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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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WO/2024/028571A1 |
An aircraft landing gear assembly comprising an oleo-pneumatic shock absorber (50) comprising an outer cylinder (52) and sliding tube (54) movable between a compressed position and an extended position, further comprising a sprung elemen...
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WO/2024/030357A1 |
This invention relates to intelligent structural and spatial three-dimensional (3D) real time guidance and training security process. Previously, when police or other law enforcement authorities are dispatched to an ongoing criminal site...
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WO/2024/028016A1 |
A hydrogen fuel delivery system (300) comprises a fuel line (312) having an inlet (315) and an outlet (316), a liquid fuel pump (307) configured to provide a flow of liquid hydrogen fuel from a hydrogen fuel storage tank (308) to the fue...
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WO/2024/028573A1 |
An aircraft landing gear shock absorber strut (50) comprising: an outer cylinder (52) and a sliding tube (54) being movably mounted within the outer cylinder so as to be movable between a compressed position and an extended position, fur...
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WO/2024/028572A1 |
An aircraft landing gear shock absorber strut (50) comprising: an outer cylinder (52) defining an oleo chamber (O) for containing pressurised oleo-pneumatic shock absorber fluid; a sliding tube (52) including a piston head (56) movably m...
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WO/2023/139459A9 |
The present disclosure includes an apparatus (10) for drone landing or drone dropping or wiring down of a package adjustable to a window and/or balcony sill (20) of a building. The present solution thereby innovatively overcomes the desc...
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WO/2024/028817A1 |
A system for generating magnetic fields in one or more axis, the system system comprising a primary electromagnet comprising a first coil having a first axis a first secondary electromagnet comprising a second coil having a second axis, ...
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WO/2024/030530A1 |
An energy harvesting system including a conductor that conducts a first current, a transformer that outputs a second current based on the first current flowing through the conductor, an energy storage device, and a rectifier connected be...
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WO/2024/028739A1 |
An unmanned aerial vehicle (UAV) comprising a rotor module comprising a coaxially arranged rotor having a substantially vertical axis of rotation and a laterally extending rotor housing, a battery located below the rotor module, a shaft ...
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WO/2024/028200A1 |
A method of applying a herbicide to a flood field (1). The method comprises providing an unmanned aerial vehicle (UAV) (2), and flying the UAV (2) along a plurality of substantially parallel spray flight paths (31). The method also compr...
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WO/2024/028858A1 |
An energy attenuation system for a seating system (having a bucket and a frame includes at least one energy attenuation component operatively coupled with a fuse system. The energy attenuation component includes first and second ends sec...
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WO/2024/028710A1 |
The present disclosure provides an aerofoil profile (200) for an aerodynamic element such as a wing, turbine blade, fin, etc. that facilitates the aerodynamic element to keep the boundary layer attached to its top surface with increasing...
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WO/2024/028553A1 |
The invention relates to a turboprop (10) comprising: - a turbine (12) mechanically connected to an input (21) of a reducer (20); - a tail shaft (30) bearing a variable-pitch propeller (31); - a rotary electric machine (46); and - an ele...
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WO/2024/024655A1 |
This hydrogen storage tank for a hydrogen aircraft includes an outer tank, an inner tank, a first strap, and a second strap. The inner tank is disposed inside the outer tank with a space therebetween, and has a shape having a longitudina...
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WO/2024/025491A1 |
The invention relates to motor groups consisting of electric motors for use in electric aircraft and the propulsion system that drives and manages them. Every electric motor has a propeller on the outside, while the rotor and stator inte...
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WO/2024/021319A1 |
A turntable type lifting airport device for a relative motion air kinetic energy aviation aircraft. A plurality of relative motion air kinetic energy reversal thrust generating devices (3) are provided on the periphery of a lower portion...
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