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WO/2024/043207A1 |
Provided are an aircraft coating removal device and method. The device comprises: a travel cart that can move; a blast head that is mounted on the travel cart and that can spray a blast material; a raising/lowering device that can move t...
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WO/2024/040482A1 |
A gimbal, a gimbal camera (400) and an unmanned aerial vehicle. The gimbal specifically comprises: a first driving mechanism (10), which is used for driving a photographing device (20) to rotate about a first rotary shaft; a base (11), w...
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WO/2024/041370A1 |
The present invention relates to the technical field of aircrafts. Disclosed are an aircraft state indication method, an aircraft, and a storage medium. The aircraft state indication method comprises: when a preset condition is satisfied...
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WO/2024/042293A1 |
The present application relates to a blade (3) of a static vane assembly (2) of a turbine engine (1) comprising: - a blade root (8) comprising a fibrous reinforcer (13) comprising a first skin (12) and a second skin (12) separated by a c...
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WO/2024/044220A1 |
Embodiments are directed, to low-profile, low-weight cargo loader, including a pair of cargo loaders including a first cargo loader arranged in tandem with a second cargo loader in a first orientation..According to an embodiment, each of...
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WO/2024/043093A1 |
This prediction device (20) predicts the required performance and/or state of a battery, which is a driving apparatus installed in an eVTOL. The prediction device (20) comprises: an acquisition unit (21) that acquires information includi...
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WO/2024/041934A1 |
The invention relates to a device (1) for cleaning fuel in a tank (92) of an aircraft (90), and use thereof. The device has a predetermined flow direction (2) for the fuel and comprises units arranged in a fluid-connected manner to forwa...
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WO/2024/042309A1 |
Air data estimation involves determining values of air data parameters such as airspeed, altitude, angle of attack and angle of sideslip. Accurate determination of air data parameter values is crucial to enable accurate control of an air...
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WO/2024/040466A1 |
A flight control method, an apparatus, an unmanned aerial vehicle, and a storage medium. The method comprises: in a flight state, determining whether a collision of an unmanned aerial vehicle occurs (31); and, when it is determined that ...
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WO/2024/039824A1 |
Systems and methods for flight control on an electric aircraft. The system includes a propulsor configured to generate lift to propel an electric aircraft, a pilot input mechanically coupled to the electric aircraft, a sensor communicati...
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WO/2024/037831A1 |
The invention relates to an air data indicating and calibrating arrangement (1) and method for a vertical take-off and landing aircraft, in particular a helicopter (50), for providing information on an air speed of the vertical take-off ...
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WO/2024/038247A1 |
A fuel delivery device for air-to-air refuelling, the device comprising: a fuel outlet; and an optical transceiver, wherein the optical transceiver is configured to: illuminate the fuel delivery device to provide visual indication to an ...
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WO/2024/038249A1 |
A flow body unit (600) for a fluid flow rig (10) for simulating fluid flow patterns; the flow body unit (600) comprising: a flow body support frame (700); a core member (800) extending from the flow body support frame (700) along a flow ...
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WO/2024/039423A1 |
A linear actuation system includes a pin pivotably coupled to an output rod of a linear motion actuator and a rotatable output shaft that includes a bushing therein. The pin can be configured to slide in and out of the bushing in respons...
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WO/2024/038189A1 |
The present invention relates to a system (40) for redistributing power in an aircraft with at least two electrical powertrain units (10), each powertrain unit (10) comprises a propulsion unit (15) powered by an energy storage unit (13);...
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WO/2024/038634A1 |
Provided is a flight method that makes it possible to prevent a collision of a drone and entanglement of a power supply cable. This flight control system relating to flight control of an electrically driven drone 3 that is connected to a...
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WO/2024/038756A1 |
In a passive radar satellite 1, one or a plurality of radar openings 18 are attached to a satellite bus unit 14 by way of a radar opening drive device 17 having a variable attachment angle, wherein: in the radar openings 18, one or a plu...
