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WO/2024/059189A1 |
Systems and methods relate to a vertical takeoff and landing (VTOL) platform that can include a stator and a rotor magnetically levitated by the stator. The rotor and stator can be annular, such that the rotor rotates about a rotational ...
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WO/2024/058566A1 |
The present invention relates to a way to prevent the deterioration of batteries in drones, and in particular, provides a power distribution circuit for preventing the deterioration of a battery due to an instantaneous high output power ...
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WO/2024/057746A1 |
An operation control unit 11 controls a flight drive mechanism 1009 so as to perform an operation by which detection values of respective sensors included in a sensor group 1007 provided to a drone 10 match target values. A detection uni...
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WO/2024/058872A1 |
A waterproof UAV that records camera footage while traveling through air and while submerged in water. The UAV alters speed and direction of propellers dependent on the medium that the UAV is traveling through to provide control of the U...
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WO/2024/056878A1 |
The invention relates to a glazed system (100, 200, 300) comprising a glass panel (110) comprising structural plies (111, 112), the glass panel being clamped in place by a structure. Said glazed system further comprises: - at least one b...
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WO/2024/056971A1 |
The present application relates to a method for calibrating a model for estimating a torque supplied by an electric machine (10), which comprises the following steps: (E1) measuring an electric current in the electric machine (10) for an...
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WO/2024/055499A1 |
An anti-false-touch safety switch (7), a locking mechanism (100), and a locking system, relating to the technical field of aviation machinery. The anti-false-touch safety switch (7) comprises: a rotary locking member (71), used to be in ...
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WO/2024/058619A1 |
The present invention relates to an airship capable of easily switching directions, the airship comprising an aerial vehicle (mother ship) formed in a disc or polygonal shape provided with a jet engine, a rotating body having a jet engin...
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WO/2024/056879A1 |
The invention relates to a glazed system (100, 200, 300) comprising a glazing (110), for example a laminated glazing, comprising structural folds (111, 112), the glazing being clamped in place by a structure. Said glazed system further c...
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WO/2024/056836A1 |
The present disclosure relates to vertical takeoff and landing aerial vehicles configured to transport a payload. The vehicle comprises a main lifting body and a propulsion assembly coupled to the main lifting body. The main lifting body...
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WO/2024/059347A1 |
A system having components coupled to an aircraft that measure the navigational state and state uncertainty of an aircraft. To do so, the aircraft captures an image of its surrounding environment including an object of interest and appli...
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WO/2024/058620A1 |
The disclosure relates to a 5G or 6G communication system for supporting a higher data transmission rate. A UE in a 5G or 6G communication system for supporting a higher data transmission rate that may efficiently report a flight path of...
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WO/2024/057287A1 |
A deployable boom mechanism, such as for a spacecraft, has a boom and a boom drum. The boom can be wound onto the boom drum. The boom drum is rotatable in a deployment direction to deploy the boom by unwinding it from the boom drum. A dr...
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WO/2024/057825A1 |
[Problem] To provide a drone device for coating and a coating method capable of performing maintenance coating safely and inexpensively. [Solution] The drone body part 10 has an IMU 15 that acquires the tilt angle of a drone device 1, a ...
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WO/2024/057034A1 |
The present disclosure comprises a portable support (1) positionable on a seat (5). The support (1) comprises a frame (2) and a flexible material (3) extending across the frame (2). The frame (2) is configured to support the flexible mat...
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WO/2024/059181A1 |
Systems and methods relate to a vehicle, such as a vertical takeoff and landing (VTOL) platform, which can include a stator and a rotor magnetically levitated by the stator. The rotor and stator can be annular, such that the rotor rotate...
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WO/2024/058565A1 |
The present invention relates to a method for preventing drone battery degradation, and in particular, provides: an apparatus for preventing battery degradation caused by a momentary high output exceeding the rating of the battery, where...
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WO/2024/059215A1 |
A method includes receiving configuration data for an unmanned aerial vehicle (UAV) simulation system, the configuration data indicating at least one base location specification, at least one aircraft specification, and at least one virt...
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WO/2024/055899A1 |
A connector and method for connecting a motor and an arm of a multi-rotor aircraft. The connector comprises a base (1), a locking disk component (2), and a guided positioning component (3), wherein one side of the base (1) is connected t...
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WO/2024/058887A1 |
The present invention is directed to systems and methods for aerially detecting and identifying explosives on the ground, and more specifically systems and methods for detecting and identifying landmines and unexploded ordnance (UXO) on ...
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WO/2024/056959A1 |
The invention relates to a propeller blade or vane (10) for a turboprop engine, made from composite material and comprising a matrix-densified fibrous reinforcement, the propeller blade or vane comprising, in the direction of its span (D...
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WO/2024/055069A1 |
Provided is a hybrid aerial hydro drone (10) comprising a body (12) with a plurality of hydraulic thrusters (14) supported on an outer surface of the body (12) and configured to propel said body (12) in a marine environment. Drone (10) a...
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WO/2024/059230A1 |
An aircraft boarding vehicle to transport passengers between airport gate area and to a front door or a rear door of an airplane positioned on a tarmac of an airport without impeding ground transportation and plane traffic having a passe...
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WO/2024/055506A1 |
The present invention relates to the field of aviation machinery. Provided is a locking mechanism used for a helicopter tail cabin door. The locking mechanism comprises: two lock box assemblies, respectively installed on two sides of a t...
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WO/2024/056195A1 |
The present invention concerns a device for a multicopter that allows the multicopter to move without tipping over. This device generates propulsion according to the x- and/or Y-axis using the air displacement of the drive propellers and...
