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WO/2023/034883A1 |
A factory for manufacturing useful products while orbiting is space uses concentrated solar energy, high vacuum, and the low temperatures available in a space environment. Gyroscopic forces from rotating machinery are carefully controlle...
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WO/2023/034291A2 |
The disclosed methods, systems, and kits provide the ability to deliver entire clean sheet designs from concept to first hot fire in under six weeks with instant specific impulses above 330 seconds in some of our engines. In examples, th...
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WO/2023/023828A1 |
The present invention relates to an innovative type of electric and/or hybrid digital glider drone with a steerable balloon for personal flight. The project consists of a compact ellipsoidal balloon with a self-levelling drone with rigid...
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WO/2023/026662A1 |
The present invention provides a skin member and a blade structure which are lightweight yet ensure strength. A skin member (100) forms an outer plate of the blade structure, and comprises: a lattice-like framework material (110) forming...
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WO/2023/025754A1 |
An interface system for cabin trolleys for a vehicle is proposed, comprising a first interface device attachable to a monument inside the cabin, a second interface device attachable to a cabin trolley, wherein the first interface device ...
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WO/2023/023697A1 |
Provided is a sensor magazine arrangement (10) for a drone (8), the arrangement (10) comprising a chassis (14) configured to receive at least a portion of a drone (8) to position a load point (26) of such drone (8) relative to the chassi...
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WO/2023/025532A1 |
The invention relates to a secure and removable attachment system (3) for attachment of a device (1) to a panel (2) comprising mortises (2c). This attachment system (3) comprises an attachment head (4a), a body (4) provided with feet ins...
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WO/2023/028500A1 |
Aspects of the present disclosure relate to a sample collection assembly for a vehicle. The sample collection assembly includes a perforated ground-engaging member of the vehicle and an associated sample collector. For example, a perfora...
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WO/2023/027892A1 |
Technology is disclosed herein for a spacecraft launch restraint and dispensing structure (100). The dispensing structure (100) has a number of trusses (110) and a central structure (104). When the trusses (110) are in a support position...
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WO/2023/025846A1 |
The present invention relates to a power conversion system for electrically-powered thrusters located on and/or inside a satellite.
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WO/2023/024968A1 |
A variable-stroke self-adaptive adjustment quasi-zero stiffness device and a parameter checking method, comprising: an integrating sphere, a target, a collimator, a pointing measuring instrument, disturbance sources, an inertia simulatio...
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WO/2023/026616A1 |
[Problem] The present invention can provide a flying object that has improved fuel consumption and can transport articles. [Solution] This flying object comprises a loading part that holds a delivery, the loading part or the delivery bei...
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WO/2023/027414A1 |
The present invention relates to various structures of vertical take-off and landing flying cars which can both travel on ground and fly. In connection with arranging motors for independently driving respective wheels on the basis of a f...
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WO/2023/027679A1 |
Proposed is a stationary ion/plasma engine comprising: a discharge chamber having an annular ionization and acceleration channel and a bottom with an inner seating surface for an anode, said chamber being made of an electrically insulati...
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WO/2023/023703A1 |
The present invention is directed to a delivery system for delivering one or more goods including at least one delivery container that is adapted to be picked up and released from at least one UAV, at least one delivery container recepta...
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WO/2023/028334A1 |
A system for swapping one or more batteries includes a battery holder configured to store a first battery, wherein the battery holder further includes retainers positioned proximate a front end and a rear end of the battery holder, the r...
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WO/2023/025942A1 |
A reconfigurable, modular, and scalable space infrastructure which provides a large diversity of services on demand in space, comprising a master truss (101) for housing systems of the space infrastructure to provide several services thr...
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WO/2023/026011A1 |
The invention relates to a spacecraft comprising: a frame (4), an electrical device (1) supplied and/or controlled by electric cables, and an orientation system for orienting the electrical device (1), the orientation system comprising: ...
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WO/2023/027773A1 |
A case for carrying loads by an Unmanned Aerial Vehicle (UAV) comprises a first end comprising a first cap and a first opening and a second end comprising a second cap and a second opening, the second opening being smaller than the first...
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WO/2023/027612A1 |
The inventions relate to the field of aviation. An aircraft comprises a multisided body having rotatable cylinders (1) mounted about the perimeter thereof. For supplying air into the aircraft, the body is provided with inlets (2) that le...
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WO/2023/028276A1 |
The present invention is a system and method for modifying a passenger aircraft and converting it for use as a cargo aircraft, wherein the steps include removing all structures that were previously put into the aircraft to accommodate pa...
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WO/2023/027902A1 |
A canister (200) is coupled to a delivery vehicle using a rail bracket (300). The canister comprises a securing channel having a first securing channel volume (216) and a second securing channel volume (218). A width of the first securin...
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WO/2023/027893A1 |
Technology is disclosed for a spacecraft launch restraint and dispensing structure. Stacks of spacecrafts (102) may be arranged around a central post (104). The dispensing structure has primary tie-down mechanisms (120) that axially clam...
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WO/2023/025441A1 |
A description is given of a method for the helicopter-assisted installation of high-voltage overhead lines (1) and elements (2) thereof and also an aerial vehicle for carrying out the method for laying power lines (3) and/or carrying out...
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WO/2023/024203A1 |
The present invention relates to the technical field of spacecraft control, and relates to a sun-oriented directional solar wing driving device. According to the sun-oriented directional solar wing driving device, two gear rings are resp...
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WO/2023/027908A1 |
In one aspect, this application describes a blade retention system―for a variable pitch aircraft proprotor system―comprising a double conical blade root encapsulated by a split sleeve. Some embodiments described additionally include ...
