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WO/2023/152147A1 |
The invention relates to a method for diagnosing a state of deterioration of an uplock comprising an unlocking actuator 12, 22 provided with a hydraulic cylinder (Ve), the method comprising the following steps: • a) supplying the cylin...
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WO/2023/133003A1 |
Methods, systems, and devices for wireless communications are described. A user equipment (UE) may be aboard an aerial vehicle such that the UE is above ground, and in some cases, moving above ground (e.g., flying). The UE may determine ...
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WO/2023/124124A1 |
A method for controlling a deformable rolling aircraft. The method comprises the following steps: after a control system receives a starting signal, a driving device (5) driving a rotor wing to rotate, and the rotor wing generating a lif...
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WO/2023/126594A1 |
The present document relates to a device (100) for electrically discharging a part of a turbine engine, said device comprising a sleeve (102) capable of receiving said turbine engine part and at least one handling arm (106) mounted on sa...
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WO/2023/124125A1 |
A deformable rolling aircraft, comprising: a base body (1), a first wing portion (21) and a second wing portion (22), two rotors arranged in parallel being provided in each of the first wing portion (21) and the second wing portion (22);...
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WO/2023/119930A1 |
A control device (50) is for controlling an electric vertical takeoff and landing aircraft (100), and in the case where the magnitude of a magnetic field detected by a magnetic sensor (70) provided to the electric vertical takeoff and la...
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WO/2023/119298A1 |
An unmanned aerial vehicle (UAV) is disclosed. The UAV comprises a body; a propulsion unit; a controller; and at least one adjustable camera unit. In some embodiments, each adjustable camera unit comprises, a camera; and a gimbal, mounti...
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WO/2023/118745A1 |
The invention relates to an assembly for an aircraft turbomachine (2), the assembly comprising: - a nacelle (1) comprising a fixed structure (11, 15, 16) that is suitable for being arranged around the turbomachine (2) comprising an inner...
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WO/2023/118746A1 |
The invention describes an assembly for an aircraft propulsion system (2), comprising: - a nacelle (1) delimiting, together with the propulsion system (2), a fire zone (100, 200); - a fire extinguisher (3) comprising a nozzle (36) for sp...
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WO/2023/113058A1 |
Disclosed is a drone control method for precise landing. The drone control method according to an embodiment of the present invention may comprise the steps of: when a drone is switched to an arming mode in a drone station, setting curre...
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WO/2023/107541A1 |
A tray table indicator includes a channel, a cover, and a magnetic ball. The channel has a first extension, a curve, and a second extension, and the cover encloses the channel. A magnetic ball is contained within the channel and is movab...
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WO/2023/104777A1 |
The invention relates to a method for checking the maximum power available to members of a propulsion system of an aircraft (1) comprising first members (M1.1, M2.1, D10, TG, BAT1) that are sized to compensate for the failure of second m...
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WO/2023/101757A1 |
A multicopter rotor fault diagnosis system includes a multicopter, a plurality of local sensors, and a controller. The multicopter includes a body, a plurality of booms secured to the body, and a plurality of rotors. Each boom has a prox...
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WO/2023/100133A1 |
A control unit (46, 46') for an aircraft (1, 1') capable of hovering or for a flight simulation system of the aircraft (1, 1') is described, the control unit (46, 46') is programmed to receive at input at least a first signal associated ...
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WO/2023/100150A1 |
A control unit (46, 46') for an aircraft (1, 1') capable of hovering or for a flight simulation system of the aircraft (1, 1') is described; the control unit (46, 46') is programmed to: - receive in input a plurality of data associated w...
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WO/2023/096414A1 |
A reusable airbag inflator according to an embodiment of the present invention may be provided, the inflator comprising: a gas cartridge mounted with an opening/closing valve which can be opened or closed to discharge compressed gas stor...
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WO/2023/094587A1 |
The present invention is related to a remotely-controlled flying device intended to approach and contact a high-voltage overhead power line for operation thereon, said flying device comprising : - a mechanical structure (1) bearing a plu...
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WO/2023/091235A2 |
The present invention is a system and methods for preconditioning a power source of an electric aircraft. The system may include a sensor attached to a power source of an electric aircraft, where the sensor is configured to detect a cond...
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WO/2023/090465A1 |
Provided is a drone comprising: a body, which is connected to a plurality of arms and includes propellers provided at each of the plurality of arms; a driving part for supplying propulsive power to the propellers provided at each of the ...
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WO/2023/082282A1 |
The present application provides a control method, a control device, and an unmanned aerial vehicle. The method comprises: obtaining a flight state of an unmanned aerial vehicle, wherein the flight state at least comprises at least one o...
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WO/2023/080172A1 |
[Problem] The present invention pertains to a system that is capable of remotely managing and remotely controlling a flying object from outside. [Solution] A manned flying object control system according to the present technology compris...
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WO/2023/079965A1 |
Provided is a flight control device that performs a flight control process for flying an aircraft. If a collision between the aircraft and another craft is predicted, this flight control device performs a discovery and avoidance process ...
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WO/2023/079964A1 |
This flight control device performs flight control processing for causing an eVTOL to fly. The flight control device sets an operating mode to one of a plurality of failsafe modes in accordance with which of a plurality of normal modes t...
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WO/2023/076708A1 |
An aerial robot may include a distance sensor and visual inertial sensor. The aerial robot may determine a first height estimate of the aerial robot relative to a first region with a first surface level using data from the distance senso...
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WO/2023/067651A1 |
The present invention comprises: a distance acquisition unit (115) that detects the separation distance between an aerial vehicle (V1) and a platform (51); a remaining charge acquisition unit (113) that acquires the remaining charge of a...
