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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/2023/128962A1 |
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/2023/129444A1 |
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/2023/127501A1 |
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/2023/128960A1 |
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/2023/124125A1 |
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/2023/119930A1 |
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/2023/119518A1 |
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/2023/122109A1 |
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/2023/113652A1 |
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/2023/112343A1 |
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/2023/111445A1 |
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/2023/109114A1 |
Disclosed in the present invention is a reconstructable flying car. A car body main body is detachably connected to a wing assembly, a propulsion assembly, an empennage assembly, and multi-axis rotor assemblies by means of a connecting m...
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WO/2023/111484A1 |
One aspect of the invention relates to a system (20) for transmitting commands to at least one hydraulic servo actuator (30), comprising: - a mechanical system (21) including: o a rotary electrical actuator (211) comprising a first and a...
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WO/2023/106538A1 |
The present invention relates to a drone having a movable propeller shaft, the drone comprising: a drone body having an opening; a plurality of propeller shafts arranged radially on the drone body, each propeller shaft having one side po...
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WO/2023/107037A1 |
The present invention relates to at least one main housing (2) which is located on the helicopter between the engine and the rotor and contains the elements for transmitting power from the engine to the rotor; a main shaft (A) that provi...
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WO/2023/104382A1 |
A method for activating at least one rotor (5) of an aerial vehicle (1), wherein the rotor (5) is designed to compensate for, or at least reduce, a torque acting on the aerial vehicle (1), the rotor (5) is provided with a casing (15), an...
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WO/2023/100597A1 |
This flight control device carries out a flight-control process for causing an eVTOL to fly. The flight control device determines, in step S101 of the flight control process, whether the eVTOL is in the midst of landing. If the eVTOL is ...
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WO/2023/101757A1 |
A multicopter rotor fault diagnosis system includes a multicopter, a plurality of local sensors, and a controller. The multicopter includes a body, a plurality of booms secured to the body, and a plurality of rotors. Each boom has a prox...
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WO/2023/101540A1 |
The present invention provides an aerial vehicle having a plurality of individually tiltable unit rotors and capable of vertical takeoff and landing. The aerial vehicle comprises: a fuselage; and a plurality of rotor groups connected to ...
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WO/2023/099117A1 |
The invention relates to a device comprising an asymmetrical wing profile (2) and an adjusting device (15), which asymmetrical wing profile (2) has a profile thickness (q) and a profile chord (p) extending between a wing leading edge (n)...
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WO/2023/100133A1 |
A control unit (46, 46') for an aircraft (1, 1') capable of hovering or for a flight simulation system of the aircraft (1, 1') is described, the control unit (46, 46') is programmed to receive at input at least a first signal associated ...
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WO/2023/100150A1 |
A control unit (46, 46') for an aircraft (1, 1') capable of hovering or for a flight simulation system of the aircraft (1, 1') is described; the control unit (46, 46') is programmed to: - receive in input a plurality of data associated w...
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WO/2023/099749A1 |
In a first aspect, a surveillance system for an offshore infrastructure is provided. The surveillance system comprises an unmanned surface vessel (USV), an unmanned vehicle for inspecting the offshore infrastructure and a controller. The...
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WO/2023/093996A1 |
The invention relates to a boom assembly and a corresponding lifting assembly for helicopters (1), and a corresponding mounting method. The boom assembly is provided with: a base unit (8) having a first upper side and a first underside, ...
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WO/2023/095630A1 |
This flight vehicle comprises a rotor shaft projecting upward from a body, a rotor head connected to the rotor shaft above the body, and a pair of plate units that are disposed above the body and extend in the longitudinal direction on t...
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WO/2023/087602A1 |
A detachable fixed-wing unmanned aerial vehicle (UAV), the UAV comprising: a body, an end plate (20), a first wing (31) and a second wing (32), wherein: one side of the body is connected to the first wing (31), the other side of the body...
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WO/2023/091389A1 |
Various implementations include a rotor control device including a shaft extending along a rotational axis, a hub, first and second pitch control components, and a swashplate. The hub has a hub axis and is hingedly coupled to the shaft s...
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WO/2023/089735A1 |
[Problem] The present invention provides a flying object with which any decrease in flight efficiency while the flying object is cruising can be minimized while safety is improved. [Solution] This flying object is provided with a safety ...
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WO/2023/082292A1 |
A multi-rotor unmanned aerial vehicle (UAV), comprising: a center body (10); a landing frame (11), which is located below the center body (10); two pairs of arms (12), which are rotatably connected to the center body (10), so as to achie...
