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WO/2023/074612A1 |
Provided is an aircraft lighting unit that reduces the effort required for outer lens replacement. An annular lens holder (4) detachably holds an outer lens (2) in a first housing (61). The lens holder (4) is formed of elastic material...
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WO/2023/075639A1 |
An aircraft sidestick is a device that can be used for controlling different types of manned and unmanned equipment, including aerial, terrestrial and underwater equipment, as well as for controlling spacecraft in outer space and for exe...
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WO/2023/070187A1 |
An aircraft with an aft-fuselage propulsion system comprises a thermal engine, a first electric motor coupled to a first propulsor, a second electric motor coupled to a second propulsor, and a mechanical interlink system integrating the ...
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WO/2023/076232A1 |
Devices, such as aerodynamic kites used in kiteboarding (also known as kitesurfing), handheld aerodynamic wings used in wing foiling and wing surfing, and paddles used in paddleboarding, for generating a force for powering a user on an a...
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WO/2023/072419A1 |
Apparatuses, methods, and systems are disclosed for communicating and storing aerial system security information. One method (600) includes transmitting (602) a request message to an uncrewed aerial system network function, a network exp...
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WO/2023/073721A1 |
An oxidizer tank is disclosed. The oxidizer tank comprises: a first shell and a second shell; and a flexible diaphragm separating the first shell from the second shell, thus defining: a first compartment, configured to contain the oxidiz...
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WO/2023/074870A1 |
This hydrogen aircraft comprises: an airframe provided with a fuselage and wings; at least one propulsion system fixed to the airframe; a pressurized cabin disposed inside the fuselage; a pressure bulkhead that is disposed at the rear of...
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WO/2023/074368A1 |
[Problem] To provide a technology capable of increasing a propulsion efficiency in a BLI propulsion technology. [Solution] An aircraft according to the present technology comprises a fuselage and a BLI propulsion unit. The fuselage is cy...
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WO/2023/072356A1 |
The present invention disclose an autonomous flying vehicle comprising a main tool carrying body, said main tool carrying body having a front side and a rear side, with body sides connecting said front and rear sides, and where said tool...
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WO/2023/074866A1 |
This fuel supply system (1) for a hydrogen aircraft comprises: a fuel tank (2) that stores liquefied hydrogen; a pump (5) that discharges liquefied hydrogen from the fuel tank (2) and supplies the same to a propulsion device (102); a pre...
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WO/2023/073533A1 |
The present disclosure relates to a damper device (100) configured to dissipate energy from at least one connecting cable (10) suitable for connecting a first satellite module (200) and a second satellite module (300), said damper device...
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WO/2023/067865A1 |
Provided is a flush switch that is for an aircraft lavatory unit comprising two types of flush switches, and that enables reduction in the number of component parts for the aircraft lavatory unit, and thus improves mounting work efficien...
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WO/2023/066301A1 |
A battery compartment assembly (1) and an unmanned aerial vehicle. The battery compartment assembly (1) comprises: a compartment body (10) provided with an accommodating cavity (101); a compartment cover (20); and a rotating assembly (30...
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WO/2023/067432A1 |
Systems and methods for an aircraft comprising: wings in tandem configuration wherein each wing having one tilting motor; an additional tilting motor located at the rear part of said aircraft; wherein all said tilting motors can tilt in ...
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WO/2023/066300A1 |
A battery compartment assembly (1) and an unmanned aerial vehicle. The battery compartment assembly (1) comprises: a compartment body (10) provided with an accommodating cavity (101) and a mounting groove (102), the accommodating cavity ...
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WO/2023/068729A1 |
The present invention relates to an operating method for a user terminal operating by at least one processor, wherein an information registration menu screen is displayed in a bus information provision application executed according to a...
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WO/2023/069723A1 |
In one embodiment, an air-scoop includes an air inlet that air molecules enter the air¬ scoop through at an orbital speed when the air-scoop is moving through an atmosphere at the orbital speed. The air-scoop also includes a rotor that ...
