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WO/2024/089412A1 |
An extendable aircraft passenger suite furniture item for mounting on a structure of an aircraft passenger suite. The extendable aircraft passenger suite furniture item comprises an extruded first frame structure (100) comprising a body ...
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WO/2024/088762A1 |
A method for controlling a drone (15) within a shaft (7) of an elevator system (1) comprises: receiving sensor data (35) in a control device (29) of the drone (15), wherein the sensor data (35) have been generated by a sensor device (27)...
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WO/2024/090127A1 |
This photoelectric conversion device (112) comprises: a photoelectric conversion element (240) that converts light energy of incident light into electrical energy; a first wavelength conversion layer (234) that is disposed in contact wit...
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WO/2024/092018A1 |
A computer-implemented method includes receiving design and/or engineering data (D/E data) corresponding to a prototype representation of a product and transmitting one or more inputs derived from the D/E data to one or more digital engi...
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WO/2024/091629A1 |
Embodiments relate to an aircraft control and interface system configured to adaptively control an aircraft according to different flight states by modifying one or more processing control loops. The system receives sensor data from one ...
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WO/2024/091674A1 |
The present invention is specifically directed to an aerial drone apparatus configured to emit a board spectrum of different signal waves in various dynamic frequencies and waveforms transmitted through an array of leveled antennas posit...
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WO/2024/088974A1 |
An item handling system for moving an item between an origin and a destination according to a first scheduled route which departs the origin at a first predetermined departure time is provided. The item handling system comprises processi...
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WO/2024/091406A1 |
A spreader for a passenger seat includes a body having a forward end and an aft end. The body defines at least one roller support rail monolithic with the body and between the forward end and the aft end. The spreader includes a non-unif...
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WO/2024/090524A1 |
This hybrid rotor drive system comprises: a gas turbine engine which includes a compressor, a combustor, a turbine, and a first output shaft mechanically connecting the compressor to the turbine; an electric motor including a second outp...
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WO/2024/089432A1 |
Unmanned inspection system for performing an unmanned inspection of an enclosed space. The system has an Unmanned Vehicle (120) and a Launch And Recovery System (10, 110). The Launch And Recovery System (10, 110) has a launch and/or land...
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WO/2024/089376A1 |
The invention relates to a pitch-change mechanism (70), which comprises a frame (72), an actuating cylinder (74), and a locking device (160). The actuating cylinder (74) comprises a cylinder block (104) and a piston (106), of which one i...
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WO/2024/091926A1 |
Functions of an unmanned aerial vehicle (UAV) can be location dependent. In some embodiments, a digital audio communications channel is synchronized and multiplexed with a high-definition video stream, captured from a user-controlled rem...
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WO/2024/092202A1 |
An aircraft includes a first inceptor assembly. The first inceptor assembly has a first base and a first control stick extending away from the first base, the first control stick defining a first longitudinal axis that extends through th...
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WO/2024/072442A3 |
Embodiments of the disclosure are directed to a vibration control system and a vibration control device for structurally isolating a load from a vibration source. In various embodiments a vibration isolation device includes a first and s...
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WO/2024/091205A1 |
The present invention relates to a body (2) on an air vehicle; at least one wing (3) located on the body (2), extending outward from the body (2), allowing the air vehicle to rise depending on the air flow; at least one flap (4) that is ...
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WO/2024/088998A1 |
In an air-ducting component (2) with a wall (16), which provides an airtight delimitation for an interior space (10) from an exterior space (18) surrounding the component (2), the wall (16) contains at least a first layer (20a) of a two-...
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WO/2024/089377A1 |
The invention relates to a pitch-change mechanism (70), which comprises a frame (72) and an actuating cylinder (74) including a movable portion (102) that is translatable relative to the frame (72). The mechanism also comprises a connect...
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WO/2024/089670A1 |
A frame device (100) for a propulsion unit (200a…200n) of a flight device (300), comprises annular elements (10a…10n) for a fixation of a fuel tank (210) of the propulsion unit (200a…200n), a retaining element (60) being arranged b...
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WO/2024/087315A1 |
Provided is a flying automobile (100). The flying automobile (100) comprises an automobile body (10), and a flight power system (20) and a land power system (30) which are connected to the automobile body (10). The flying automobile (100...
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WO/2024/089338A1 |
The invention relates to a method for manufacturing a propeller blade or vane made of composite material, the method comprising: - producing, by means of three-dimensional weaving between warp yarns (101) and weft yarns (102), a fibrous ...
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WO/2024/089998A1 |
Provided are a flight route generation device and a flight route generation method which are for generating, with respect to various flight bodies, a safe flight route by suitably considering the weather resistance of the flight body. ...
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WO/2024/088472A1 |
The invention relates to an aircraft (1) having a fuel-cell propulsion system (2), wherein the fuel-cell propulsion system (2) comprises - a fuel cell (3) for supplying electricity to an electric propulsion apparatus (4) of the aircraft ...
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WO/2024/090940A1 |
A method for guiding landing of an unmanned aerial vehicle and a system to which the method is applied are provided. One of several embodiments according to the present disclosure provides a method for guiding landing of an unmanned aeri...
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WO/2024/087465A1 |
The embodiments of the present disclosure belong to the technical field of aerospace structure designs. Disclosed is a satellite-rocket-carrier integrated spacecraft. The satellite-rocket-carrier integrated spacecraft comprises a satelli...
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WO/2024/089273A1 |
A device (1) for stabilising the attitude of a load (3) carried by a drone (2) along a space horizontal axis (x-x), the drone having a lower surface (20) wherein a connection seat (21) is obtained at a drone vertical axis (z0-z0) passing...