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WO/2024/057935A1 |
Provided is a rotary wing that is unlikely to be deformed by fluid. A rotary wing 1 comprises: a hub 10; a first blade 20, a second blade 30, and a third blade 40, being a plurality of blades which each have one end connected to the hub ...
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WO/2024/059113A1 |
A method of imparting anti-icing characteristics to an article includes combining a part A composition with a part B composition and a part C composition to form a ready-to-use composition; applying the ready -to-use composition on at le...
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WO/2024/059777A1 |
Conventional proprotor systems have a large region in the middle of the proprotor disk area that is occupied by the hub mounted systems including blade pitch control systems and blade retention systems. The hub-mounted systems use rotor ...
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WO/2024/055900A1 |
The present invention relates to the technical field of unmanned aerial vehicles, and provides a battery management system having a plurality of backup communication main units, and an aircraft. In the battery management system provided ...
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WO/2024/055381A1 |
A perching robot and a perching method of the perching robot. The perching robot relates to the technical field of robots, and comprises: a body (101), a control unit, a perching module (102) and a data acquisition unit (103); the contro...
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WO/2024/056549A1 |
The present invention relates to a system (10; 20; 30) for reconfiguring power distribution in an aircraft, the system comprises at least two propulsion units (3), at least two energy storage units (13) and an interconnecting network (15...
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WO/2024/056258A1 |
The invention relates to an item of furniture (30), in particular for an aircraft seat, comprising: -a frame (31), - a movable element (26), - a pivot connection (34) for rotating the movable element (26) relative to the frame (31) betwe...
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WO/2024/056929A1 |
The present invention relates to a smart device (100) for supplying ammonia and hydrogen for mixed combustion in aircraft, as shown in Figure 1, for propulsion. The smart device comprises a subassembly (120) that stores ammonia and suppl...
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WO/2024/052616A1 |
The invention relates to an actuator (20) designed to be connected to a mechanical flight control chain (13) of a vehicle, comprising a motor (22), a first output shaft (23) driven in rotation by the motor (22) about an axis of rotation ...
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WO/2024/054818A1 |
An unmanned vehicle includes at least one navigation sensor configured to measure navigation data indicative of an environment, at least one status sensor configured to measure status data indicative of operating parameters of a hardware...
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WO/2024/050585A1 |
The invention relates to a luggage compartment (1) for an aircraft, comprising: a luggage-compartment housing (2); a chute (6) for receiving an item of luggage (13); a joint (10) between the luggage-compartment housing (2) and the chute ...
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WO/2024/052286A1 |
The invention relates to a protective device (6) for protecting a protruding aerial part (3) of an anemobarometric sensor (1) comprising a sleeve (7) configured to protect said protruding part (3), a grab handle (8) comprising a bar that...
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WO/2024/054833A1 |
An unmanned aerial vehicle comprises a central body; at least one rotor motor configured to drive at least one propeller to rotate, rotation of the at least one propeller generating thrust and causing the unmanned aerial vehicle to fly; ...
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WO/2024/053047A1 |
The present invention comprises at least one processor that outputs information about a mission on a celestial body other than the Earth by executing the processing corresponding to the operation by a user in accordance with the operatio...
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WO/2024/053375A1 |
Provided are a flight device and a method for controlling the same, by which it is possible to accurately measure the power remaining in a battery with a simple configuration. A flight device 10 is provided with a rotor 11, a motor 12,...
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WO/2024/052237A1 |
The invention relates to a hybrid metal/plastic spring rod (1) comprising a guiding system (3) made up of a metal pin (4) and a plastic sliding body (5), a compression spring (2) and two plastic-moulded connecting members (6a, 6e). The c...
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WO/2024/052190A1 |
During the transition of a vertical take-off and landing (VTOL) aircraft (1) from hover flight to cruise flight and vice versa, a method for controlling this transition is configured to push propulsion units (2) of the VTOL aircraft (1) ...
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WO/2024/054197A1 |
The invention relates to space engineering and can be used in the creation of a suborbital rocket plane with substantially vertical takeoff and landing. A rocket plane comprises a body (1), movable front and rear aerodynamic control surf...
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WO/2024/052505A1 |
The invention relates to a wing arrangement (10) that comprises a main wing (12) and a slat (14) mounted to the main wing in front of the main wing (12) and counter to a direction of flow. A gap (16) with a flow inlet (18) and a flow out...
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WO/2024/054310A2 |
A method may include a first UAV of a plurality of UAVs flying a first vector comprising a first heading and speed; a second UAV of the plurality of UAVs flying a second vector comprising a second heading and speed; at a first time, whil...
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WO/2024/053327A1 |
Provided are a flying device and a control method therefor capable of suppressing a flight in a state in which the weight of a transported body is excessively large. A flying device 10 comprises a fuselage base portion 16, a rotor 11, ...
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WO/2024/054195A1 |
A closed-wing vertical take-off and landing aircraft comprising: a fuselage (1); a tail unit comprising two angularly inclined stabilizers (12); and a closed wing, comprising a front wing formed by two planes (2) mounted to the fuselage ...
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WO/2024/050552A1 |
Devices, systems and methods that are configured to use image processing to detect structural changes in infrastructure assets are described. An example method for identifying damage in an infrastructure asset includes receiving multitem...
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WO/2024/050178A2 |
A unmanned aerial vehicle (UAV) includes a fuselage including a top, a. bottom, a cavity that forms a cargo bay between the top and the bottom, and a lower access opening in the bottom for lowering a payload from the cargo bay. A movable...
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WO/2024/046666A1 |
The invention relates to a seat unit (10) for a transport vehicle comprising - a seat comprising a seat-base and a backrest (12.2), - an induction charging housing (30) for a portable electronic device (31) having a vertical orientation,...
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