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WO/2023/068041A1 |
[Problem] To provide: a safety device which enables rapid expansion of a float, which has sufficient buoyancy at the time of contact with water, and which has reduced weight compared to prior art; and an aircraft comprising this safety d...
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WO/2023/067653A1 |
An aerial vehicle control device (1) for controlling an aerial vehicle that flies over water, said device comprising: a crash detection unit (31) for detecting that the aerial vehicle has crashed into the water; and an acoustic wave outp...
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WO/2023/062675A1 |
Provided is a drone protection system for protecting a drone 2 from thunderstroke, the drone protection system comprising a Faraday cage 1 which surrounds the drone 2 and a wire 3 which can move on the Faraday cage 1 while an end portion...
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WO/2023/064188A1 |
The disclosed invention describes a method for determining a current state of a gas cell in an airship, particularly the lift. A computing device receives depth measurements of the interior of the gas cell using a lidar sensor positioned...
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WO/2023/059427A1 |
The systems/methods analyze the vast reservoir of data that is collected in-flight during a commercial aircraft's travels over several months. That data is analyzed to identify and remove data points that do not represent stable cruise. ...
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WO/2023/057198A1 |
A signal transmitter apparatus configured for use in an aircraft moveable element monitoring system. The signal transmitter apparatus comprising a signal transmitter circuit. The signal transmitter circuit comprises: a first electrical p...
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WO/2023/055878A1 |
A smart landing platform system includes a flat and rigid platform for landing a drone and having a geometrical center, a center of gravity and a weight, a digital scale disposed beneath the platform for providing measurements of a weigh...
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WO/2023/052459A1 |
The present disclosure provides a coated aircraft propulsion system component, in particular an aircraft blade, comprising a coating applied to at least a part of said aircraft propulsion system component, wherein said coating comprises ...
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WO/2023/044535A1 |
An emergency interface system for an autopilot system has an actuator mechanically interfacing an actuator switch, the actuator throwing the actuator switch when operated. The actuator switch has an actuator output connected to an input ...
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WO/2023/036897A1 |
A method for unlocking a door (20) of an aircraft landing gear movably mounted between an open position and a closed position, the door (20) being associated with attachment means comprising a first attachment housing (23.1) and a second...
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WO/2023/022098A1 |
[Problem] To provide an inspection system with which it is possible to achieve the accuracy of detection suitable for the maintenance of structural soundness while reducing costs by circuit simplification and suppressing an interference ...
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WO/2023/015233A1 |
Landing pads for a drone. One of the landing pads can include a landing area with a first surface configured to receive a second surface of a landing gear of a drone; a docking area i) with a first end adjacent to the landing area and a ...
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WO/2023/009801A1 |
A rapidly disassembled hinge suitable for use in an aircraft includes a first attachment plate attached to a supported structure, a second attachment plate attached to a supporting structure, and a pin with a notch in an outer surface th...
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WO/2023/010103A1 |
Disclosed herein are methods, devices, and systems for facilitating pilots in determining current and predicted performance specifications of their aircraft. According to one embodiment, a method is implemented on a mobile computing devi...
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WO/2023/003336A1 |
A drone integrated control apparatus for controlling a drone, in which each component of the control apparatus is integrated on a single board, is characterized by comprising: a flight control unit which has a plurality of sensors and co...
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WO/2023/002131A1 |
The invention relates to a system (200) for the thermal management of an external electric-power-generating nacelle equipping an electrically powered airship, said nacelle comprising electrical generation means implementing at least one ...
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WO/2023/004119A1 |
A battery module includes a plurality of electrically connected cells. These cells may, in turn, include a parallel, series, or combination of both, collection of electrochemical or electrostatic cells hereafter referred to collectively ...
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WO/2023/281180A1 |
The invention relates to a three-dimensional electroconductive mat formed of an electroconductive knitted fabric capable of homogeneously distributing electrical charges over the entire surface thereof, characterised in that the knitted ...
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WO/2023/272489A1 |
A propeller and an unmanned aerial vehicle. The propeller comprises: a hub (10); blades (20) connected to the hub (10), the blades (20) each comprising a connecting end connected to the hub (10), and a tail end distant from the hub (10);...
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WO/2023/274914A1 |
In order to reduce maintenance work and to improve long-time reliability, the invention provides a health monitoring method for checking a functionality of a flight control surface driving apparatus (104) using at least one load sensor (...
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WO/2023/277657A1 |
Disclosed is a transmission line construction method using wire pulling and wire tensioning, by which, after measuring a coordinate point of a power line connection hole of a transmission line tower by using a drone, a power line is cut ...
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WO/2023/274913A1 |
In order to reduce maintenance work and to improve long-time reliability, the invention provides a health monitoring method for checking a functionality of a flight control surface driving apparatus (104) using at least one load sensor (...
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WO/2022/270856A1 |
The present invention relates to a drone having a laser beam emission function, wherein a laser beam may be emitted during fight, and thus, a visible range of a place for landing may be easily checked with the naked eye through the emiss...
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WO/2022/263365A1 |
The invention relates to an on-board system for detecting impacts on the fuselage (110) of an aircraft (100), comprising: a plurality of impact sensors (2) arranged on a plurality of areas of the fuselage, each sensor (2) being capable o...
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WO/2022/261864A1 |
A control method and apparatus for an unmanned aerial vehicle system, and an unmanned aerial vehicle system and a storage medium. The unmanned aerial vehicle system comprises an unmanned aerial vehicle and a parachute mounted on the unma...
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