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WO/2023/182127A1 |
Provided is a flying apparatus in which inner ends of arms can be rigidly connected to an airframe. A flying apparatus 10 comprises an airframe 11, arms 12, and rotors 13. The arms 12 each have a first arm part 121 and a second arm par...
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WO/2023/178687A1 |
An unmanned aerial vehicle (100). The unmanned aerial vehicle (100) comprises a main body (10), first rotation portions (20), and first arms (30). The first arms (30) can rotate around the first rotation portions (20) relative to the mai...
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WO/2023/178688A1 |
An unmanned aerial vehicle (100). The unmanned aerial vehicle (100) comprises a housing (10), a heating component (20), a heat sink (30) and an arm assembly (40). The housing (10) is provided with an air inlet (11) and an air outlet (12)...
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WO/2023/182089A1 |
The purpose of the present invention is to improve the accuracy of three-dimensional surveying if sloping ground is included in the target region for surveying. A control device according to the present technology comprises: a point cl...
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WO/2023/176782A1 |
Provided is a flying apparatus in which the engine can be effectively cooled during flight. The flying apparatus 10 is provided with an airframe 19, a rotor 14, an engine 30, and a cooling unit 11 for cooling the engine 30. The cooling...
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WO/2023/173307A1 |
Provided in the present application are a movable platform and a control method therefor, an information prompting method and apparatus, and a movable platform, an electronic device and a computer-readable storage medium. Each of a plura...
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WO/2023/173374A1 |
An unmanned aerial vehicle and an arm assembly. The unmanned aerial vehicle comprises a fuselage (10); at least one arm assembly (20), which comprises an arm (21) and a fuselage connection part (22) for being connected to the fuselage (1...
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WO/2023/171872A1 |
A cyclic swing rotor assembly comprises: a first shaft; a blade rotating along with the first shaft; a hinge apparatus connecting the blade and the first shaft; a second shaft rotating independently from the first shaft; a swing hub rota...
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WO/2023/167131A1 |
[Problem] To achieve high safety performance and extend cruising time in an aircraft. [Solution] An aircraft according to the present invention can be boarded by a passenger and moves while floating above the ground. A method for control...
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WO/2023/167130A1 |
[Problem] To improve the flight performance of an aircraft. [Solution] This aircraft on which a passenger can ride, and which moves by floating from the ground, is characterized by comprising: a fuselage on which the passenger rides; lif...
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WO/2023/164862A1 |
A dual-propeller universal transmission device, used for dual-propeller transmission of an aircraft or aerial vehicle, consisting of an input sleeve shaft, input double bevel gears, a revolving sleeve shaft, revolving double bevel gears,...
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WO/2023/164739A1 |
A tank assembly for a helicopter is disclosed herein. The helicopter has a fuselage with at least two spaced-apart longitudinal floor beams and at least one lateral floor member extending therebetween. The tank assembly comprises a retra...
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WO/2023/167624A1 |
The present invention relates to an unmanned aerial tree harvesting system (1) comprising a remotely and/or autonomously controlled UAV (100), an autonomously and/or remotely controlled tree harvesting tool (117) configured for holding a...
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WO/2023/162953A1 |
Provided is a control system for a flying vehicle, the control system including: a speed sensor that detects the flight speed of the flying vehicle; a distance sensor that obtains a first distance, which is the distance between the flyin...
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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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