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WO/2023/085198A1 |
The present invention provides a blade in which the specific rigidity of a flap part is further increased. This blade has a thick body part and a thin flap part integrally formed in the rear end of the body part. The flap part has a skin...
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WO/2023/085338A1 |
Provided are a mechanism and device that can increase the degree of freedom of the placement of the center of rotation of a rotating body relative to a rotation reference. Also provided is a system using the same that suppresses changes ...
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WO/2023/082294A1 |
A coaxial two-propeller unmanned aerial vehicle, comprising a body (10), an arm (20), and a power mechanism (30). The arm (20) is mechanically coupled to the body (10); the power mechanism (30) is mounted on the arm (20); the power mecha...
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WO/2023/080172A1 |
[Problem] The present invention pertains to a system that is capable of remotely managing and remotely controlling a flying object from outside. [Solution] A manned flying object control system according to the present technology compris...
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WO/2023/079965A1 |
Provided is a flight control device that performs a flight control process for flying an aircraft. If a collision between the aircraft and another craft is predicted, this flight control device performs a discovery and avoidance process ...
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WO/2023/081025A1 |
An aircraft uses trajectory-based control algorithms for blade pitch (or twist). This approach greatly enhances the ability of the actuator to accurately achieve the desired blade pitch and to track the commanded pitch position. An actua...
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WO/2023/079900A1 |
Provided is a flight device capable of accurate attitude control with sub-rotors.　The flight device 10 comprises an airframe 19, an engine 30, a motor 21, main rotors 14, and sub-rotors 15. The engine 30 rotates the main rotors 14. The...
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WO/2023/079433A1 |
The present invention relates to a vertical take-off and landing module (200) for a fixed-wing aircraft (110), which includes at least one vertically-acting propulsion unit (240), actuator means (245) and support means (230), so as to be...
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WO/2023/079523A1 |
An unmanned aerial vehicle ("UAV") (1) for non-destructive testing ("NDT") comprises: an outer protective cage (2), a propulsion system (3) mounted inside the outer protective cage (2) and fixed thereto, an arm (4) comprising a first end...
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WO/2023/059209A9 |
The method of obtaining both, lifting force and thrust, required for horizontal flight of the vertical take-off and landing flying machine while maintaining horizontal flight stability of the machine which is realized due to suction atmo...
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WO/2023/081387A1 |
A rotary wing vehicle has a vehicle body. A gimbal assembly mounted to or within the body. A propeller assembly is mounted to the gimbal. The propeller assembly has first and second fixed pitch propellers. The gimbal assembly has a first...
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WO/2023/074357A1 |
This power supply device is for an unmanned mobile body. The power supply device has a drive mechanism and control unit. The drive mechanism moves on water. The control unit controls the drive mechanism so that a positional relationship ...
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WO/2023/074883A1 |
This conveyance system (1) comprises: a plurality of first movable bodies (10) capable of autonomous movement; and a second movable body (20) which conveys the plurality of first movable bodies (10) as a first collective body (60) in whi...
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WO/2023/074095A1 |
Provided are a threat-countering system and a threat-countering method for efficiently countering incoming threats by using laser irradiation. The threat-countering system comprises a countering device, a deterrent device, and a decision...
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WO/2023/073440A1 |
A control device (50) for controlling the variation of the angle of attack of the blades (8) of the anti-torque rotor (4) for an aircraft (1) capable of hovering is described, comprising a control element (16) sliding along a first axis ...
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WO/2023/067432A1 |
Systems and methods for an aircraft comprising: wings in tandem configuration wherein each wing having one tilting motor; an additional tilting motor located at the rear part of said aircraft; wherein all said tilting motors can tilt in ...
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WO/2023/069537A1 |
The present invention provides a system for remote vehicle operation by human pilot and artificial intelligence systems. The system comprises: a vehicle capable of movement, a human operator and control station situated outside of the ve...
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WO/2023/067286A1 |
The invention relates to a method for manufacturing a part made of composite material, the method comprising: - three-dimensional weaving (S10) of a structure (20) having a longitudinal axis (A); and - braiding (S40) of at least one laye...
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WO/2023/067653A1 |
An aerial vehicle control device (1) for controlling an aerial vehicle that flies over water, said device comprising: a crash detection unit (31) for detecting that the aerial vehicle has crashed into the water; and an acoustic wave outp...
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