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WO/2023/157189A1 |
This aircraft performs vertical takeoff and landing. The aircraft is provided with: at least a pair of fixed blades 20-j; a rotor blade 402-1 that is rotary driven to generate a propulsion force for propelling the aircraft vertically upw...
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WO/2023/153879A1 |
This disclosure relates to various multi-rotor aircrafts including at least one passively tiltable rotor group which may be tilted, typically in a direction of their movement. More importantly, the passively tiltable rotor group can tilt...
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WO/2023/152746A1 |
An aircraft, comprising: a fuselage; two wings mounted to the sides of the fuselage, extending laterally; a pusher propeller, statically mounted to the fuselage, wherein a rotational axis of the pusher propeller is parallel to a longitud...
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WO/2023/148595A1 |
The invention relates to a device (1) for propelling, by means of counterrotating coaxial propellers, a rotary wing aerodyne with vertical take-off and landing. This device comprises a hollow chassis (5) and two propellers each having a ...
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WO/2023/149106A1 |
The purpose of the present invention is to provide an operation management system capable of safely and space-efficiently optimizing an operation path in accordance with various events that occur during an operation. An operation managem...
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WO/2023/145762A1 |
A drone (10) determines whether landing is possible at a destination. When the landing is possible, the drone lands and performs an operation for releasing cargo. When the landing is not possible, the drone performs an operation for deli...
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WO/2023/146965A1 |
Embodiments provide a VTOL aircraft including a plurality of tilting propeller assemblies each coupled to a support structure and configured to transition between a vertical flight and a forward flight position. Each tilting propeller as...
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WO/2023/139969A1 |
The eVTOL according to this invention comprises an EPU and a blower fan. The blower fan cools the EPU by blowing cooling wind to the EPU. The flight control device according to this invention carries out abnormality diagnosis control for...
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WO/2023/140032A1 |
Provided is a control device (110) comprising a control unit (112) that controls an EPU (10) which supplies drive power to a rotor blade (30) of an electric aircraft (20), wherein the EPU has: a motor (11); an inverter (121); a control c...
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WO/2023/136014A1 |
This flight control device carries out a flight control process for causing an eVTOL to fly. When an EPU abnormality occurs during vertical takeoff, a flight control device (40) performs a during-takeoff process in a flight control proce...
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WO/2023/135275A1 |
Rotary-wing aircraft, comprising: - a drive motor (12) with a motor output shaft (12-3), - a transfer gearbox (14) having the motor output shaft (12-3) as an input and having a first output (14-1) and a second output (14-2), - a cockpit ...
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WO/2023/130313A1 |
An unmanned aerial vehicle circulating storage device (10) and a corresponding circulating storage system (100). The unmanned aerial vehicle circulating storage device (10) comprises: multiple storage units (12) capable of circularly mov...
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WO/2023/129011A1 |
The present invention relates to a body (2); a cut out (3) located on the body (2); a sensor (4) located in the cut out (3) so as to move outwards from the body (2), and enabling the data requested by the user to be obtained; at least on...
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WO/2023/128955A1 |
This invention relates to the Coaxial Aluminum Sigma Drone Chassis, which can be used in drones capable of carrying people or cargo, and its feature is; The sigma profile (1), which is the basic part that forms the chassis, the hidden co...
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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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