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WO/2023/177986A1 |
Described herein are apparatuses and methods for use therewith that can be used to remove dust and other types of particulates from a solar array of a spacecraft, a lander, a rover, or the like. Such an apparatus can include a main body ...
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WO/2023/175127A1 |
Protective envelope for a portion (2 to 7) of an aircraft body (1), comprising a framework (23) and a fabric (24), the fabric (24) being mechanically coupled to the framework (23) and extending around the framework (23) such that, in a d...
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WO/2023/178121A1 |
A calibration of an unmanned aerial vehicle is performed without the use of a magnetometer. The unmanned aerial vehicle generates a first acceleration vector in a navigation frame of reference and a second acceleration vector in a GPS fr...
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WO/2023/177774A1 |
A vehicle for travelling on a road and in the air is provided, comprising a fuselage extending from a forward to a rear end along a horizontal longitudinal roll axis, a pair of main wings mounted on the rear end of the fuselage, a pair o...
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WO/2023/176782A1 |
Provided is a flying apparatus in which the engine can be effectively cooled during flight. The flying apparatus 10 is provided with an airframe 19, a rotor 14, an engine 30, and a cooling unit 11 for cooling the engine 30. The cooling...
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WO/2023/178180A2 |
The present disclosure provides cargo systems for unmanned aircraft systems ("UAS") such as drones, and method of using same to deliver (e.g., load, transport, and unload) cargo.
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WO/2023/178175A2 |
Exemplary disclosed embodiments include systems, methods, and devices for a ground maneuvering system for aircraft. The systems, methods, and devices may include a ground maneuvering system including at least one processor in communicati...
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WO/2023/173202A1 |
A brake assembly is suitable for use in conjunction with a wheel having a rim rotatably mounted to an axle. The brake assembly includes a rotor configured to rotate about the axis with the rim. The rotor has a first frustoconical rotor s...
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WO/2023/175278A1 |
The present invention relates to an electrical system (4) for an aircraft (100), comprising: a first bus (411); a second bus (412); a first generator (401); a first converter (421); a second generator (402); and a second converter (422).
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WO/2023/175258A1 |
The invention relates to a seal (23) configured to be arranged between a first element (17) and a second element (11) of a propulsion assembly in an assembled configuration, the seal comprising a longitudinal sector (29) designed to be i...
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WO/2023/175251A1 |
The present disclosure relates to a method for manufacturing a coating for a porous substrate, and to a mechanical part equipped with such a coating, the method comprising the following steps: providing a substrate to be protected (31), ...
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WO/2023/173307A1 |
Provided in the present application are a movable platform and a control method therefor, an information prompting method and apparatus, and a movable platform, an electronic device and a computer-readable storage medium. Each of a plura...
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WO/2023/175265A1 |
The present invention relates to an aircraft part comprising: a composite material structure comprising a fibrous reinforcement embedded in a matrix; a heating element (9) configured to heat the part, the heating element (9) being embedd...
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WO/2023/173374A1 |
An unmanned aerial vehicle and an arm assembly. The unmanned aerial vehicle comprises a fuselage (10); at least one arm assembly (20), which comprises an arm (21) and a fuselage connection part (22) for being connected to the fuselage (1...
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WO/2023/175260A1 |
Dismountable aeronautical pod device 30 with cryogenic storage capacity, for external transportation by an aircraft, comprising a front cryogenic tank 36, a rear cryogenic tank 37, and at least one central temporary storage tank for the ...
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WO/2023/173377A1 |
A vibration isolation pad (100), used for connecting a main body (12) and a gimbal (300) of a movable platform (200). The vibration isolation pad (100) comprises: a first connecting portion (14), at least two first connecting members (18...
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WO/2023/175360A1 |
The crop harvesting drone (20) comprises a rigid frame (1), multiple rotors (13, 23) fixed to the frame (1), motors (14) for rotating the rotors (13, 23), a motorized gripping device mounted to the frame (1), an electric power source att...
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WO/2023/177942A1 |
A monopropellant rocket thruster includes a thruster, a pump, a decomposition catalyst, and an igniter. The thruster housing includes a reaction chamber and a divergent nozzle. The pump, coupled to the thruster housing, is operable to pu...
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WO/2023/177117A1 |
The present invention relates to an anti-drone detection method for privacy protection and, more specifically, in order to protect privacy, provides, at a downtown area building including skyscrapers, apartments, hotels, and the like, a ...
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WO/2023/175784A1 |
A measuring system (1) comprises an aircraft (30) that flies in a measurement zone and performs measurement and a management device (10) that controls the flight path of the aircraft (30). The management device (10) comprises an informat...
