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WO/2021/005057A1 |
A hybrid propulsion chain (1) for an aircraft, the hybrid propulsion chain (1) comprising a plurality of propulsion rotors (R1-RX) connected to an electrical distribution module (10) by a plurality of electrical connections (E1-E4), the ...
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WO/2021/004110A1 |
A water-air amphibious cross-medium bionic robotic flying fish, comprising a body, pitching pectoral fins (4), structure variable pectoral fins (5), a tail propulsion module, a detection sensor and a controller. The present invention con...
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WO/2021/006725A1 |
A fuselage structure of an aircraft is described. The fuselage structure comprises a fuselage skin, and a plurality of frame elements (30), spaced apart from one another in a direction parallel to the aircraft longitudinal axis for suppo...
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WO/2021/003551A1 |
The engine is adapted to generate thrust or designed to generate torque includes a combustor, the combustor generates an exhaust gas flow to push the rotor blades of a rotor in a rotor housing, the exhaust gas flow rotates the rotor, sha...
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WO/2021/005304A1 |
The invention relates to an electric propulsion architecture for a multi-rotor vertical take-off and landing aircraft, comprising: - four electric generators (G1-G4); - four pairs of rotors (R1_2 ‐ R2_1; R3_4 ‐ R4_3; R5_6 ‐ R6_5; R...
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WO/2021/005942A1 |
This unmanned flight vehicle (100) is provided with: a microphone (103) having a plurality of elements (131); and a processor (101) which processes signals outputted from the plurality of elements (131), wherein the processor (101) execu...
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WO/2021/007216A1 |
Technologies are described herein for a drag recovery scheme using a boundary layer bypass duct system. In some examples, boundary layer air is routed around the intake of one or more of the engines and reintroduced aft of the engine fan...
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WO/2021/005050A1 |
A movable flow body device for an aircraft is proposed, comprising an elongated flow body having a main extension axis, a first mechanical interface in a first position along the main extension axis, a second mechanical interface in a se...
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WO/2021/005595A1 |
There is provided a composite air vehicle system including: a first air vehicle capable of independent aerodynamic flight; a second air vehicle capable of independent aerodynamic flight; and at least one connector element configured for ...
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WO/2021/005044A1 |
The invention relates to a system for updating data for computing devices in an aircraft (10) in which at least one computing device (1401) of a first group of computing devices is, when the data of the computing device are updated, pron...
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WO/2021/006339A1 |
[Problem] The present invention addresses the problem of safely moving or landing an aerial vehicle having a plurality of rotor blades when trouble has occurred in a power source. [Solution] An aerial vehicle having a plurality of rotor ...
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WO/2021/005166A1 |
The invention relates to a tactile interface (1) comprising a touch pad (3) and a support (2), the touch pad (3) being hingedly attached to the support (2) between an extended active position and a retracted inactive position, in which t...
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WO/2021/004889A1 |
A skew detection system for an aircraft flight control surface, the flight control surface being moveable relative to fixed structure of the aircraft by operation of a first gear rack driven by a first gear pinion and by operation of a s...
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WO/2021/005809A1 |
A controller (2): obtains a first horizontal distance and a first vertical distance, which are a component in a horizontal direction and a component in a vertical direction, respectively, of a distance, from an unmanned aerial vehicle (1...
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WO/2021/000628A1 |
Disclosed is a bionic robotic manta ray, comprising a head cabin, a central cabin, a pair of pectoral fins, and a caudal fin cabin, wherein each of the pectoral fins comprises a crank and rocker mechanism and a bevel gear mechanism, and ...
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WO/2021/002094A1 |
Provided is an aerial vehicle having a control unit that sets a horizontal ground speed on the basis of wind information containing information relating to wind direction and wind speed.
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WO/2021/002881A1 |
The present invention provides an unmanned aerial vehicle ("UAV") operations system for cleaning one or more designated surfaces such as a solar panel installed on a roof, or the surface of a window, wall, billboard, scoreboard, etc., wh...
