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WO/2023/124124A1 |
A method for controlling a deformable rolling aircraft. The method comprises the following steps: after a control system receives a starting signal, a driving device (5) driving a rotor wing to rotate, and the rotor wing generating a lif...
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WO/2023/126919A1 |
A VTOL-type air vehicle is transitioned from forward speed mode to hover mode via a transient path in transition mode. The air vehicle includes first and second propulsion systems, and high lift, mild stall fixed wings. The first propuls...
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WO/2023/128008A1 |
The present invention relates to an aircraft inspection automation system based on an image and explainable artificial intelligence, and, more particularly, to an inspection automation system using an inspection automation platform for d...
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WO/2023/127501A1 |
Provided are a control device, a control method, and a control program which can transfer, with high accuracy, information through image projection or capturing, even in a situation in which high accuracy projection or capturing is diffi...
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WO/2023/129817A1 |
A system for an automated ML-based design of a wireless network. The system includes a processor of a design server node connected to at least one server node over a network and a memory storing machine-readable instructions that when ex...
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WO/2023/126201A1 |
The invention relates to a propulsion system (100) for a spacecraft. The system comprises an electrical propulsion engine (101) comprising an anode (103) and a cathode (104), a chemical propulsion engine (102), a pressurant gas system co...
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WO/2023/128960A1 |
This invention relates to the apparatus that enables the assembly of the engine that rotates the wings of the unmanned aerial vehicle (drone) to take off, on the chassis, and its feature is; There is at least one motor connection hole (1...
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WO/2023/126041A1 |
In a first aspect of the present invention there is provided a wind turbine comprising a tower, a nacelle mounted on the tower, and a rotor mounted to the nacelle. The rotor comprises a hub and at least three pitchable wind turbine blade...
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WO/2023/126594A1 |
The present document relates to a device (100) for electrically discharging a part of a turbine engine, said device comprising a sleeve (102) capable of receiving said turbine engine part and at least one handling arm (106) mounted on sa...
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WO/2023/126599A1 |
The present invention relates to an electrical propulsion system (20) for an aerial vehicle, including a plurality of electric motors (21), a plurality of power batteries (22) for powering said electric motors with electrical power, and ...
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WO/2023/124125A1 |
A deformable rolling aircraft, comprising: a base body (1), a first wing portion (21) and a second wing portion (22), two rotors arranged in parallel being provided in each of the first wing portion (21) and the second wing portion (22);...
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WO/2023/130126A1 |
Provided is an aircraft hand controls. The aircraft hand controls may comprise a set of left and right brake hand controls and a rudder hand control. The set of left and right brake hand controls may be operatively connected to the rudde...
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WO/2023/121899A2 |
For global navigation satellite system (GNSS)-independent operation of auxiliary PNT systems, one or more ground stations of the auxiliary system have access to a non-GNSS source of precision timing. That source and known locations of th...
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WO/2023/118747A1 |
The present invention relates to an assembly for a tank comprising: an inner wall (1) delimiting a cavity (2) intended to receive a liquid, the inner wall (1) having a first surface (101) facing the cavity (2), and a second surface (102)...
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WO/2023/119930A1 |
A control device (50) is for controlling an electric vertical takeoff and landing aircraft (100), and in the case where the magnitude of a magnetic field detected by a magnetic sensor (70) provided to the electric vertical takeoff and la...
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WO/2023/120773A1 |
An unmanned aerial vehicle and a method for supporting task offloading are disclosed. An unmanned aerial vehicle for supporting task offloading according to an embodiment may comprise: a communication unit that communicates with at least...
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WO/2023/122111A1 |
In accordance with some embodiments, a system for controlling an aircraft is provided. The system can include a computing device, wherein the computing device includes at least one processor configured to control a flight path angle of t...
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WO/2023/118304A1 |
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/2023/122145A1 |
Additive manufactured airframe (10) structure having a plurality of additive manufactured airframe segments (30) operable to be linked together in an assembled direction (40). Each of the plurality of additive manufactured airframe segme...
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WO/2023/118686A1 |
The invention relates to a turbine engine module, comprising: - a fan (3) intended to be rotated by a fan shaft (32) and comprising a plurality of variable-pitch blades (30); and - a pitch change system comprising a control means (52) co...
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WO/2023/121940A1 |
A payload retrieval apparatus is provided including a stand or base, wherein the base or stand has an upper end and a lower end, a first sloped surface positioned over the upper end of the stand or base, a second sloped surface positione...
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WO/2023/122717A1 |
A method of operating an aircraft including takeoff of an aircraft; transitioning the aircraft to a forward flight configuration by increasing an amount of forward propulsive force generated by a propeller assembly from equal to or less ...
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WO/2023/120908A1 |
The present invention provides a system for obtaining positional coordinates of a camera video object by using a drone having an onboard flight control computer, the system comprising: a global positioning system (GPS) configured to use ...
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WO/2023/118873A1 |
A vehicle (1) for capturing a falling object comprises a plurality of air cushion units (100), wherein each of the air cushion units is configured to generate a propulsive force to drive the vehicle and a lift force to elevate the vehicl...
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WO/2023/118876A1 |
A rapidly deployable structure is provided comprising: one or more structural members configurable between a compressed configuration and an expanded configuration; at least one chemical inflator configured to rapidly expand the one or m...
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WO/2023/120803A1 |
The present invention relates to a port air quality and air pollution management system using measurement data collected from an infrastructure built on the basis of IoT technology, and a method for operating same. The port air quality a...
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WO/2023/118830A1 |
A tethered aerostat (101, 201, 203, 205, 401, 601, 708) positioned at an elevated location in the atmosphere, the aerostat (101, 201, 203, 205, 401, 601, 708) having an elongate body (403) having a length extending between an upper end (...
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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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