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WO/2023/173205A1 |
An aircraft has retractable landing gear configured to reciprocate between a deployed position and a stowed position. A landing gear door installation includes a first door rotatably coupled to the aircraft about a first axis for movemen...
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WO/2023/174678A1 |
The present invention provides a visual aid (200) for improving a pilot's awareness of the situation and status of an aircraft, which comprises means for: (202) determining, on the basis of information relating to the current navigation ...
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WO/2023/177228A1 |
The present invention relates to an electrical umbilical system for a space launch vehicle, using an electromagnet, the electrical umbilical system applying an electromagnetic method so as to fix an umbilical unit to a connection module ...
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WO/2023/170890A1 |
According to the present invention, an aircraft response characteristic providing system comprises: an aircraft holding device that holds a mounted drone; and an information output device that displays information for specifying data rel...
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WO/2023/172843A1 |
Systems and methods for targeted operational disablement that may utilize, for example, UAV-delivered shaped charges coupled to specific features of a target object. A UAV may navigate to, identify, and attach a disabling device to a cri...
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WO/2023/170223A1 |
An ejection unit for a satellite comprises a housing (10) closed by a door (12-18) in which housing a guiding structure for the satellite is provided. The guiding structure comprises angle bars (50-56) and a clamping device for clamping ...
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WO/2023/171872A1 |
A cyclic swing rotor assembly comprises: a first shaft; a blade rotating along with the first shaft; a hinge apparatus connecting the blade and the first shaft; a second shaft rotating independently from the first shaft; a swing hub rota...
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WO/2023/170940A1 |
The present invention provides an estimation device and so forth that can reduce time for accident investigation, without increasing staff for the accident investigation. A control device 10 according to an aspect of the present disclo...
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WO/2023/172364A2 |
An apparatus for a ground-based battery management for an electric aircraft is presented. The apparatus includes a battery pack mechanically coupled to the electric aircraft, wherein the battery pack includes at least a battery module, w...
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WO/2023/170472A1 |
An imaging survey platform utilizes imaging sensors arranged in one or more arcs to capture nadir and oblique views as required for photogrammetric processing into image maps and 3D surface maps, where a common primary lens subsystem is ...
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WO/2023/169957A1 |
The present invention relates to a piece of furniture intended for installation in an aircraft cabin and including a composite panel (30) comprising: - a first skin (31), - a second skin (32), and - a central honeycomb core (33) arranged...
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WO/2023/172224A1 |
The invention relates to a maintenance station (1) for unmanned aerial vehicles (100) which comprises a housing (10) having at least one opening (11a) for the entry and exit of the unmanned aerial vehicle (100), at least one platform (20...
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WO/2023/172244A1 |
An electric ion propulsor and method of using is provided comprising a substrate having an inner surface and outer surface. A plurality of antennae mounted adjacent to each other on the inner surface and are enabled to transmit RF energy...
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WO/2023/141166A3 |
A detent mechanism is provided for a tray table of an aircraft. The detent mechanism includes an actuator configured to move along with a table leaf of the tray table as the table leaf rotates between a stowed position and a deployed pos...
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WO/2023/169966A1 |
The invention relates to a motorised propeller-based paraglider propulsion assembly comprising a wing, suspension lines, and a seat (2) mounted on a rigid frame (3) which carries a pilot (1) who is positioned in front of the frame (3) an...
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WO/2023/168623A1 |
Provided are an unmanned aerial vehicle base station (100) and an unmanned aerial vehicle system. The unmanned aerial vehicle base station (100) comprises a base body (10), a landing pad (20) arranged on the base body (10), and a base st...
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WO/2023/169895A1 |
The invention relates to a system for measuring the fatigue (11) of a mechanical structure (10), comprising: - a first force sensor (19.1) capable of generating a first signal (S1) representative of a force applied to a first mechanical ...
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WO/2023/129062A3 |
This invention relates to an antimicrobial additive material with a flame retardancy and antimicrobial feature which can be used as an additive material for interior surfaces in passenger aircraft.
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WO/2023/139580A3 |
Systems, methods, subsystems and apparatuses for controlling of installment, removal, maintenance and/or transporting of solar panel units (SPUs) in a solar facility. Each SPU may be installable/supportable by a panel support structure (...
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WO/2023/172357A2 |
Aircraft (20) and airfoils (24) for more efficient flight operations using electric motors. An aircraft (20) includes an airfoil (24) and a thrust device (44) rotatably mounted within the airfoil (24). An airfoil (24) includes a top surf...
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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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