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WO/2021/001081A1 |
The invention relates to a device for starting and/or maintaining jet engines of aeroplanes and other aircraft and, optionally, for air conditioning the aeroplanes and other aircraft, said device comprising at least one compressor (10) a...
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WO/2020/182692A3 |
The invention relates to an androgynous coupling means (10) exhibiting both male and female coupling sections, wherein the androgynous coupling means is configured for form fit coupling with at least one further androgynous coupling mean...
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WO/2021/001636A1 |
The invention concerns an aircraft seat comprising an actuator and a movement transmission device comprising: - a frame (20) provided with an immobilising part (52), - a drive shaft (30), - a gear wheel (34) provided with coupling teeth ...
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WO/2021/000028A1 |
The invention relates to a novel vertical take-off and landing cocoon-type flying vehicle that pertains to the field of articles for air transportation, preferably for use in individual transportation, but optionally capable of being con...
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WO/2021/002232A1 |
The present invention provides a resin composition which is capable of effectively blocking neutrons and is suitable as a material for aircraft. The present invention specifically provides a resin composition which contains an aromatic p...
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WO/2020/247148A9 |
An electrically powered vertical takeoff and landing aircraft (EVTOL) includes a payload module, a plurality of electrical power sources, a wing, and a plurality of electric thrust generators. The wing is pivotally attached to the payloa...
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WO/2021/002521A1 |
A drone take-off control method using a drone station is disclosed. A drone take-off control method using a drone station, according to one embodiment of the present invention, acquires, from a drone station, time information about the m...
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WO/2021/001734A1 |
The aim of the invention is a device for detecting the approach of a vortex ring state for a rotary-wing aerodyne (10), said detection device comprising a set of vibration sensors (16a, 16b, 16c) configured to be distributed in or over t...
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WO/2021/002204A1 |
Provided is a structure for freely changing the arrangement interval of seats (2) inside a passenger compartment (1) of a vehicle. The structure comprises: a support frame (3) that supports the seats (2) from below, as a cantilever, and ...
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WO/2021/001295A1 |
The invention relates to an electronic arrangement for an aircraft (1), an aircraft having a structure and such an electronic arrangement (3) and a method for providing such an electronic arrangement (3). The electronic arrangement has a...
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WO/2020/243364A3 |
The subject matter described herein relates to aircraft designs and more particularly to aircraft designs using tandem wings and a distributed propulsion system. The embodiments described enable synergies between aerodynamics, propulsion...
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WO/2021/002320A1 |
According to the present invention, in a display area (D) of a display device of a maneuvering device (30), the image (C) of a power transmission line as a subject is displayed. When the power transmission line is imaged from a position ...
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WO/2021/001945A1 |
The present invention provides a spectroscopic imaging device (1) including: a spectroscopic unit (2) that includes a field diaphragm (2d), a shading optical element (2c), a dispersion element (2f), and a two dimensional detector (2h); a...
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WO/2021/000047A1 |
The present disclosure relates to a low mass system for releasably securing a robotic arm to a spacecraft and also securing various payloads to the robotic arm and to each other, permitting the robotic arm to be both moved from one locat...
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WO/2020/260391A1 |
A leading-edge arrangement for an aircraft is proposed, comprising a plurality of movable flow bodies, a supply duct, an air transfer duct, and at least one perforated tube, wherein the movable flow bodies are arranged in a consecutive a...
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WO/2020/260394A1 |
Disclosed is a wing (3) for an aircraft (1), comprising a fixed wing (5), a foldable wing tip portion (9) and a flight latch device (17) for latching the foldable wing tip portion (9) in the extended position, wherein the flight latch de...
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WO/2020/262189A1 |
The present disclosure relates to a mobile body, a control method, and a program which make it possible to achieve safer movement and stopping. On the basis of external environment information on an external environment, a safety level e...
