/2020/022263A1 |
[Problem] To provide an aircraft with which it is possible to reduce vibrations of a fuselage by manipulating the arrangement position of the fuselage which is equipped with a control unit required by an aircraft. [Solution] The present ...
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