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WO/2023/067253A1 |
The invention relates to a flying device comprising a main body, to which a combustion engine (MC), an electric motor (ME), an electricity generator (GE) and an electrical energy transfer circuit (300) are attached. The combustion engine...
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WO/2023/034302A9 |
A system and method for lift augmentation of an aircraft having a wing with a leading edge and a trailing edge extending along a wingspan, a plurality of thrust-producing devices connected to the bottom of said wing, at least one flap co...
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WO/2023/068577A1 |
The present invention relates to a system for providing user-customized information by using an autonomous driving device, and a problem to be solved by the present invention is to automatically recognize and analyze a user and his/her e...
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WO/2023/067339A1 |
A VTOL aerial vehicle (10) is disclosed, comprising: an airframe (12); one or more arms (202) coupled to the airframe (12) at a pivot (206); and three or more propulsion units, each mounted on a gimbal (16) having a gimbal axis, and each...
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WO/2023/066753A1 |
The invention essentially consists of a heat pipe with re-entrant grooves, in which the connection channels between the liquid channels and vapour channel are open more widely in the condenser than in the other zones of the heat pipe (ev...
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WO/2023/067269A1 |
The invention relates to a method for manufacturing a vane (300) made of composite material and having a cavity, the method comprising at least: - producing a core (1; 2; 3; 4) having the shape of the cavity of the vane (300) to be manuf...
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WO/2023/067015A1 |
Disclosed herein is a forestry monitoring system comprising an unmanned aerial vehicle, UAV (30) and a computing device (35). The UAV comprises an electrical energy storage (31), an electric motor (32) powered by the electrical energy st...
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WO/2023/067270A1 |
The invention relates to a method for manufacturing a turbine engine part made of composite material and having a cavity, the method comprising at least: - producing a core (1) having the shape of the cavity of the vane to be manufacture...
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WO/2023/067266A1 |
Device for de-icing an aerodynamic profile (100), comprising a surface referred to as a lower surface, a plurality of unitary cavities (2a, 2b) delimited by a lattice of partitions (3a, 3b) on the surface, and a barrier arranged on the l...
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WO/2023/066960A1 |
The invention relates primarily to an assembly for an aircraft cabin (10), comprising: - at least one seat unit (11) comprising a seat (12) and a privacy shell (13) extending at least partially around the seat (12); - at least one separa...
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WO/2023/067005A1 |
The invention relates to a device (1) for handling and transferring an aircraft engine (2) having a receiving cradle (10) comprising at least two holding elements (30), and at least three support modules (20) suitable for supporting the ...
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WO/2023/067252A1 |
The invention relates to a method (100) for correcting the thrust vector created by a thrust assembly associated with electrical means for correcting said thrust vector. Such a thrust assembly comprises a mechanical rotor rotated by a ro...
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WO/2023/066934A1 |
The present invention relates to a thermal protection system (10) for an aircraft comprising a cockpit, the cockpit comprising a plurality of transparent surfaces (12, 14, 16), at least two transparent surfaces (14) being openable. The p...
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WO/2023/068477A1 |
The present invention relates to an air purifier having a 3D active tracking monitoring drone and, more specifically, to an air purifier having a 3D active tracking monitoring drone, in which a drone interlocked with an air purifier dete...
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WO/2023/066970A1 |
The invention relates to aircraft landing gear (0) having a male part (M0, M1, M3) interlocked with a female part (F0, F1, F2, F3) along an interlocking direction (D). The external contact surface of the male part (M0, M1, M3), when it i...
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WO/2023/067651A1 |
The present invention comprises: a distance acquisition unit (115) that detects the separation distance between an aerial vehicle (V1) and a platform (51); a remaining charge acquisition unit (113) that acquires the remaining charge of a...
