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WO/2023/272445A1 |
A frame, a stand, and an unmanned aerial vehicle. The frame (1) comprises at least one support member (100), the at least one support member (100) forming a frame structure. Each support member (100) comprises: a first support component ...
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WO/2023/274896A1 |
An aircraft landing gear comprising: a strut mounted on an aircraft structure so as to move between an extended position and a retracted position; a bracing member comprising a first connecting rod hinged to the aircraft structure and a ...
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WO/2023/274740A1 |
The invention relates to an assembly of a vehicle door and of a panel (1) surrounding the door (3), wherein an edge protector (4) extends along the skin of a vehicle door (3a) next to the skin of the panel (1a) and has a portion that is ...
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WO/2023/275473A1 |
The invention relates to a propulsion assembly comprising a shroud defining a flow duct for a secondary flow. This shroud comprises bifurcation panels (19A, 19B, 19C) of which at least one (19C) is hinged to a pylon via connecting member...
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WO/2023/276454A1 |
The control device according to the present invention comprises a processor and a memory that is connected to or built into the processor. The processor carries out, when the processor causes a rotary drive device on which a distance mea...
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WO/2023/274826A1 |
A foldable sheet material (10) having a plurality of stiff sections (12) which are foldable or rotatably connected along straight edges (14), wherein a straight primary edge (16) extends from a first point (18) on the margin of the sheet...
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WO/2023/272353A1 |
An aerial vehicle configured to fly both vertically and horizontally, suited to fighting fires or assisting search and rescue operations. The aerial vehicle has an airframe, a drive shaft, a rotor having blades that allow the angle of pi...
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WO/2022/269052A1 |
A computer-implemented method for providing operation data for treatment devices (102, 104, 106, 107) on an agricultural field (112), wherein the treatment devices include at least a first treatment device (102) and a second treatment de...
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WO/2022/271789A1 |
In an embodiment, there is provided a method for determining a spacecraft instantaneous velocity using starlight. The method includes determining, by a star pairing module, a plurality of star pairs in a selected star field image. The se...
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WO/2022/271283A1 |
A flammability reduction system and method for controlling air pressure and allowing an air separation module (ASM) to consume less pressurized air includes a pressure limiting valve that is dynamically controlled based upon a defined pr...
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WO/2022/268366A1 |
In order to increase the capacity of a transport-container conveyor system (2), sorting processes and dimensions of the items (14) arriving at a loading station (4) are determined. If two or more items (14) with matching sorting processe...
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WO/2022/270856A1 |
The present invention relates to a drone having a laser beam emission function, wherein a laser beam may be emitted during fight, and thus, a visible range of a place for landing may be easily checked with the naked eye through the emiss...
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WO/2022/266806A1 |
A moving platform (1000), comprising a body (200) and an obstacle avoidance assembly (100), wherein the obstacle avoidance assembly (100) is mounted on the body (200); the obstacle avoidance assembly (100) comprises a plurality of vision...
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WO/2022/269487A1 |
In a first aspect, the present application relates to a method for the treatment of black water, comprising the steps of: collecting black water; treating said black water in an electrocoagulation cell with iron or aluminum electrode, su...
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WO/2022/269762A1 |
[Problem] The present invention makes it possible to provide an aerial vehicle in which, during flight of the aerial vehicle, the influence of wind which hits the frame in a prescribed direction is reduced, and fuel efficiency and stabil...
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WO/2022/267987A1 |
Disclosed are a shock-absorbing device, a gimbal and an unmanned aerial vehicle, relating to the technical field of aircrafts. The shock-absorbing device comprises: a first fixing plate; second fixing plates, which are arranged at interv...
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WO/2022/270337A1 |
A backup satellite group (22) including a plurality of satellites (30) stands by at an orbital altitude lower than the orbital altitude of a stationary operation satellite group (21) in a satellite constellation (20). When a satellite (3...
