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WO/2020/130333A1 |
The present invention relates to a vertical take-off and landing type hybrid drone comprising: a pair of front rotary rotors, which are formed on a fixed blade, perform a vertical rotation operation so that vertical taking-off and landin...
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WO/2020/129344A1 |
The purpose of the present invention is to provide a cable used to at least moor a moving body to be moored and supply power thereto, such that weight of the whole cable can be reduced. This cable (1) is a cable used to at least connect ...
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WO/2020/121671A1 |
A motor-integrated fan 1 including one or more motors integrated therein comprises: a shaft part 11 which serves as a supporting system disposed at the center of a rotational axis; a rotation part 12 which is a rotating system rotating a...
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WO/2020/122056A1 |
The present invention provides a motor-integrated fan that suctions air through a suction port and blows out the suctioned air through a blow-out port, wherein: the motor-integrated fan comprises a shaft part provided in the center of a ...
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WO/2020/121582A1 |
[Problem] To provide a flight body comprising a multicopter mechanism, the flight body having both a vertical takeoff and landing function and a horizontal circling function, and also having exceptional circling capability. [Solution] In...
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WO/2020/122077A1 |
[Problem] To provide a motor cooling structure capable of improving cooling efficiency when cooling a motor that has reached a high temperature. [Solution] In the motor cooling structure equipped with a motor disposed on a board and a pr...
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WO/2020/121067A2 |
A metal air battery electrolyte replenishment system comprised of a base station with docking receptor apparatus and matching docking probe on a flying drone. The probe onboard the drone has a sensor that guides the drone to connect with...
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WO/2020/122433A1 |
The present invention relates to a drone provided with a foldable rotary wing and, more specifically, to a drone (an unmanned aerial vehicle) provided with a foldable rotary wing, wherein the wing of the drone can be folded through a sim...
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WO/2020/116492A1 |
[Problem] Through cooperative operation of a drone and a movable body which is movable with the drone loaded thereon and at which takeoff and landing of the drone is allowed, high safety can be maintained even when the drone performs aut...
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WO/2020/116396A1 |
[Problem] Through cooperative operation of a drone and a movable body which is movable with the drone loaded thereon and at which takeoff and landing of the drone is allowed, high safety can be maintained even when the drone performs aut...
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WO/2020/116442A1 |
[Problem] To provide a configuration in which a drone and a moving body that can move with the drone loaded thereon and that enables the drone to take off therefrom and land thereon operate together, and a high degree of safety can be ma...
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WO/2020/116496A1 |
[Problem] To provide a system in which a drone and a moving body that can move with the drone loaded thereon and that enables the drone to take off therefrom and land thereon operate together, and a high degree of safety can be maintaine...
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WO/2020/116443A1 |
[Problem] To cooperatively operate a drone and a movable body which can move while loading the drone thereon and on which the drone can take off and land, and to be capable of maintaining high safety even when the drone autonomously flie...
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WO/2020/116493A1 |
[Problem] To achieve coordinated operation of a drone and a moving body which can move with the drone loaded thereon and from which the drone can take off and land, and to maintain a high degree of safety even when the drone flies autono...
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WO/2020/116341A1 |
[Problem] To enable a high level of safety to be maintained even when a drone and a moving body, which is capable of moving with the drone carried thereon and on which the drone can takeoff and land, operate in cooperation and the drone ...
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WO/2020/116392A1 |
[Problem] Through cooperative operation of a drone and a movable body which is movable with the drone loaded thereon and at which takeoff and landing of the drone is allowed, high safety can be maintained even when the drone performs aut...
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WO/2020/116925A1 |
A drone takes off and lands vertically in the same way that an existing drone takes off and lands. The drone has a foldable wing portion to which a solar cell panel is attached, and when reaching a predetermined height, the drone unfolds...
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WO/2020/055220A9 |
A self-propelled vehicle which can be configured in the form of an aircraft and comprises a central system of compartments, working members, and a drive comprising the following components: a source of energy, a transmission mechanism, c...
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WO/2020/116444A1 |
[Problem] The present invention addresses the problem of enabling a drone to operate in cooperation with a mobile unit that is mobile with the drone mounted thereon and that allows the drone to land thereon and to take off therefrom, in ...
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WO/2020/116494A1 |
[Problem] To provide a system in which a drone and a moving body that can move with the drone loaded thereon and that enables the drone to take off therefrom and land thereon operate together, and a high degree of safety can be maintaine...
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WO/2020/113386A1 |
An electronic speed controller, a power device, and an unmanned aerial vehicle. The electronic speed controller is mounted on the outside of an arm, and comprises a first housing (611), a second housing (612), a circuit board (620), a fi...
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WO/2020/116495A1 |
[Problem] To provide a system in which a drone and a moving body that can move with the drone loaded thereon and that enables the drone to take off therefrom and land thereon operate together, and a high degree of safety can be maintaine...
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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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