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WO/2023/122624A1 |
A solar energy conversion system configured to increase a flux of photons from solar radiation can include a solar panel comprising a semiconductor substrate, a permanent magnet having a helical shape, an electromagnetic receiver, an ant...
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WO/2023/118688A1 |
The invention relates to a device (94) for transferring fluid, for a turbine engine (1) having a longitudinal axis X, which device includes a stator part (96) intended to be connected to a stator apparatus (98, 99) of the turbine engine ...
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WO/2023/119298A1 |
An unmanned aerial vehicle (UAV) is disclosed. The UAV comprises a body; a propulsion unit; a controller; and at least one adjustable camera unit. In some embodiments, each adjustable camera unit comprises, a camera; and a gimbal, mounti...
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WO/2023/118745A1 |
The invention relates to an assembly for an aircraft turbomachine (2), the assembly comprising: - a nacelle (1) comprising a fixed structure (11, 15, 16) that is suitable for being arranged around the turbomachine (2) comprising an inner...
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WO/2023/116153A1 |
A vertical takeoff unmanned aerial vehicle hangar system, comprising a hangar outer frame (100), a storage opening being provided on an upper side of the hangar outer frame (100); an inner side of the hangar outer frame (100) being provi...
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WO/2023/120657A1 |
Provided is a compact and lightweight power supply system installed in an electric vehicle. This power supply system for an electric vehicle comprises a battery system for supplying power to a drive unit of an electric vehicle, and a ran...
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WO/2023/117425A1 |
The invention relates to a mechanical drive connection assembly (1) for driving in rotation a carrier shaft (2) of a structure rotating about a central axis (2a) passing through this carrier shaft (2). This connection (1) comprises at le...
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WO/2023/121963A1 |
An access management system includes a mobile device with a processor and a memory and a software platform including at least a processor and a memory. The software platform is configured to analyze data obtained from the mobile device a...
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WO/2023/121784A2 |
A tiltrotor aircraft comprising a wing carrying an engine on each wing half, and a fuselage-mounted third engine with a transmission system configured to drive each of the tilting rotors from the third engine. The engines may be any powe...
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WO/2023/118725A1 |
The invention relates to a hydraulic control circuit (57) of a dual-action orientation actuator (61) for the orientation of fan blades of a turbojet engine, comprising an oil reservoir (63), a variable-displacement axial piston pump (26)...
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WO/2023/122350A2 |
A structural element, such as for use in conjunction with a satellite, may include one or more thin film solar cells, which are supported on a substrate, and a plurality of thin film antenna elements, which are supported on a carrier lay...
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WO/2023/118746A1 |
The invention describes an assembly for an aircraft propulsion system (2), comprising: - a nacelle (1) delimiting, together with the propulsion system (2), a fire zone (100, 200); - a fire extinguisher (3) comprising a nozzle (36) for sp...
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WO/2023/119209A1 |
The invention relates to an inflatable structure comprising a plurality of inflatable ribs attached to a flexible and foldable sheet, and to an inflatable deployment system that deploys such a structure. The inflatable deployment system ...
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WO/2023/119559A1 |
In the present invention, to make it possible to reduce the wait time for charging an unmanned aerial vehicle at a charging facility, information that can be used to determine the cruising range of an unmanned aerial vehicle is acquired,...
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WO/2023/119518A1 |
Provided is an engine generator unit which is for flying bodies and can be attached to various types of flying bodies while improving power generation responsiveness to load fluctuations of the flying bodies. When a target rotation speed...
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WO/2023/118689A1 |
The invention relates to a turbomachine module, having: - a fan comprising variable-pitch blades, - a speed reducer (34) connected to a fan shaft guided in rotation by two guide bearings, - a system for changing the pitch of the blades t...
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WO/2023/121436A1 |
Vertical take-off and landing (VTOL) aircraft of the fixed-wing type, comprising a centre section defining a centreline of the aircraft, and a pair of wings, arranged on either side of the centre section, wherein the wings extend longitu...
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WO/2023/121942A1 |
A payload retrieval apparatus is provided including a channel having a first end and a second end provided with a curved portion, wherein the channel has a tether slot therein and is configured to receive a payload retriever attached to ...
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WO/2023/122109A1 |
An aircraft has port side and starboard side propeller blades that each have a portion of the blade hidden or overlapping with the fuselage. This hidden or overlapping blade may extend into a slot of the fuselage. The advancing or retrea...
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WO/2023/120760A1 |
A method for operating a blasting system according to one embodiment of the present invention comprises the steps in which: a blast design device generates a blast design comprising at least one from among blast hole information, explosi...
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WO/2023/118297A1 |
An apparatus for preparing a ventilation gas mixture, the apparatus comprising: a first gas feed configured to receive carbon dioxide via a first gas valve; a second gas feed configured to receive oxygen via a second gas valve; a gas mix...
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WO/2023/116520A1 |
Disclosed herein is a spiral-propulsion-type spacecraft launching method, which comprises a method for launching a spacecraft from a celestial body in the solar system and a method for launching a spacecraft toward the outside of the sol...
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WO/2023/118773A1 |
An aerial imaging array comprising at least two imaging devices provided on a mount, attachable to an aircraft such that the imaging devices view downwards, wherein each imaging device has a field of view; wherein each imaging device has...
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WO/2023/119354A1 |
Provided is an engine generator unit which is exclusively for electric power generation and is capable of dampening the vibration of a horizontally-opposed engine without coupling the vibration. An engine generator unit 1, which is exclu...
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WO/2023/118724A1 |
The invention relates to a hydraulic control circuit (57) of a dual-action orientation actuator (61) for the orientation of fan blades of a turbojet engine, comprising an oil reservoir (63), a variable-displacement axial piston pump (26)...
