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WO/2023/126933A1 |
An explosive bolt system includes an explosive bolt and an initiator device. The explosive bolt includes a shank having a first longitudinal end, an opposed second longitudinal end, and a longitudinal axis. The explosive bolt is configur...
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WO/2023/127289A1 |
This automatic takeoff/landing system for a vertical takeoff/landing aircraft comprises: a relative wind information acquisition unit that acquires the direction of relative wind at a moving object; and a control unit that executes takeo...
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WO/2023/129406A1 |
A method and apparatus for aiding a police officer in writing a report by creating a depiction of an incident scene is provided herein. During operation a drone will photograph an incident scene from above. Relevant objects will be ident...
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WO/2023/124378A1 |
A propeller and an aircraft. The propeller comprises a propeller blade (1) and a spoiler portion (2). At least part of the spoiler portion (2) protrudes out of a suction surface of the propeller blade (1), and the spoiler portion (2) ext...
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WO/2023/126936A1 |
The present subject matter provides a combination system for manipulating an electrical potential of a plurality of plants and manipulating an electrical charge of particles that interact with at least one plant of which electrical poten...
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WO/2023/127953A1 |
There is provided a technique for implementing instantly responsive communication flexibly by setting communication occasions in an on-demand manner that are not included in a communication plan scheduled in advance for inter-satellite o...
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WO/2023/125554A1 |
A vehicle, which has a vehicle door (110) system, the vehicle door (110) system comprising a vehicle door (110), an actuating mechanism (120), and a controller (150). The vehicle door (110) is mechanically coupled and connected to a vehi...
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WO/2023/126930A1 |
A method is provided for operating a parachute-payload system with respect to a predetermined target zone location. The method includes: providing the parachute-payload system; constructing a predicted descent trajectory for the parachut...
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WO/2023/129006A1 |
The present invention relates to a body (2) provided on an air vehicle; at least a first mount (3) which is located on the body (2) so as to move on the body (2) in a direction it lies, and which carries the air vehicle by contacting the...
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WO/2023/126701A1 |
A method for estimating rotor torques (TQmast1, TQmast2,…,TQmastN) of an aircraft (1; 1'; 1'') capable of hovering and comprising a plurality of rotors (31, 32; 33', 34'), which are rotatable under the action of respective rotor torque...
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WO/2023/128715A1 |
The present invention relates to an electric motor, and more specifically to a turbine-blade type electric motor having an expandable structure that allows for easy increase in output as necessary, and a stackable module capable of produ...
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WO/2023/125883A1 |
Embodiments of the present invention relate to the technical field of unmanned aerial vehicles, and particularly disclose a camera module and an unmanned aerial vehicle; the camera module comprises: a mounting frame; a lens assembly mova...
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WO/2023/128962A1 |
The present invention relates to an aircraft capable of vertical landing-takeoff, which has arms with folding mechanisms and safety systems that minimize the risks that may occur during an accident, and its feature. The vehicle chassis (...
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WO/2023/127028A1 |
This propulsion device comprises a first conducting wire and a second conducting wire that are spaced apart and fixed, and a power source that outputs alternating current. The propulsion device is configured such that the alternating cur...
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WO/2023/128795A1 |
The group of inventions relates to an unmanned aerial vehicle (UAV) for diagnosing, maintaining and repairing a high-voltage overhead power line and to a method for equalizing potentials during landing on a conductor or earth wire of a l...
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WO/2023/129014A1 |
The present invention relates to an air vehicle (V); a plurality of wheels (2) located on the air vehicle (V) and enabling movement of the air vehicle (V) on the ground (Z); at least one rotating structure (3) located on the air vehicle ...
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WO/2023/124434A1 |
A multi-rotor dronebox, comprising an external box frame (100), wherein a receiving port (110) is formed on an upper side of the external box frame (100); a receiving platform (200) is arranged on an inner side of the external box frame ...
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WO/2023/124099A1 |
A dual-duct hybrid power device, a flying vehicle, and a control method. The device comprises an outer duct, an inner duct, and a compression propulsion system which uses compressed air as a working medium, wherein the inner duct is arra...
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WO/2023/129013A2 |
The present invention relates to a body (2) located on an air vehicle; at least one weapon (W) located on the body (2) to attack a target; a carrier (3) that allows the weapon (W) on the body (2) to be moved and carried as desired by the...
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WO/2023/129439A2 |
An exemplary charger for an electric aircraft with failure monitoring includes a charging circuit, the charging circuit including: a connector configured to mate with an electric aircraft port of an electric aircraft; at least a current ...
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WO/2023/129021A1 |
This invention is an invention that can be used for autonomous battery replacement of unmanned aerial vehicles and its feature is; It does not cause data loss by enabling the replacement of multiple batteries of the UAV, which lands in t...
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WO/2023/129007A1 |
The present invention relates to a body (2) located in air vehicles; at least one gas discharge element (E) on the body (2), which enables the discharge of hot waste gases; at least one cartridge (F) launched from the body (2) against th...
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WO/2023/129444A1 |
Aspects relate to a system for flight plan generation of an electric vertical takeoff and landing (eVTOL) aircraft. An exemplary system for flight plan generation includes a flight controller mounted on an eVTOL aircraft. The flight cont...
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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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