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WO/2023/170592A1 |
It is an object of the invention to provide an apparatus (10) for remotely controlling the flight of aircraft, wherein said apparatus (10) comprises a first wireless transceiver module (20) located on board the aircraft and a second wire...
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WO/2023/170933A1 |
An extension boom (120) comprises a fiber-reinforced composite material. When the extended extension boom (120) is opened, the directions of the fibers in a first region are a first low-angle direction which forms a negative angle in the...
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WO/2023/170357A1 |
The invention relates to an aeronautical propulsion unit (10) with a longitudinal axis (X), comprising a hub (12), an annular row of non-ducted upstream rotor blades (14) and an annular row of non-ducted downstream stator blades (16), wh...
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WO/2023/172675A1 |
An inerting fuel tank system comprising a closed tank and any number of flow impingement valves. The flow impingement valve allows uninhibited flow in one direction. In the reverse direction, the fluid flows back into the input flow stre...
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WO/2023/170358A1 |
The invention relates to an aeronautical thruster (10) with a longitudinal axis (X), comprising a hub (12), an annular row of non-ducted upstream rotor blades (14) and an annular row of non-ducted downstream stator blades (16), each down...
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WO/2023/169217A1 |
The embodiments of the present application relate to the technical field of unmanned aerial vehicles, and particularly relate to a quick release mechanism, a battery and an unmanned aerial vehicle. The quick release mechanism comprises: ...
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WO/2023/170365A1 |
The invention relates to a seat comprising a cushion (10) and a backrest (11) which are articulated to one another, the seat (1) also comprising at least one electric actuator (2) configured to make the cushion (10) and/or the backrest (...
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WO/2023/173047A1 |
A hybrid battery system comprises a high-power energy element; a high-capacity energy element; a switching element; a sensor configured to measure current draw; and a microcontroller. Current draw by an electrical load from the hybrid ba...
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WO/2023/164893A1 |
Provided in the embodiments of the present invention are an unmanned aerial vehicle, and a control method of an unmanned aerial vehicle. The unmanned aerial vehicle comprises a frame, a material box and a spreading mechanism. The materia...
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WO/2023/167790A1 |
A leg assembly for a passenger seat for a vehicle such as an aircraft includes a forward leg and an aft leg. The forward leg includes a top end and a bottom end opposite the top end, and the top end of the forward leg includes a forward ...
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WO/2023/166273A1 |
A device (20) for supporting a fluid duct (C), comprising: - a link (22) for supporting the duct via two end parts (22a) of the link that are spaced apart from one another in a longitudinal direction and adopting, transversely, a curved ...
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WO/2023/166221A1 |
A re-usable intercept drone (104) comprises an elongate fuselage (200), a first wing (202) and a second wing (206) operably coupled to the elongate fuselage (200) and extending substantially away from the elongate fuselage (200). A first...
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WO/2023/167334A1 |
The present invention relates to: a core material that has air permeability and that has both lightweight and mechanical properties; and a skin-core structure that uses said core material. The core material according to the present inven...
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WO/2023/167131A1 |
[Problem] To achieve high safety performance and extend cruising time in an aircraft. [Solution] An aircraft according to the present invention can be boarded by a passenger and moves while floating above the ground. A method for control...
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WO/2023/167130A1 |
[Problem] To improve the flight performance of an aircraft. [Solution] This aircraft on which a passenger can ride, and which moves by floating from the ground, is characterized by comprising: a fuselage on which the passenger rides; lif...
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WO/2023/164862A1 |
A dual-propeller universal transmission device, used for dual-propeller transmission of an aircraft or aerial vehicle, consisting of an input sleeve shaft, input double bevel gears, a revolving sleeve shaft, revolving double bevel gears,...
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WO/2023/164739A1 |
A tank assembly for a helicopter is disclosed herein. The helicopter has a fuselage with at least two spaced-apart longitudinal floor beams and at least one lateral floor member extending therebetween. The tank assembly comprises a retra...
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WO/2023/165951A1 |
The invention relates to a movement transmission device (10) for a mechanism for actuating and/or opening and/or closing and/or locking and/or unlocking a door or a flap of a mechanical movement control device of an aircraft, the device ...
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WO/2022/204239A9 |
A flight control arrangement for a hybrid aircraft includes a fixed-wing flight (F/W) control module and vertical takeoff/landing flight (VTOL) control module. The F/W control module is an integrated component having a respective network...
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WO/2023/167624A1 |
The present invention relates to an unmanned aerial tree harvesting system (1) comprising a remotely and/or autonomously controlled UAV (100), an autonomously and/or remotely controlled tree harvesting tool (117) configured for holding a...
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WO/2023/166389A1 |
The invention relates to a device (1) for pneumatic launching of a drone (2), comprising a launch tube (3), a pressurization chamber (6) situated at the rear of the tube (3) and provided with a passage opening (63) leading into the tube ...
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WO/2023/167597A1 |
In one aspect the invention provides a helicopter grapple assembly including a support frame which includes a cargo hook connector, a pair of opposed grapple jaws pivotally connected to the support frame, and a hydraulic drive ram connec...
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WO/2023/167335A1 |
Provided is a core material that can be smoothly manufactured with an improvement in the formation and strength of a base material and has excellent strength and lightness. The present invention provides the core material comprising a st...
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WO/2023/166256A1 |
A propulsive assembly (100) for a multi-engine hybrid aircraft, comprising a first and a second gas turbine (10, 20) each having a gas generator (12, 22) and a free turbine (11, 21), a main rotor (62) coupled to the free turbine (11, 21)...