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WO/2024/037875A1 |
The invention relates to a pivoting wing (1) for an aircraft (13), characterised in that the pivoting wing (1) is designed as a partial profile pivoting wing, wherein the partial profile pivoting wing is assembled from individual partial...
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WO/2024/038362A1 |
Provided is a vertical take-off and landing unmanned aerial vehicle (VTOL UAV) comprising a body, a pair of wings pivotably attached to the body with at least one pair of front rotors mounted on the wings, a rear rotor pivotably attached...
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WO/2024/038489A1 |
[Problem] The ability to acquire information useful for the flight of an aircraft is demanded. [Solution] In the present invention, terminal devices 600 provided in the cabin space of a target aircraft 810 each comprises a sensor unit 68...
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WO/2024/038463A1 |
A flight mode transitioning device, method and system configured to facilitate transitioning between vertical flight mode and horizontal flight mode in a vertical take- off and landing (VTOL) aircraft, the device comprising at least one ...
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WO/2024/038047A1 |
A power transmission system (20) for a propeller hub of an aircraft is described, wherein the power transmission system comprises a hollow inner conductive cylinder (4) configured to be mounted to a rotatable shaft a hollow outer insulat...
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WO/2024/038582A1 |
An unmanned aerial vehicle according to the present invention comprises: an anchoring member which is capable of anchoring an article; a linear member which is connected to the anchoring member; and a reel on which the linear member is w...
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WO/2024/038696A1 |
Provided are a device and a method for attaching an aircraft engine comprising: a linear movement device that supports a support frame, by which an aircraft engine is supported along the horizontal direction, so as to be movable along a ...
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WO/2024/038548A1 |
[Problem] To provide a spacecraft that has an improved heat discharging capability. [Solution] A spacecraft (1) according to one embodiment of the present invention comprises: a body (300) which has mounted therewithin multiple devices i...
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WO/2024/038811A1 |
A conveyance control method according to one aspect of the present disclosure is a method for lifting and conveying cargo via a plurality of flexible cables by using a plurality of unmanned aerial vehicles, each of which is capable of ge...
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WO/2024/035885A1 |
A craft comprises at least one hull, at least one wing configured to generate upwards aero lift as air flows past the at least one wing to facilitate wing-borne flight of the craft, at least one retractable hydrofoil configured to genera...
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WO/2024/032113A1 |
Provided in the present invention are a self-driving early-warning unit and early-warning method for stall of a moving body. The early-warning unit comprises: a triboelectric sensing unit, which comprises a friction electrode layer and a...
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WO/2024/033345A1 |
The artefact comprises a flat or curved body substantially made of metal or metal alloy or composite material and comprising one or more ice protection panel(s). The ice protection panel(s) comprise a heater film and at least one ply mad...
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WO/2024/033587A1 |
The invention relates to an assembly for a turbine engine, in particular of an aircraft, the assembly comprising a ring (2) with a rotationally symmetrical axis (O). According to the invention, the assembly comprises a plurality of suppo...
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WO/2024/035451A1 |
A method includes obtaining (402) thermal energy from a structure (112) to be cooled, where the structure includes micro-channels (208). The method also includes providing (402) the thermal energy to a water-based polymer network (206), ...
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WO/2024/033532A1 |
This disclosure relates to a carrier device (100) for securing a payload in spacecraft, having a carrier surface (102), the carrier surface (102) being provided with an arrangement of local resonators (108), which each comprise at least ...
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WO/2024/035711A1 |
An aircraft indudes a fuselage, a forward wing assembly, a mid-body wing assembly, and an aft wing assembly, and a hybrid propulsion system. The hybrid propulsion system includes a plurality of primary thrust assemblies and a plurality o...
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WO/2024/033432A1 |
A method (700) by a user equipment, UE, (112) for communicating in a restricted zone includes determining (702) a location of the UE in relation to the restricted zone. Based on the location of the UE in relation to the restricted zone, ...