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WO/2023/067289A1 |
The invention relates to a method for mounting an axle (12) in a bore (14) of a bogie (16) mounted on an aircraft landing gear (18), the landing gear (18) being in a gear-down position, the bore (14) extending in a substantially horizont...
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WO/2023/067000A1 |
The invention mainly relates to an assembly for an aeroplane cabin (10), comprising: - a rear seat unit (11.1), - a front seat unit (11.2), - a passage for accessing an aisle way extending between the rear seat unit (11.1) and the front ...
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WO/2023/069537A1 |
The present invention provides a system for remote vehicle operation by human pilot and artificial intelligence systems. The system comprises: a vehicle capable of movement, a human operator and control station situated outside of the ve...
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WO/2023/065175A1 |
A support, a control device, a gimbal system, a photographing assembly and system; the support (300) is used for connecting the control device (2000); the support comprises a support part (1), a mounting part (2) and an electrical connec...
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WO/2023/065779A1 |
The present application relates to a vortex generator, a radome and an antenna, and belongs to the technical field of wind resistance reduction. The vortex generator comprises a first vortex generating portion and a second vortex generat...
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WO/2023/067527A1 |
A system includes a first electric motor that when in operation imparts rotation to a fan stage of an engine. The system also includes a combustion section of the engine comprising a combustor that when in operation generates combustion ...
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WO/2023/070001A1 |
Aspects of the present disclosure relate to an extendable conductor assembly. A conductor of the extendable conductor assembly may be extended (e.g., into a thermal target, such as a preexisting or a newly created feature of a planetary ...
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WO/2023/067286A1 |
The invention relates to a method for manufacturing a part made of composite material, the method comprising: - three-dimensional weaving (S10) of a structure (20) having a longitudinal axis (A); and - braiding (S40) of at least one laye...
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WO/2023/066030A1 |
The present application provides an unmanned aerial vehicle (UAV) surface coating, a preparation method therefor, and a UAV. The coating at least comprises: an adhesive layer, an anti-oxidation layer, an oxygen barrier transmission layer...
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WO/2023/068041A1 |
[Problem] To provide: a safety device which enables rapid expansion of a float, which has sufficient buoyancy at the time of contact with water, and which has reduced weight compared to prior art; and an aircraft comprising this safety d...
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WO/2023/067653A1 |
An aerial vehicle control device (1) for controlling an aerial vehicle that flies over water, said device comprising: a crash detection unit (31) for detecting that the aerial vehicle has crashed into the water; and an acoustic wave outp...
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WO/2023/067010A1 |
The invention relates to a method and a system for determining the temperature in a mounted aircraft tyre. The system is characterized in that it comprises two temperature sensors installed inside the tyre.
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WO/2023/066991A1 |
The present invention mainly relates to an assembly for an aircraft cabin (10), comprising: - at least one seat unit (11) comprising a seat (12) and a privacy shell (13) extending at least partially around the seat (12), - a compartment ...
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WO/2023/062243A1 |
A method of transmitting energy comprises a production step of producing hydrogen, a first transferring step of transferring the hydrogen into a tank at a first location, a transporting step of transporting the tank to a second location ...
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WO/2023/064286A1 |
A vehicle includes a vehicle ceiling, a vehicle floor, and a vehicle seat assembly that couples with the vehicle ceiling and the vehicle floor. The vehicle seat assembly includes a seat support that supports a vehicle seat from the vehic...
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WO/2023/060679A1 |
Disclosed are an aircraft (1), a wing assembly, and an aerocar. The aircraft (1) comprises a fuselage (10), a wing assembly (20), a tilting connector (30), and a rotor assembly (50). The wing assembly (20) comprises a fixed portion (21) ...
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WO/2023/062622A1 |
The present invention relates to a transport vehicle, comprising an unmanned aerial vehicle (UAV) configured to operate autonomously; a compartment sized and shaped to hold at least one passenger; and an adaptor arm for selectively inter...
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