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WO/2020/259748A1 |
The invention relates to a device for preventing access to an area on an aircraft, having a first vertical jamb (8) and a second vertical jamb (9) for fastening to a structure of the aircraft and having a barrier element (13), which is d...
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WO/2020/260010A1 |
The invention comprises an assembly (200) comprising a mast (106) with an upper spar (202) and two lateral blades (230), a wing (104) with a skin (210) and a front spar (208), port/starboard front/rear brackets, each with a housing (218,...
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WO/2020/260644A1 |
The invention relates to an aircraft cabin device comprising at least one first aircraft seat row (12a; 12b; 12c; 12d; 12e; 12f; 12g; 12h), which comprises at least two aircraft seats (16a, 18a, 20a; 16b; 16c; 16d;16e, 18e; 16g, 18g, 20g...
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WO/2020/260642A1 |
The invention relates to an aircraft cabin device comprising at least one first aircraft seat row (12a; 12b; 12c; 12d), which has at least two aircraft seats (16a, 18a, 20a; 16b, 18b, 20b; 16c, 18c, 20c; 16d, 18d, 20d) that are aligned i...
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WO/2020/260678A1 |
Disclosed and described is an aircraft galley (1) having a plurality of galley inserts (GAINs) (3) and a master aircraft galley control unit (MGCU) (5), wherein the galley inserts (3) are connected to the MGCU (5) via an aircraft galley ...
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WO/2020/261470A1 |
A control device (100) comprises an acquisition unit (110) that acquires transport article information indicating characteristics of an article being transported, and a generation unit (130) that generates transport control information t...
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WO/2020/259570A1 |
Disclosed in the present invention are a modular intermeshing and tandem unmanned helicopter and a working method thereof. The modular intermeshing and tandem unmanned helicopter is composed of two helicopter units which are connected to...
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WO/2020/260150A2 |
A self-propelled drive unit for moving aircraft on the ground, with a receiving region for receiving at least one wheel unit, which can be rotated about a wheel axis, of a nose wheel unit of an aircraft to be moved, and with an automatic...
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WO/2020/264487A1 |
A distributed control system for a vehicle includes a configuration controller and at least three nodes communicatively coupled to the configuration controller. Each of the at least three nodes includes a memory device for storing local ...
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WO/2020/262528A1 |
In the present invention, a server device 20 controls a flying object 10 to cause the flying object to fly close to a transmission line and photograph the transmission line. The flying object 10 is equipped with a GPS positioning device,...
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WO/2020/261102A1 |
An aircraft, in particular a drone or an aircraft for personal air mobility, comprises at least one horizontal planar structure (2), wherein four ducted propeller rotors (3) with vertical axis are incorporated, which are substantially co...
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WO/2020/263528A1 |
An overhead storage bin display system that includes an overhead storage bin defining a bin interior and a display member associated with the overhead storage bin. The display member is configured to display passenger related information...
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WO/2020/263266A1 |
A portable electronic device holder for a passenger seat includes a base plate, a back plate pivotally attached to the base plate, and at least one movable arm attached to the back plate. The back plate may be adjustable relative to the ...
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WO/2020/259822A1 |
The present disclosure relates to a method for providing assistance to a vehicle (100, 102, 104), specifically by means of an unmanned aerial vehicle (UAV) (206) comprised with the vehicle (100, 102, 104), where the UAV (206) is provided...
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WO/2020/242477A8 |
Propulsion systems, such as electro spray thrusters, may include an electrically actuated valve to permit a selective flow of propellant to a thruster. The valve may be located and arranged such that it physically separates a propellant,...
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WO/2020/260399A1 |
Disclosed is a wing (3) for an aircraft (1), comprising a fixed wing (5), a foldable wing tip portion (9), and a flight latch device (17) for latching the foldable wing tip portion (9) in the extended position, wherein the flight latch d...
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