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WO/2024/032907A1 |
An electric vertical take-off and landing aircraft comprises a fuselage (1) and a tilt wing (7). The tilt wing (7) is tiltable relative to the fuselage (1) in a range of tilt wing angles. Control surfaces (13) are arranged at the tilt wi...
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WO/2024/033594A1 |
The invention relates to a method for assisting with propulsion by detecting a failure of a turboshaft engine of an aircraft operating in a nominal mode, the aircraft comprising a deactivated assistance motor, which method comprises a st...
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WO/2024/033590A1 |
The invention relates to a propeller (10) for an aircraft turbine engine, this propeller (10) having: - a hub (12), - vanes (14), - bearings (46, 48) for guiding the roots (18) of the vanes (14) into orifices (12a) in the hub (12), and -...
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WO/2024/033166A1 |
A device for subdividing a passenger cabin (1) of an aircraft, comprising a wall element (2). The wall element (2) has a fastening element so that it can be fastened to at least one element of the passenger cabin (1) in such a way that t...
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WO/2024/031120A1 |
A locking device (1) for locking a pivotably mounted door (21) of a container (20) in the closed position, with a housing (2), at least one hook (3) for hooking into a holder shaft (26), and an actuating handle (4) for unlocking the hook...
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WO/2024/033468A1 |
A computerized system of controlling a bag-drop process via a mobile device is provided. The system is arranged to create a virtual zone in front of a bag-drop station using signal emitter(s) located at the bag-drop station. Signals emit...
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WO/2024/033273A1 |
According to one aspect, the present disclosure relates to a device for reducing the electric charge of a space vehicle, the device comprising: a substrate (201) made of a conductor or semiconductor which is configured to be electrically...
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WO/2024/035714A1 |
A compact and lightweight, drone delivery device propelled by an electric ducted air propulsion system. The device is called an ArcSpear Electric Jet Drone System and is relatively di f ficult to track in flight ( stealth), relatively fa...
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WO/2024/034498A1 |
Provided is a robot arm in which a first sensor detects the posture of a flying robot. The robot arm has a control unit that controls a second drive module, on the basis of a detection signal from the first sensor, and that thereby cause...
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WO/2024/035019A1 |
The present invention relates to a low-impact landing system for a rotary wing aircraft for reducing landing impact transmitted to an airframe (11) upon landing of a rotary wing aircraft (10), comprising: a landing platform (110) having ...
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WO/2024/034419A1 |
This protection device comprises an outer shell container, a protective body, and a driving unit. The protective body is provided with: frame assemblies that each include at least two frames which are disposed at a distance from each oth...
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WO/2024/033589A1 |
The invention relates to an electrical system (100) having: - an electric circuit (102) having a electrically insulating flat support (104) and two electric conductors (106, 108) secured to the flat support, the two electric conductors (...
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WO/2024/033430A1 |
The invention relates to a passenger seat device comprising a stand unit (14a; 14b), a leg support module (20a; 20b) which is pivotally mounted on the stand unit (14a; 14b), a bearing module (29a; 29b) which is designed to adjust the leg...
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WO/2024/030996A1 |
An aircraft air conditioning system comprises intakes ram air from outside the aircraft, and uses a heat exchanger to pretreat (preheat or precool) some of the ram air. The system further includes a heat recovery unit that uses the cabin...
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WO/2024/028671A1 |
Aircraft (1) capable of hovering comprising a fuselage (2), at least one rotor (3a, 3b, 4) that is rotatable with respect to the fuselage (2), electrical drive means adapted to rotate the rotor (3a, 3b, 4) and electrically powered by a b...
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WO/2024/029430A1 |
[Problem] To provide a parachute having a float that can exhibit greater long-term buoyancy than is conventional, without being damaged during deployment, and a safety device and a flying body comprising the same. [Solution] A parachute ...
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