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WO/2024/088721A1 |
The invention relates to a device for securely locking an adjustment system (1) of a fastener (2) of an opening panel, this fastener comprising at least one splined washer (4) translating along a cylindrical body (3a) of an adjustment sl...
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WO/2024/086930A1 |
A main fitting includes an elongate piston and a cylinder configured to slidingly receive the piston. A first end of the piston extends from a first end of the cylinder, and a second end of the piston extends from a second end of the cyl...
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WO/2024/091922A1 |
The present disclosure relates to a jetstream power generating system. The system is configured to harness the energy of jetstream forces in farms as power generating infrastructure. The system comprises an airborne element configured to...
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WO/2024/089336A1 |
The subject matter of the present invention is glazing (7) for flush attachment with a frame (10), the glazing (7) having at least one recessed area (8), by which the glazing (7) is configured to be fixed to the frame (10), the at least ...
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WO/2024/082667A1 |
The present invention relates to the field of airport towbarless tractors. Disclosed is a green intelligent comprehensive-energy-supply towbarless tractor, comprising a chassis unit, which comprises a vehicle control unit, a power supply...
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WO/2024/084490A1 |
The present invention "ERASS" provides an Unmanned Aerial Vehicle (UAV) based lifesaving vests/buoy and/or lifesaving kits dropping system. The UAV lifesaving kits dropping device comprises of a lifesaving kit which provides the connecti...
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WO/2024/084297A1 |
Apparatus for installing equipment at a remote location includes a gripper that is releasably coupled to a controller. The gripper includes a first grip member and a second grip member. The second grip member is pivotally joined to the f...
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WO/2024/084029A1 |
The invention relates to a method for destroying a satellite (10) comprising cycles (2000) of updating an onboard memory (11) when the satellite is in outer space (100). Each update cycle comprises receiving, by a communication device (1...
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WO/2024/084953A1 |
The present disclosure relates to an information processing device, an information processing method, and a program with which improved sound collection can be achieved. An information acquisition unit acquires information necessary for ...
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WO/2024/083722A1 |
An aircraft engine seal apparatus has an inflatable seal with a front wall (3, 803, 1103) a rear wall (9, 840) and a side wall (4, 804) forming a rim for pressing and sealing against an internal surface of an engine intake. There is at l...
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WO/2024/085765A1 |
Disclosed is a system and a method for projecting a solution onto a facade of a structure. The system comprises: a pump for pumping the solution; a tool for projecting the pumped solution onto the facade; a hose for connecting the pump t...
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WO/2024/082001A1 |
An embodiment provides a protective suit system that is configured for protecting an occupant in extreme environments. The system may comprise a base layer to be worn on the occupant that is configured for thermal regulation of the occup...
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WO/2024/084781A1 |
At the destination of a drone (10), a detection unit (12) detects a landing-possible area and a landing-impossible area for the drone (10). A safety level specifying unit (13) specifies one of a plurality of safety levels at the time of ...
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WO/2024/082833A1 |
A multirotor electric-manned aerial vehicle, comprising: a cabin (1) for carrying people; multiple rotor support arms (2), wherein each rotor support arm has one end fixedly connected to the top of the cabin by means of a central connect...
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WO/2024/085438A1 |
The present invention relates to a reverse propulsion overtilting tiltrotor drone, which is an unmanned aerial vehicle, consisting of: a main body (10); wings (20) extending from both sides of the main body (10); a tilt rotor (30) provid...
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WO/2024/083876A1 |
The present invention relates to an aerostat of the type comprising a lift enclosure (1), filled with gaseous dihydrogen, electric propulsion means allowing the propulsion of the aerostat and means for supplying electricity to the propul...
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WO/2024/083452A1 |
The invention relates to a method for taxiing an aircraft while anticipating an inability of a drive member equipping at least one wheel (RA) borne by a landing gear (AA) of the aircraft (A) to move said aircraft on the ground, the metho...
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WO/2024/084156A1 |
The present disclosure relates to an assembly for an aircraft comprising: a compensator (5) comprising: a chassis (50) intended to be fixedly mounted on a cell of the aircraft; and an actuator (52) movably mounted on the chassis (50); a ...
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WO/2024/084222A1 |
The present invention concerns a system for positioning an airborne vehicle (502) at a geographic location, the system comprising the airborne vehicle (502) having one or more infra-red ( I R) detectors, and a positioning beacon (504) lo...
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WO/2024/083756A1 |
The present invention relates to a crash handling system (10) for an aircraft, comprising an altitude surveillance system (20), which is adapted to receive altitude data from at least one altitude sensor (22) and to issue an altitude war...
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WO/2024/082392A1 |
A method and system for actively controlling the center of gravity of an aircraft, the method comprising: before an aircraft takes off, acquiring heading centers of gravity of a rear water tank (01) and a front water tank (02) on the air...
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WO/2024/084523A1 |
This invention is designed to solve the problem of drone and helicopter landing in uneven and sloping areas and landing on the variable deck slope during a storm, which is very difficult or even impossible for a helicopter with a simple ...
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WO/2024/084009A1 |
A gap cover (3) for a device component (1), preferably for a cabin attendant seat, for visually closing a gap (2) relative to a further cabin component (6) in a passenger cabin (7) is provided. The gap cover (3) has at least one covering...
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WO/2024/082367A1 |
An airborne real-time three-dimensional imaging radar, and an aircraft. The radar comprises: double antennas (2), which are used for acquiring observation signals from an observation area; a signal transceiver, which is used for transcei...
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WO/2024/086324A1 |
The disclosed embodiments are directed to an eVTOL aircraft comprising a fuselage, wings mounted to the fuselage, where the wings comprise an undercambered lower surface, and an array of ducted fans mounted to the undercambered lower sur...
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