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WO/2024/076837A1 |
A method for carrying a payload (150) using a multi-rotor flight vehicle (MRFV) (130), including receiving an indication that the payload (150) is connected to the MRFV (130), receiving an input from the payload (150), determining, from ...
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WO/2024/074775A1 |
The invention relates to a radiant heating device (2) for an aircraft, the device comprising a heating layer (4) provided with at least one anode (6) and at least one cathode (8), a front protective layer (10) and a rear protective layer...
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WO/2024/076290A1 |
A single-wing rotorcraft with multiple flight modes is provided, including: a frame member; a wing member coupled to the frame member; a flap member rotatably coupled to the frame member; a first thrust unit rotatably coupled to the fram...
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WO/2024/076124A1 |
Proposed are a method by which a first device performs wireless communication and an apparatus supporting same. For example, the first device may acquire information related to a PRS configuration. For example, the information related to...
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WO/2024/073807A1 |
A portable power hub comprising a housing comprising one or more batteries for storing energy; one or more photovoltaic arrangements adjustable relative to the housing and electrically connected to the one or more batteries for charging ...
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WO/2024/074680A1 |
The present invention relates to a recognition device (10) for recognizing empty trays (LW) in a conveying device (100) for trays (W) for transporting objects (O), comprising: an inspection light source (20) for generating inspection lig...
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WO/2024/076396A2 |
A method includes determining, by an unmanned aerial vehicle (UAV), a position of an autoloader device for the UAV; based on the determined position of the autoloader device, causing the UAV to follow a descent trajectory in which the UA...
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WO/2024/076966A1 |
A system for an aircraft includes a tiltable proprotor that is tiltable between a lift position for providing lift for the aircraft and a forward flight position for providing forward propulsion for the aircraft is provided. The system i...
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WO/2024/077213A1 |
In one embodiment, an electrical propulsion system includes an electrical motor configured to drive one or more propellers of the aircraft, a capacitor configured to stabilize a direct current (DC) bus voltage, a first inverter circuit c...
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WO/2024/074448A1 |
The invention relates to an injector (3) for a de-icing device for an air intake of an aircraft turbojet nacelle, the injector (3) comprising a peripheral member (30) internally defining a passage duct (6), the peripheral member (30) com...
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WO/2024/076447A1 |
An air hose includes a first component, a second, elastic component and one or more fastening positions and/or a continuous fastener. The first component has a first end and a second end, wherein the first and second ends of the first co...
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WO/2024/075276A1 |
[Problem] To provide a flight vehicle capable of improved fuel efficiency while cruising. [Solution] A flight vehicle 100 according to the present technology comprises: a plurality of rotor blades 11; a main body 50 supporting the plural...
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WO/2024/077280A1 |
An electric propulsion system for a vertical takeoff-and-landing aircraft having an inverter assembly, a gearbox assembly, an electric motor assembly. The inverter assembly, the gearbox assembly, and the electric motor assembly may be su...
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WO/2024/076965A1 |
A system includes a first frame for mounting to the aircraft; a second frame for mounting the proprotor, the second frame being rotatably mounted to the first frame; a first gear located along the rotation axis of the second frame and fi...
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WO/2024/074743A1 |
The invention relates to a microthruster applicable to space engineering that comprises printed circuit boards (PCBs) connected to each other, wherein the first board comprises a fuel tank (1) and an outlet nozzle (2) and the second boar...
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WO/2024/077260A1 |
A tilt propeller for a vertical takeoff and landing (VTOL) aircraft includes a tilt actuation assembly for moving a tilt propeller between a lift configuration and a cruise configuration. The tilt actuation assembly may comprise multiple...
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WO/2024/074862A1 |
A magnetic arrangement for a solid state propulsion system. The propulsion system includes a spiraling inward and upward cone shape permanent magnet made of magnetic material such as superconductors or neodymium magnets. The propulsion s...
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WO/2024/074822A1 |
In some examples, a wing for an aircraft, the wing having a passive variable aeroelastic geometry for accommodating efficient flight at multiple aircraft speeds, comprises a wing skin comprising a composite structure comprising a laminat...
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WO/2023/137082A9 |
A satellite includes a structural element that is deformable during a collision with space object(s). The structural element includes a first side, a second side spaced apart from the first side to define an interior portion between the ...
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WO/2024/074543A1 |
Vertical take-off and landing aircraft (1) comprising a fuselage (2), at least one propulsion system (5), at least four lift propellers (10) and at least two fixed wing planes (20, 30, 40). The fixed wing planes (30, 40) which are locate...
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WO/2024/076775A2 |
Implementations described and claimed herein provide apparatus and methods for accessory attachment. One example apparatus includes an attachment device having a base plate, a support structure on the base plate, at least one pole, where...
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WO/2024/076945A1 |
A soap or sanitizer dispenser including a housing and a receptacle for receiving a refill unit. The refill unit includes a container with a neck and a closure, with the neck at the lower most position of the container when the refill uni...
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WO/2024/077248A1 |
An electrical propulsion system for a vertical take-off and landing (VTOL) aircraft comprises an electrical motor assembly and an inverter assembly. The inverter assembly comprises a housing, a capacitor assembly, at least one printed ci...
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WO/2024/069095A1 |
Device (210) for measuring a rotational speed of an aircraft propeller (211), comprising: - an optical speed sensor (220); - an optical fiber (230) connected to the optical speed sensor and intended to be connected to a control unit of t...
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WO/2024/072711A1 |
A system for predicting vegetation encroachment into a utility asset that includes a remote sensing controller that stores a set of 3D data characterizing a utility asset and vegetation in a digital twin database. The digital twin databa...