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WO/2023/026308A1 |
A landing and docking system for an unmanned aerial vehicle (UAV), the system comprises two main parts, a docking unit configured to be attached to a UAV and a mating ground base platform. The docking unit has clamping arms that can swin...
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WO/2023/026063A1 |
Spacecraft Heat Shield A deployable spacecraft atmospheric-entry heat shield (30, 40, 50, 60) is configured in a flasher pattern with a transformable polyhedral-surface. The transformable polyhedral-surface has a plurality of sectors (2,...
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WO/2023/027658A1 |
The present invention relates to a drone (1) used in fire extinguishing, which is used in fire extinguishing operations and reduces its damage from fire during its use.
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WO/2023/026338A1 |
[Problem] To provide a flight vehicle for which fuel consumption can be improved and which is capable of transporting an article. [Solution] This flight vehicle comprises a load part for holding a load, wherein, in a landed state or a ho...
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WO/2023/026016A1 |
An aircraft includes a chamber (1), a processor, a memory, and a compressor system (12b) in fluid communication with the chamber. The compressor system (12b) configured to selectively pressurize the chamber (1). The chamber supports a fu...
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WO/2023/024102A1 |
A control method for an aerial vehicle. The method comprises: during a cruising process of an aerial vehicle, controlling all rotors of a multi-rotor assembly to rotate, such that a lifting force is provided to the aerial vehicle by the ...
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WO/2023/027611A1 |
The invention relates to the design of unmanned vertical takeoff and landing aircraft. The claimed device comprises a multisided body having rotatable cylinders (1) mounted about the perimeter thereof. Situated inside the body is a gas i...
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WO/2023/028326A1 |
A landing system suitable for receiving an unmanned aerial vehicle (UAV) comprises an autonomous ground vehicle (AGV). A landing surface is disposed on the AGV, and the landing system comprises a loading channel suitable for passing an o...
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WO/2023/024049A1 |
The invention relates to the technical field of ventilation apparatuses, in particular to an efficient aerospace ventilation device with a heating function. In order to solve the problem of poor air quality due to most of the existing ve...
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WO/2023/027572A1 |
Unmanned Aerial Vehicle having an on-board hydrogen generator The present invention provides an unmanned aerial vehicle (100) that has VTOL and fixed wing capabilities. The unmanned aerial vehicle of the present invention is built to hav...
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WO/2023/026797A1 |
Provided is an engine-carrying flight device capable of stably hovering. An engine-carrying flight device 10 can fly in a hovering state, in which altitude is maintained, and in an ascending/descending state, in which altitude is chang...
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WO/2023/027736A1 |
A torque limiter includes a housing; an input shaft which is rotatably supported in the housing; an output shaft which is rotatably supported in the housing coaxially with the input shaft; and a ball detent mechanism which is connected b...
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WO/2023/023989A1 |
An electric motor (100), a power mechanism (200) and an unmanned aerial vehicle (300), the electric motor (100) comprising an electric motor seat (10), a rotating shaft (20) and a bearing assembly (50), wherein the electric motor seat (1...
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WO/2023/026672A1 |
Provided is an unmanned aerial vehicle capable of loading cargo so that the loaded cargo does not influence maneuvering stability. The unmanned aerial vehicle which flies in the air to transport the cargo comprises a cargo bed 210 and ...
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WO/2023/024311A1 |
Disclosed is a flexible space capsule, comprising a pneumatic apparatus, a solar power generation apparatus and a rotating apparatus. A capsule body comprises a first capsule body, a second capsule body and a third capsule body. Capsule ...
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WO/2023/027914A1 |
A thermally controlled payload container for carrying payloads by an Unmanned Aerial Vehicle (UAV) comprising an inner wall and an outer wall. The inner wall forms a chamber having an open end and a closed end. The payload container also...
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WO/2023/023608A2 |
In some embodiments, a video decoder decodes a video from a bitstream of the video using a history-based Rice parameter derivation. The video decoder accesses a binary string representing a partition of the video and processes each codin...
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WO/2023/022937A1 |
The present invention provides a system for use with UAVs to allow for mechanical activities at-height on elevated structures. According to a first preferred embodiment, the present invention includes multiple tool types which allow for ...
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WO/2023/019740A1 |
The present invention provides a cooperative transportation method and system based on multiple agents. The method comprises: constructing, according to the number of agents and formation requirements thereof, a multi-agent cooperative t...
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WO/2023/021948A1 |
In the present invention, after a drone 10 reaches the sky above a building designated as a destination of the drone 10, an inspection unit 12 inspects candidate landing positions at the destination on the basis of an image of the entire...
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WO/2023/021099A1 |
A system for controlling yaw during vertical take-off and landing (VTOL) operation of an airborne craft, where the airborne craft comprises multiple crossflow fan lift, propulsion and control elements (LPCEs) disposed around a central lo...
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WO/2023/021548A1 |
Provided is an unmanned aircraft that is capable of taking off stably. The fuselage 11 of the unmanned aircraft 1 has an information acquisition device 6, rotor blades 51-54, and a protective member 8 disposed around the rotor blades 5...
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WO/2023/023279A1 |
Systems and methods according to embodiments of the present technology vary engine throttle and flight control surfaces (such as high-lift devices, which can include flaps and/or slats) during takeoff, climb, approach, and/or landing of ...
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WO/2023/021188A1 |
A detector module (100, 300, 400, 500, 600, 802, 1102, 1604, 1610, 1614) for image capture, in particular for an optoelectronic image capture system (200, 700, 800, 900, 1000, 1100) for an aircraft, such as a spacecraft, comprising a mai...
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