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WO/2024/108412A1 |
An alternate landing location planning method for an aircraft, comprising: acquiring an alternate landing location configuration instruction, the alternate landing location configuration instruction being used to configure an alternate l...
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WO/2024/111751A1 |
An electronic device for detecting a state of a battery included in external automation equipment according to various embodiments of the present disclosure may comprise: a processor; a communication circuit; at least one thermoelectric ...
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WO/2024/108244A1 |
The invention relates to an ice protection device (1) for aircraft (2), in particular unmanned aircraft (2), wherein the ice protection device (1) has at least one tank (7) for storing at least one deicing fluid and at least one nozzle (...
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WO/2024/110717A1 |
The invention relates to a propulsion unit (10) for an aircraft, said propulsion unit (10) comprising: - a turbine engine (14) comprising a fluidic system (18); - a cowling (16) which comprises at least one panel (20) having a longitudin...
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WO/2024/109354A1 |
The present invention relates to a ground unmanned aerial vehicle power supply network testing system and a testing method. A measurement and control channel of an engine is connected to an upper computer to transmit measurement and cont...
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WO/2024/111708A1 |
The present invention relates to an observation device for use in polar regions, which can be attached to/detached from various unmanned vehicles used in polar environments, such as the North Pole and the South Pole, and can be stably op...
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WO/2024/110189A1 |
An actuator (12) for a vehicle (2) having at least two redundant similar vehicle electrical systems (4a,b), which are each provided for full electrical working power (Aa,b) and full powerline communication (PLCa,b), contains an electric ...
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WO/2024/109328A1 |
The present utility model relates to the field of aircrafts. Disclosed are a linkage assembly, a steering gear buffer structure, and an aircraft. The linkage assembly comprises a linkage body, and the linkage body comprises a first end a...
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WO/2024/108248A1 |
The invention relates to an overhead luggage compartment for an aircraft, comprising: a luggage compartment housing (4) having two side parts (4A), an upper part (5) and a lower part (6) which enclose a receiving space (7) for luggage; a...
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WO/2024/110705A1 |
The invention relates to a fuel system for an aircraft (1) comprising at least one wing tank (5a) having at least one manifold (7), a transfer system, able to supply the manifold (7) with fuel, and a filling system, able to introduce fue...
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WO/2024/111826A1 |
The present invention relates to a grass preservation system using vegetation identification through multispectral image information and a grass preservation method using the same system, the system comprising: an unmanned aerial vehicle...
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WO/2024/110733A1 |
The invention relates to a method capable of providing information to an operator, for example a pilot, or to an automated system, for example an autopilot, to assist in managing, flight after flight, at least one cumulative ageing proce...
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WO/2024/111273A1 |
A monitoring device (50) monitors the state of a battery (151) mounted on an eVTOL. The monitoring device (50) comprises: an acquisition unit (51) that acquires information regarding the battery (151); a computing unit (52) that computes...
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WO/2024/108249A1 |
The invention relates to an overhead cabin fitting (1) for an aircraft, comprising: an overhead luggage compartment (3) for luggage; a ventilation device (4) having a housing (5), an air inlet (6), an air channel (7) and an air outlet (8...
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WO/2024/110211A1 |
The invention relates to a mechanical interface between an interior actuating handle (1) ensuring, by rotation about an axis (1a), the opening of an aircraft door, and a reserve of electrical energy intended for assisting the emergency o...
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WO/2024/108238A1 |
The invention relates to an ice protection device (1) for aircraft (2), in particular unmanned aircraft (2), the ice protection device (1) having at least one tank (7) for storing at least one deicing fluid and at least one nozzle (5), w...
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WO/2024/111658A1 |
Provided are an authentication method, a validity determination method, an aerial vehicle control method, an authentication system, and an aerial vehicle control system that make it possible to authenticate a drone with greater ease and ...
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WO/2024/109329A1 |
An aircraft and a drive mechanism thereof. The drive mechanism comprises a drive device (1), a bent connection rod (2) and a control surface (3), wherein the drive device (1) is connected to the control surface (3) by means of the bent c...
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WO/2024/111520A1 |
[Problem] To provide an unmanned aerial vehicle with which it is possible to efficiently create a turning force by means of a plurality of rotors. [Solution] An unmanned aerial vehicle comprises: a plurality of rotors for generating a th...
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WO/2024/112314A1 |
The invention relates to fluid dynamics, and more particularly to influencing the flow of a fluid passing over a body made of a solid material, and can be used for generating lift in aircraft and unmanned aerial vehicles. Claimed is a fl...
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WO/2024/111274A1 |
A battery system (15) is for mounting on an eVTOL. This battery system (15) comprises batteries (151), a supplementary battery (152), and a charge-related appliance (153). The batteries (151) supply electric power to objects to be driven...
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WO/2024/112495A1 |
Systems, apparatus, and methods are presented for testing a device. One method includes activating an actuator device to cause a. carriage, coupled to a device, to be moved in one or more directions along a guide rail, wherein the device...
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WO/2024/112321A1 |
Systems, apparatus, and methods are described herein for display stowage detection. A display device having a display screen can be disposed within a housing, such as an armrest of a vehicle. The housing can have one or more objects disp...
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WO/2024/110859A1 |
The present disclosure relates to a controlled aerial vehicle (100). The controlled aerial vehicle (100) includes a frame (102) defining housing. The frame (102) is configured to house a control module of the controlled aerial vehicle (1...
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WO/2024/111726A1 |
The present invention relates to a pilot training device for a virtual flight simulator, which is a pilot training device for a virtual flight simulator that allows a user to virtually experience the operation of controlling an elevator,...