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WO/2024/069103A1 |
The invention relates to a control device including a mechanical seal (24) which guides the rotation of a control lever (22) relative to a frame (20) about two pivot connections of orthogonal axes. The mechanical seal (24) comprises, for...
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WO/2024/065001A1 |
Slope monitoring systems, prism assemblies and drones are provided, which alleviate the need for personnel to access a slope to be monitored, significantly reducing risk associated with rockfall. The slope monitoring system includes a pl...
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WO/2024/068275A1 |
The invention relates to an assembly with a mechanism (2) for locking a door (1a) in circular translation, the door being of the vehicle semi-plug type. The mechanism (2) comprises a handle (3) actuating a rotation of the door (1a) on it...
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WO/2024/068607A1 |
According to a first aspect of the disclosure, there is provided a firearm mount assembly for a wearable flight system. The firearm mount assembly comprises a firearm mount and an actuator. The firearm mount is configured to rotate about...
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WO/2024/066918A1 |
A fixed-wing aircraft having vertical take-off and landing electric rotors and driven by a fuel power to fly forwards, comprising vertical take-off and landing electric rotor mechanisms (6) embedded in a fixed wing (2) or/and in an empen...
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WO/2024/066601A1 |
A preparation method for an aircraft cargo hold floor, and an aircraft cargo hold floor. The preparation method comprises the following preparation steps: separately preparing phenolic resin upper panel layers (4), phenolic resin lower p...
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WO/2024/069788A1 |
[Problem] To ensure safety during aerial photography. [Solution] A mobile body system 1 comprising a mobile body 100 that flies in a subject area F and a flight mode switching unit 330 for switching flight modes M102 and M105 in which fl...
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WO/2024/067896A1 |
The invention relates to an aircraft, comprising a body, at least four arms and/or supporting surfaces arranged on the body at a respective one end and extending away from the body with a respective free end, vertical and/or lateral rudd...
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WO/2024/073763A1 |
Carbon nanostructure-based composites and methods of making and using thereof are described. The carbon nanostructure-based composites may be single-layered or multi-tiered composites. Such composites can be useful for radiation shieldin...
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WO/2024/073166A2 |
Systems and methods for charging unmanned aerial vehicles (UAVs) using ultra-low frequency wireless power transfer technology are disclosed herein. In some embodiments, a UAV can carry a wireless power transfer (WPT) unit configured to t...
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WO/2024/068395A1 |
The invention relates to a rocket engine (100, 200, 300, 400) comprising a first tank (102) and a second tank (106), wherein the first tank is filled with a fuel and the second tank with an oxidising agent, such as liquid hydrogen peroxi...
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WO/2024/073373A1 |
Rudder pedal input control devices (100, 200, 300, 400A, 400B, 500, 600) are described that utilize a straight-line mechanism and rotary joints to achieve straight line motion in a compact volume. The devices include bar linkages (106, 1...
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WO/2024/069790A1 |
[Problem] To achieve labor efficiency in photography work and to make it possible to perform appropriate photography according to the situation of a photography subject. [Solution] An aerial photography system 1 comprises: a mobile body ...
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WO/2024/068661A1 |
A control unit (6, 7) is indicated for controlling the pitch of an aircraft (1), the control unit (6, 7) comprising at least one adjustable control element (6) and an adjustment mechanism (7) for actively adjusting the at least one contr...
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WO/2024/065917A1 |
A reconfigurable blended wing vertical take-off and landing aircraft, comprising a fuselage, wings, canards, and a cabin door. The wings are respectively arranged on the two sides of the fuselage, two rotor wing modules are respectively ...
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WO/2024/069669A1 |
[Problem] To provide an information processing system or the like capable of extracting only an edge of a near or far object. [Solution] According to one embodiment of the present invention, provided is an information processing system o...
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WO/2024/071521A1 |
The present invention relates to a sensing structure for diagnosing a drone drive system, and a block-type diagnostic device for a drone drive system, including the sensing structure, in which a plurality of diagnostic sensors for measur...
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WO/2024/072361A1 |
The present invention relates to a body (B); at least a first piece (2) located on the body (B); at least a second piece (3) positioned opposite the first piece (2); a plurality of extensions (201) made of a flexible material, located on...
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WO/2024/072596A1 |
A roller-and-rail cargo handling system that includes tracked rollers and side rails for receiving cargo pallets. A trolley system is used to move the pallets along the tracked rollers, which includes a trolley movable along a trolley tr...
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WO/2024/069633A1 |
During aircraft descent, flight control systems seek and maintain a glide slope determined from a single pilot input parameter; e.g., the position of a control axis of a flight stick. Appropriate guide slope selection by the pilot is rea...
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WO/2024/071577A1 |
The present invention relates to a lunar gravity simulation system for testing performance of a lander, characterized by comprising: a plurality of first frames extending in the height direction; a plurality of second frames extending in...
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WO/2024/071410A1 |
Provided is a liquid storage container in which a device is disposed and with which high durability can be achieved.　This liquid storage container includes: a seamless cylindrical container body in which a storage chamber capable of st...
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WO/2024/069210A1 |
The present invention concerns a method of manoeuvring a vertical take-off and landing, unmanned aerial drone (100) comprising at least an aerodynamic surface (101), wherein, during a flight of the drone, the aerodynamic surface generate...
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WO/2024/065886A1 |
A fire-fighting unmanned aerial vehicle cluster (1), comprising a ground platform (200) and N unmanned aerial vehicles (100) arranged at intervals. The ground platform (200) comprises a main water pump. Each unmanned aerial vehicle (100)...
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WO/2024/073696A1 |
A method and apparatus for aerial delivery of a package dropped from an elevated location. The apparatus includes a main body having an internal compartment for receiving a package to be delivered. A controllable component is detachably ...
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