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WO/2022/269061A1 |
The invention relates to a seat device (12a; 12b; 12c), in particular an aircraft seat device, said seat device comprising a backrest (20a; 20b; 20c) having: a base frame (24a; 24b; 24c) which comprises two lateral frame elements (26a, 2...
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WO/2022/266879A1 |
A fault detection method and apparatus for a plant protection system, and a movable platform and a storage medium. The plant protection system is carried in the movable platform. The method comprises: during the process of a movable plat...
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WO/2022/266869A1 |
An unmanned aerial vehicle, having a landing state and a flight state, and comprising: a housing (11) provided with a photographing window (11a); a camera (12) provided in the housing (11) and facing the photographing window (11a); a pro...
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WO/2022/271429A1 |
A vehicle includes a fuselage, a wing, a pylon that is coupled to the wing, and a tractor tiltrotor. The tractor tiltrotor is coupled to the pylon and is located forward of the wing; the tractor tiltrotor tilts upwards during a hover mod...
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WO/2022/271136A1 |
The present invention relates to the charging apparatus and the transmission of electrical power to the charging apparatus for charging the energy consumption devices using in-depth contact tips and for stable/mobile energy consumption d...
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WO/2022/266836A1 |
A heat dissipation structure, a movable platform and a heat dissipation control method. The heat dissipation structure comprises a heat dissipation bracket (100), an airflow generation assembly (200) and a shunting assembly (300). At lea...
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WO/2022/269309A1 |
The present disclosure relates to an autonomous, electric, vertical takeoff and landing (VTOL) aircraft that is low-noise, safe, and efficient to operate for cargo transportation over relatively long ranges. A VTOL aircraft includes a fu...
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WO/2022/271835A1 |
A flame arrestor which will generally comprise two hollow sections, each of which includes a plurality of hollow channels, and with a throat between them which is open. This open portion can be used to induce turbulent flow into fluid wh...
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WO/2022/271436A1 |
An air and road vehicle system includes a road vehicle having a chassis, a plurality of wheels, an engine, and a cabin area. A flight vehicle having a main body, wings, flight control surfaces, and a plurality of propulsion devices is re...
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WO/2022/269597A1 |
A connection system is provided for releasably connecting a first component and a second component in a first direction parallel to a reference longitudinal axis, including one or more locking devices and an actuator. Each locking device...
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WO/2022/266807A1 |
An unmanned aerial vehicle (100), comprising a fuselage (10) and a plurality of arms (20). The plurality of arms (20) are rotatably connected to the fuselage (10) to allow the unmanned aerial vehicle (100) to be in a folded state or an u...
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WO/2022/261691A1 |
The invention relates to an aircraft (1), more particularly a drone, and to a corresponding method for cleaning especially substantially flat surfaces that are preferably delimited by a frame (5), especially of windows or doors. The airc...
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WO/2022/263660A1 |
The invention relates to an aircraft landing gear (1) comprising a stationary element and at least one movable element which can move relative to the stationary element between a first position and a second position, and detection means ...
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WO/2022/264671A1 |
The present invention addresses the problem of providing a system that, when a plurality of aircraft approach one landing field, enables safe and efficient takeoff and landing. A control device (120) according to the present invention ma...
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WO/2022/266597A1 |
An Intermediate Load Attachment Platform (ILAP) for attaching a cargo load to at least one main parachute, the ILAP protects a release mechanism disposed at least partially therein, the release mechanism is coupled to a drogue mechanism,...
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WO/2022/263947A1 |
A convertible aircraft (1, 1') with an airframe (2) defining a first longitudinal axis (Y) is described; a pair of half-wings (3); a first, a second, a third, a fourth, a fifth and a sixth rotor (20a, 20b, 21a, 21b, 22a, 22b) rotatable a...
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WO/2022/263777A1 |
The invention relates to an aircraft flight compensator comprising a friction module (8) that has variable friction and is coupled on one side to a drive shaft (11) and on the other side to an output shaft (13) via a kinematic chain (12)...