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WO/2024/109589A1 |
A fully automated towing, alignment and hangar system suitable for an offshore operation helicopter includes a quick mooring device, a wide-angle camera installed on a rear wall of the quick mooring device, a longitudinal towing device, ...
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WO/2024/108247A1 |
The method relates to a cabin fitting (1) for a passenger cabin, comprising: - a first pivoting part (3), - a second pivoting part (4) which can be pivoted with respect to the first pivoting part (3) about a pivot axis (5) between an ope...
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WO/2024/112291A1 |
The present invention relates to a body (2); at least one engine (3) on the body (2) for generating a power required for the flight of the air vehicle; at least one air inlet (4) located as an opening on the body (2) and allowing air ent...
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WO/2024/110078A1 |
The invention relates to a conveying device for conveying cargo in an aircraft hold, comprising a flat main part which extends along the longitudinal axis of the conveying device, a main part surface which forms the top face and along wh...
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WO/2024/112772A1 |
An aircraft defining a vertical direction, a longitudinal direction, and a transverse direction is provided. The aircraft includes: a fuselage; a propulsion system comprising a power source and a plurality of vertical thrust electric fan...
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WO/2024/110720A1 |
The invention relates to a propulsion unit (10) for an aircraft, said propulsion unit (10) comprising: - an engine pylon (12), - a turbine engine (14) fixed to the engine pylon (12) and comprising a fluidic system (18), - a cowling (16) ...
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WO/2024/110718A1 |
The invention relates to a propulsion unit (10) for an aircraft, said propulsion unit (10) comprising: - an engine pylon (12), - a turbine engine (14) fixed to the engine pylon (12) and comprising a fluidic system (18), - a cowling (16) ...
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WO/2024/112190A1 |
The invention relates to an aeroplane winching system (100) for winching an aeroplane over a platform (10) having landing gear, comprising: a seat assembly (110) for seating at least part of the landing gear of the aeroplane; a winch (13...
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WO/2024/111737A1 |
An aerial drone having a coaxial motor, according to one embodiment of the present invention, may comprise: a first motor part provided in the center of a drone body so as to provide rotational power; a first blade provided at one end of...
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WO/2024/110115A1 |
An aerial vehicle comprises at least one balloon configured to receive gas having a density lower than air; at least four engines, each coupled to a propeller; a structure for fixing the engines and the at least one balloon, wherein the ...
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WO/2024/110723A1 |
The invention relates to a universal control system (1) for a trim tab of an aircraft (2) comprising a control member (3) that pivots about at least one axis of rotation (5), a main force-feedback means (9), which comprises an electric m...
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WO/2024/112582A1 |
A method and related system for regulating power to a heating device that is coupled to a discharging high voltage DC battery bank in which a voltage level of the discharging DC power source is continuously measured. Based on the measure...
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WO/2024/110929A1 |
The disclosed invention relates to a system (100) enabling mid-air payload transfer between unmanned aerial vehicles (UAVs). The system (100) includes a pair of Transfer Container Modules (TCMs) (102). Each TCM (102) includes receptacle ...
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WO/2024/110719A1 |
The invention relates to a propulsion unit (10) for an aircraft, said propulsion unit (10) comprising: an engine pylon (12), a turbine engine (14) fixed to the engine pylon (12) and comprising a fluidic system (18), a cowling (16) which ...
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WO/2024/107381A1 |
Movable platforms for use with a vehicle capture assembly of a capture vehicle and related devices, systems, and methods include floors with rotatable legs extending between the floors. The rotation of the legs relative to one or more of...
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WO/2024/103279A1 |
Provided in the present invention are a dual-rotor tilt aircraft and a flight control method therefor. The aircraft comprises: a fuselage body; a left tilt wing, which is fixed on the left side of the fuselage body; a left rotor, which i...
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WO/2024/107894A1 |
Systems and methods for performing accurate, high-resolution forest inventories within a forest environment. The systems and methods preferably make use of an unmanned aerial vehicle and a ground-based carrier for acquiring first and sec...
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WO/2024/106648A1 |
The present invention relates to a system capable of converting an air drone to a maritime or land drone, the system comprising: a drone body; a buoyancy unit which is disposed in the drone body; an image capture unit which is disposed i...
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WO/2024/107760A1 |
A power distribution system for an aircraft, comprising a plurality of electric propeller units (EPUs), includes a first paired battery pack unit comprising a first battery electrically connected to a second battery via a first high volt...
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WO/2024/107678A1 |
Systems and methods for controlling a center of gravity (CoG) of a device include one or more weights mechanically coupled to the device and operable to move along one or more body axes of the device, one or more motion sensors configure...
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WO/2024/103278A1 |
Provided in the present invention are a multi-propeller tilting aircraft and a flight control method therefor. The aircraft comprises a fuselage main body, a left tilt wing fixed on the left side of the fuselage main body, at least one l...
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WO/2024/107856A1 |
Flight vehicles having electric propulsion systems, such as "e-Wave systems," for generating acoustic waves in a plasma, and associated methods and systems are described herein. A representative flight vehicle can travel through an exter...
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WO/2024/103517A1 |
A nest (1), comprising a landing slope (11) and a stop structure (12), wherein the landing slope (11) has a landing position, and the stop structure (12) is arranged on the landing slope and is using for stopping an unmanned aerial vehic...
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WO/2024/107123A1 |
The subject of invention is aerial vehicle drive system and procedure of its use, solving these technical problems: simplified learning and memorisation of driving system; simplified visualisation of flight system parameters with alarms ...
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WO/2024/107264A2 |
A propeller according to an embodiment includes a hub and a series of blades extending outward from the hub. Each blade of the series of blades includes a core and a skin covering the core. The core may be formed of a ceramic first mater...
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