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WO/2023/113908A1 |
An unmanned aerial vehicle (UAV) includes lift rotors and control rotors. The lift rotors are mounted to the UAV and oriented to provide a first vertical thrust to the UAV. The control rotors are mounted to the UAV outboard of the lift r...
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WO/2023/108578A1 |
An expert-type aerial robot system (100) for autonomous field work. The system comprises an unmanned aerial vehicle platform (110); a computer vision system (120), comprising a camera and a visual processor connected thereto; a robotic a...
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WO/2023/113394A1 |
An operating method of a smart drone for crime prevention, according to an embodiment of the present invention, comprises the steps of: receiving, from a wearable sensor worn on a subject to be guarded, a rescue request signal, an electr...
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WO/2023/111469A1 |
The present invention relates to an annular air intake lip (40) for a nacelle (3) of an aircraft propulsion assembly (1), the lip (40) extending about an axis of revolution (X) and comprising: - an external annular wall (42), - an intern...
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WO/2023/112245A1 |
One of the purposes of the present invention is to provide a management device that make it possible to properly calculate the tolls required for corridor transit. A management device according to one embodiment of the present disclosure...
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WO/2023/110542A1 |
An elevation system (1) for an aircraft seat (S), the elevation system (1) comprising a support base (2) comprising a right lateral part (21) and a left lateral part (22), a first frame (3) comprising a lower end (31) mounted such that i...
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WO/2023/114895A1 |
An aircraft tire component is disclosed herein, including natural rubber, a peptizer, carbon black, graphene, wherein the graphene has a thickness of less than about 3.2 nm, a particle size of between about 50 nm and about 10 µm, and co...
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WO/2023/113652A1 |
The invention relates to the field of aviation. The claimed rotary-wing aerial vehicle comprises a fuselage, a front wing having mounted at its ends propellers that are tilted forwards in the direction of flight, and a rear wing. Mounted...
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WO/2023/114402A1 |
Systems, methods and computer-readable media for telemetry data visualization are described herein. The described system includes paths and reduced components in between reception of sensor data and display to an engineer, reducing time ...
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WO/2023/112343A1 |
The present invention comprises at least two internal combustion engines, which are a first internal combustion engine (20) and a second internal combustion engine (22), and at least four rotary wings, which are a first rotary wing (12a)...
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WO/2023/114353A2 |
A fuel cell system (100) configured to provide electrical power to an electrical motor (102) producing propulsive thrust for an aircraft includes a plurality of fuel cell stacks (106) radially arranged about a central cavity (108). Fuel ...
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WO/2023/109154A1 |
Disclosed are a wing and a method for improving control efficiency of a two-dimensional airfoil rudder surface. According to the technical solution, an original symmetric airfoil rudder surface is transformed into an asymmetric airfoil r...
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WO/2023/111438A1 |
The invention relates to a hydraulic assembly (450) for an aircraft engine, the assembly comprising: - a pump (54) comprising a housing (54a) and a rotor (54b) arranged inside the housing (54a), the housing (54a) having at least one hydr...
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WO/2023/114523A1 |
Method and tools for manufacturing core foam sections for a propeller is disclosed. In an embodiment, a method comprises wrapping a first adhesive film around pre-drilled rods; placing the rods into a first mold using placement features;...
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WO/2023/112023A1 |
A boom member for in-flight refueling includes a first boom member portion, a second boom member portion, and a connect/disconnect mechanism. The first boom member portion includes a first boom lumen, a first boom axis, and a fuel receiv...
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WO/2023/111445A1 |
The invention relates to a method for regulating the speed of a propulsion device of a hybrid propulsion unit for an aircraft comprising: the propulsion device and an MGB; the heat engine and at least one electric motor, mounted in paral...
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WO/2023/111476A1 |
A method for managing the torque of an aircraft turbomachine comprising a fan (6) or a propeller of variable pitch connected to a turbine (5) by a shaft (7) and a reduction gear (8), and an electric generator (9) connected to the shaft (...
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WO/2023/113654A1 |
The invention relates to the field of video and audio communication, and more particularly to devices for receive, transmit and display purposes. An arrangement of devices for receiving, processing, storing, transmitting and reproducing ...
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WO/2023/113058A1 |
Disclosed is a drone control method for precise landing. The drone control method according to an embodiment of the present invention may comprise the steps of: when a drone is switched to an arming mode in a drone station, setting curre...
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WO/2023/111517A1 |
An interface node for enabling a robotic arm to be used as a reconfigurable fixture for vehicle manufacture is described. The interface node comprises an attachment element for attaching the interface node to the robotic arm. The interfa...
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WO/2023/115004A1 |
A package coupling apparatus for securing a package to an unmanned aerial vehicle (UAV) is provided. The package coupling apparatus includes a hanger and a strap coupled to the hanger. The hanger includes a base configured, to be positio...
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WO/2023/114373A1 |
Described herein is an aerial material delivery system (100), which includes an unmanned aerial vehicle (UAV) (102) and a material dispensing assembly (114) mounted to the UAV (102). The material dispensing assembly (114) includes a rota...
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WO/2023/113651A1 |
The invention relates to nautical and aeronautical design, and more particularly to flow propellers for use in water or air, and can also be used as a generator for converting water and air flows into electrical energy. A flow propeller ...
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WO/2023/113753A1 |
The present invention comprises a stratospheric unmanned aerial vehicle in which 5 solar panels and internal electric power unit are used as hybrids, and particularly, in order to ensure the security of civilians and military personnel, ...
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WO/2023/112681A1 |
Provided is an information processing device comprising: a status-related information reception unit that, with respect to a flying object that, functions as a stratosphere platform and emits, from a service link (SL) antenna, an SL beam...
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