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WO/2022/263327A1 |
A cargo drone wherein the goods transported by the cargo drone are arranged inside a hold (C), which can be positioned longitudinally in various ways with respect to the aerodynamic center of gravity (X) of the fuselage (A) of the elemen...
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WO/2022/263911A1 |
A structure for an unmanned aerial vehicle is provided. The structure includes a wing-type fuselage (20). The structure also includes at least two fixed wings (40) which form a fixed-wing platform (70) of a cropped delta wing structure w...
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WO/2022/261720A1 |
A swashplate assembly for controlling rotor blades of a rotorcraft, comprising a rotating assembly, wherein the rotating assembly is arranged to rotate with the rotor blades about an axis and is coupled to the rotor blades; a base assemb...
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WO/2022/263512A1 |
A lift structure for an aerodrome structure comprises: an upstanding tubular frame comprising an upper ring located over a base ring and supported thereon by columns; a platform located within the tubular frame; and a lift mechanism arra...
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WO/2022/263949A1 |
A series of convertible aircraft (1, 1') with a core (100) with an airframe (2) defining a first axis (Y) is described; a first, a second, a third, a fourth, a fifth and a sixth rotor (20a, 20b, 21a, 21b, 22a, 22b) which are rotatable ab...
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WO/2022/263365A1 |
The invention relates to an on-board system for detecting impacts on the fuselage (110) of an aircraft (100), comprising: a plurality of impact sensors (2) arranged on a plurality of areas of the fuselage, each sensor (2) being capable o...
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WO/2022/263753A1 |
The invention relates to a system (40) for changing the pitch of the blades of a turbomachine propeller, each blade (25) being mounted so as to pivot about a pitch axis (A), the system comprising a control means and a connection mechanis...
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WO/2022/261688A1 |
The invention relates to a vacuum tank (1) for a vacuum toilet, which tank comprises an inlet opening (2) which is located in a side wall of the tank and can be connected to the main drain (4) of a bowl (5) via a valve (3), and comprises...
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WO/2022/261864A1 |
A control method and apparatus for an unmanned aerial vehicle system, and an unmanned aerial vehicle system and a storage medium. The unmanned aerial vehicle system comprises an unmanned aerial vehicle and a parachute mounted on the unma...
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WO/2022/263752A1 |
The invention relates to an unducted rectifier for a turbomachine comprising: - stator vanes (23) each comprising a root (25) and a blade (24) radially projecting from the root, the root comprising two half-platforms (40A, 40B) extending...
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WO/2022/263588A1 |
A method for producing a stiffened structural aircraft panel, comprising the following steps: - manufacturing a web (2) by shaping a metal sheet; - manufacturing a stiffener (3) comprising an attachment edge (7) and a reinforcing edge (5...
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WO/2022/265787A1 |
A hinge includes internal on-axis stopping mechanisms that cause the hinge to shear and break at an on-axis weakened region of the hinge when rotation of the hinge reaches a predetermined angle with a specified torsional load. The on-axi...
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WO/2022/264696A1 |
Provided are a flight vehicle operation management system and a flight vehicle operation management method for airports, said system and method enabling improved airport utilization efficiency at an airport which is for the takeoff and l...
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WO/2022/263770A1 |
The invention relates to a de-icing system which comprises: - actuators (210) attached to the part (106); and - a device for controlling the actuators (210) in order to vibrate the part (106). The control device is designed for the follo...
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WO/2022/264665A1 |
Provided is a flight vehicle control system that performs proper control on flight vehicles capable of vertical takeoffs and landings and that enables the flight vehicles to perform takeoffs and landings safely in a dense state in accord...
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WO/2022/264177A1 |
Electromagnetic propulsion system for spacecraft movement without the emission of reaction mass, characterised in that it comprises two arms (10) which share one of their vertices at a point called feedpoint (14); said feedpoint (14) bei...
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