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WO/2023/168116A2 |
A control system for a kite having a quick release loop assembly includes a retention mechanism configured to release one end of the loop upon sliding a handle from a covered disposition to an uncovered disposition. The quick release ass...
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WO/2023/167703A1 |
Various implementations include a low-drag smart tether system for measuring fluid speed and direction. The system includes a sleeve, a pressure sensor, and a tether. The sleeve has a longitudinal axis and an airfoil shaped cross-section...
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WO/2023/164004A1 |
The present disclosure provides an unmanned vehicle system that includes: a first non-terminal cell enclosing a first plurality of terminal cells, each of the first plurality of terminal cells enclosing a respective unmanned arial vehicl...
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WO/2023/161454A1 |
The invention relates to a device (10) for fastening cabin components in the region of side walls (6) of an aircraft structure (1), in particular the aircraft structure (1) of a commercial aircraft, said side walls extending in the verti...
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WO/2023/159304A1 |
A personal flying apparatus comprising a body structure adapted to support and detachably couple a user thereto; and a pair of wings rotationally coupled to opposite sides of the body structure and powered by a battery, the body structur...
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WO/2023/163817A1 |
An optical system can include a mirror that reflects incoming light to a sensor for detection. The position and/or orientation of the mirror can be controlled to reflect incoming light from different locations and/or directions. Position...
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WO/2023/161722A1 |
A space vehicle including a space vehicle body, wherein the space vehicle body includes an interior surface defining an interior of the space vehicle body and an exterior surface opposite the interior surface, and wherein at least a port...
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WO/2023/161586A1 |
The present invention relates to an aircraft engine assembly comprising: a duct (4); a beam (51); and an acoustic fairing.
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WO/2023/162405A1 |
In order to provide a moving device which facilitates taking off and landing of an unmanned flying body, the moving device comprises: a body device which travels by a travel device; a taking-off/landing unit which is provided to the body...
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WO/2023/161719A1 |
Ae methhod includes providing a quantity of sheet metal, press-forming a first panel from the sheet metal to form a first stamped panel, press-forming a second panel from the sheet metal to form a second stamped panel, fixing at least on...
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WO/2023/162953A1 |
Provided is a control system for a flying vehicle, the control system including: a speed sensor that detects the flight speed of the flying vehicle; a distance sensor that obtains a first distance, which is the distance between the flyin...
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WO/2023/163310A1 |
The present invention relates to a drone station for automatically supplying a spray agent, and a drone spray system comprising same. The drone station for automatically supplying a spray agent, according to one embodiment of the present...
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WO/2023/163401A1 |
The present invention relates to a temperature maintenance drone capable of transporting a human organ for medical use, and a control method therefor. The temperature maintenance drone capable of transporting a human organ for medical us...
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WO/2023/161714A1 |
A system, including: a satellite; a first solar array (310), where the first solar array has at least a first solar panel; a second solar array (312), where the second solar array has at least a second solar panel; a boom (320) having a ...
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WO/2023/162583A1 |
An IoT device (40) is installed by a user living in a dwelling unit (30), in order to perform communication for a variety of purposes in said dwelling unit (30). In the present embodiment, the dwelling unit (30) is included in a multiple...
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WO/2023/161718A1 |
A space vehicle including a body having an interior, an exterior, a first side and a second side; a first stacking pillar positioned on the exterior of the body at the first side thereof; a second stacking pillar positioned on the exteri...
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WO/2023/161712A1 |
A system having a first layer of satellites, where the first layer of satellites includes a first satellite (100a), a second satellite (100b), a third satellite (100c), and a fourth satellite (100d), where each of the first, second, thir...
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WO/2023/161729A1 |
The invention relates to a device (1) for launching a drone (2) using spring thrust, in which the means (7) that control the unlocking of an ejection assembly (5) from its armed position comprise a release housing (34) containing a relea...
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WO/2023/159323A1 |
A system for inspecting surfaces of an aircraft prior to takeoff. The system includes a device movable relative to the surfaces of the aircraft. At least one camera on the device is provided for determining conditions of the surfaces of ...
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WO/2023/161216A1 |
The invention relates to a method for landing a kite system (23). The kite system (23) comprises a kite (14) and a gondola (25), and the kite (14) is held on the gondola (25) via a line tree (24). The gondola (25) is held on an attachmen...
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WO/2023/163617A2 |
The present method and device provide an increase in the operational efficiency of telescopes by mitigating the effect of bright, fast-moving objects on the operation of the guiding system and on the observation results of at least one t...
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WO/2023/161717A1 |
A space vehicle includes a first aluminum panel, a second aluminum panel fixed to the first aluminum panel around at least a portion of respective perimeters thereof to thereby form an enclosed structure having an interior volume, a plur...
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WO/2023/161713A1 |
A space vehicle includes a body; a stacking pillar (200a) coupled to an exterior of the body and defining a longitudinal axis, wherein the stacking pillar (200a) is configured to be removably coupled to a stacking pillar (200b) of an adj...
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WO/2023/160824A1 |
An aircraft that is certifiable for freighter transport is disclosed herein. The aircraft can include a hybrid fuselage including a plurality of modular sections, wherein the plurality of modular sections includes a first section, a seco...
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WO/2023/164149A1 |
Radioisotope power system and propulsion system technologies to increase the energy efficiency, mass efficiency, and duration capability of a vehicle during operation. A radioisotope power system includes a radioisotope power unit that e...
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WO/2023/162486A1 |
A delivery drone 10 comprises: an arrival determination unit 31 which determines that information on the current location of the drone indicates an arrival in a prescribed range from article delivery destination location information; a s...
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