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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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WO/2023/060679A1 |
Disclosed are an aircraft (1), a wing assembly, and an aerocar. The aircraft (1) comprises a fuselage (10), a wing assembly (20), a tilting connector (30), and a rotor assembly (50). The wing assembly (20) comprises a fixed portion (21) ...
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WO/2023/062691A1 |
This flight vehicle comprises: attachment sections that are disposed at the tips of a pair of fixed wings disposed to the left and the right with a main body therebetween, and that have side surfaces on sides facing away from the main bo...
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WO/2023/062675A1 |
Provided is a drone protection system for protecting a drone 2 from thunderstroke, the drone protection system comprising a Faraday cage 1 which surrounds the drone 2 and a wire 3 which can move on the Faraday cage 1 while an end portion...
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WO/2023/062689A1 |
An aerial vehicle according to the present invention comprises: a structure for flying as an aircraft; a control system for flying as an aircraft; a structure for flying as a multicopter; and a control system for flying as a multicopter;...
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WO/2023/063141A1 |
An EDS (50) includes a motor housing (70) and an inverter housing (90). The inverter housing (90) includes inverter fins (92). The motor housing (70) includes motor fins (72) and motor guide plates (77). The motor fins (72) and the motor...
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WO/2023/062611A1 |
Disclosed is a multicopter foldable between a stowed state and an operational state, the multicopter comprising a hub configured to receive one or more payloads and a battery, two or more flight arms that extend substantially horizontall...
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WO/2023/060678A1 |
An aircraft (1), comprising a fuselage (10), a wing assembly (20), a tilt rotor assembly (50), and a coaxial dual-rotor assembly (60). The wing assembly (20) is connected to the fuselage (10); the tilt rotor assembly (50) is tiltably con...
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WO/2023/062690A1 |
This flight vehicle comprises: a plurality of arms one end of each of which is connected to a body; an attachment part that is provided to the other end of each of the plurality of arms; propellors that are attached to the attachment par...
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WO/2023/063140A1 |
An EDS (50) has a motor housing (70) and an inverter housing (90). The inverter housing (90) has inverter fins (92). The motor housing (70) has forward inclined fins (721) as motor fins (72). The forward inclined fins (721) are provided ...
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WO/2023/062751A1 |
A controller according to one example of the present disclosure is provided with: a body module including an operating machine that outputs an operation signal in response to input of a user's operation for steering a drone equipped with...
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WO/2023/058721A1 |
Provided is a flight device with a simplified mechanism for transmitting motive power. The flight device 10 comprises an airframe 19, a main rotor 14, an engine 30, and a power transmission shaft 25. The main rotor 14 rotates to thereb...
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WO/2023/051013A1 |
The present patent discloses a vertical take-off and landing aircraft based on variable propeller wing technology and a double-propeller wing layout. A main wing surface employs a propeller wing design and may be switched between a rotor...
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WO/2023/055319A1 |
The present invention relates to at least one fuselage (2) located in an air and/or space vehicle; at least one structural part (3) in the fuselage (2), which supports an inner surface of the fuselage (2) in terms of strength; a pluralit...
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WO/2023/053847A1 |
Provided are a sound wave reception device, a sound source bearing standardization device, and a method for standardizing sound source bearings, with which it is possible to suppress the effect of sound wave noise produced by rotating bl...
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WO/2023/056093A1 |
Systems, methods, and apparatuses for an aerial vehicle (AV). The AV can include a frame structure comprising an upper frame, a lower frame, and bridges connecting the upper frame and the lower frame. The upper frame can include a housin...
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WO/2023/051929A1 |
The invention relates to an aircraft, comprising: at least one pair of wings (2, 3) for an aerodynamic flight; a flight propulsion drive (10) acting mainly in the forward direction (u) for the purpose of said aerodynamic flight; and a ho...
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WO/2023/044833A1 |
An unmanned aerial vehicle, a camera mechanism and a cradle head. The unmanned aerial vehicle comprising a fuselage (10) and a power assembly (20). The fuselage (10) comprises a nose (11) and a tail (12) opposite to the nose (11). The po...
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WO/2023/044668A1 |
A plant protection unmanned aerial vehicle (UAV) (100), comprising: a rack (102), which comprises an arm; a first motor (302), which is mounted on the arm; a spraying component (307), which is mechanically coupled to a rotor (3022) of th...
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WO/2023/044821A1 |
A multi-rotor unmanned aerial vehicle (100). The multi-rotor unmanned aerial vehicle (100) comprises a fuselage (10) and arms (30). The roots of the arms (30) are connected to the fuselage (10); a protrusion (31) is provided on the front...
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WO/2023/042561A1 |
Provided is a flight device that comprises a plurality of drive sources and that can use, even when any one of the drive sources stops during the flight, another drive source to continue the flight. This flight device 10 is provided wi...
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WO/2023/044342A1 |
Embodiments of the present disclosure provide systems and methods for a hub. The system provides a hub comprising at least two blades, a motor mechanically connected to the at least two blades to rotate the at least two blades, wherein t...
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WO/2023/043313A1 |
Actuation device for a high-lift device of a rotor blade, comprising a first link, movable in a span- wise direction, outwardly by a centrifugal force, a biasing member, connected with the first link and configured to exert an opposite f...
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WO/2023/039726A1 |
A driving wheel for a vehicle, and the vehicle. The driving wheel comprises a support unit (1), a deformation unit (2), and a wheel face unit (3). The support unit (1) is connected to the wheel face unit (3) by means of the deformation u...
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WO/2023/042601A1 |
In the present invention, an acquisition unit (11) acquires data indicating the results of detecting the shape of a multiple dwelling unit including a target dwelling which is the destination of a drone (10). The acquisition unit (11) al...
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WO/2023/039066A1 |
A system which includes a plurality of cylindrical battery cells that have a uniform orientation, where each of the plurality of cylindrical battery cells has a first planar surface and a second planar surface. There is also a thermal ma...
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