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WO/2024/059181A1 |
Systems and methods relate to a vehicle, such as a vertical takeoff and landing (VTOL) platform, which can include a stator and a rotor magnetically levitated by the stator. The rotor and stator can be annular, such that the rotor rotate...
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WO/2024/055899A1 |
A connector and method for connecting a motor and an arm of a multi-rotor aircraft. The connector comprises a base (1), a locking disk component (2), and a guided positioning component (3), wherein one side of the base (1) is connected t...
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WO/2024/057935A1 |
Provided is a rotary wing that is unlikely to be deformed by fluid. A rotary wing 1 comprises: a hub 10; a first blade 20, a second blade 30, and a third blade 40, being a plurality of blades which each have one end connected to the hub ...
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WO/2024/055381A1 |
A perching robot and a perching method of the perching robot. The perching robot relates to the technical field of robots, and comprises: a body (101), a control unit, a perching module (102) and a data acquisition unit (103); the contro...
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WO/2024/052616A1 |
The invention relates to an actuator (20) designed to be connected to a mechanical flight control chain (13) of a vehicle, comprising a motor (22), a first output shaft (23) driven in rotation by the motor (22) about an axis of rotation ...
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WO/2024/053375A1 |
Provided are a flight device and a method for controlling the same, by which it is possible to accurately measure the power remaining in a battery with a simple configuration. A flight device 10 is provided with a rotor 11, a motor 12,...
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WO/2024/054195A1 |
A closed-wing vertical take-off and landing aircraft comprising: a fuselage (1); a tail unit comprising two angularly inclined stabilizers (12); and a closed wing, comprising a front wing formed by two planes (2) mounted to the fuselage ...
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WO/2024/045724A1 |
An anti-crash rotor wing guide rail device for a tandem dual-rotor wing unmanned aerial vehicle, comprising a main beam (1), a rotor wing structure, a rotor wing guide rail device, a self-locking device (2), and a sensing device. The rot...
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WO/2024/049387A1 |
The present invention relates to a body (2); at least one engine (3) on the body (2), which generates the necessary force for the flight of the air vehicle (1); at least one rotor (4) capable of rotating around itself, connected with the...
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WO/2024/049386A1 |
The present invention relates to a body (2); at least one wing (3) located on the body (2); at least one icebreaker (4) on the wing (3), which enables the ice formed on the wing (3) surface to be removed from the wing (3) surface; an act...
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WO/2024/042894A1 |
Provided is a flying mobile body 1 that comprises a body 3 and a plurality of rotor blade units 2 mounted to the body 3. The rotor blade units 2 each have rotor blades 20 and a cylindrical body 10 that covers the rotor blades 20. During ...
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WO/2024/040407A1 |
A ducted aircraft (100) and a duct (10) thereof. The ducted aircraft (100) comprises a duct (10), a fuselage (20), and power assemblies (30). The duct (10) comprises at least two duct units (11). The duct units (11) are each provided wit...
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WO/2024/040466A1 |
A flight control method, an apparatus, an unmanned aerial vehicle, and a storage medium. The method comprises: in a flight state, determining whether a collision of an unmanned aerial vehicle occurs (31); and, when it is determined that ...
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WO/2024/038634A1 |
Provided is a flight method that makes it possible to prevent a collision of a drone and entanglement of a power supply cable. This flight control system relating to flight control of an electrically driven drone 3 that is connected to a...
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WO/2024/033594A1 |
The invention relates to a method for assisting with propulsion by detecting a failure of a turboshaft engine of an aircraft operating in a nominal mode, the aircraft comprising a deactivated assistance motor, which method comprises a st...
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WO/2024/034498A1 |
Provided is a robot arm in which a first sensor detects the posture of a flying robot. The robot arm has a control unit that controls a second drive module, on the basis of a detection signal from the first sensor, and that thereby cause...
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WO/2024/028671A1 |
Aircraft (1) capable of hovering comprising a fuselage (2), at least one rotor (3a, 3b, 4) that is rotatable with respect to the fuselage (2), electrical drive means adapted to rotate the rotor (3a, 3b, 4) and electrically powered by a b...
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WO/2024/025491A1 |
The invention relates to motor groups consisting of electric motors for use in electric aircraft and the propulsion system that drives and manages them. Every electric motor has a propeller on the outside, while the rotor and stator inte...
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WO/2024/021640A1 |
A control method and apparatus, an aircraft, a mobile platform, and a storage medium. The control method comprises: controlling a driving assembly of the aircraft to drive a wing assembly of the aircraft to move relative to a central bod...
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WO/2024/021186A1 |
Disclosed in the present utility model is an electric flying lifebuoy, comprising a housing, flight assemblies, a flight control assembly and a power module, wherein the housing is a lifebuoy with an air storage inner cavity; the flight ...
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WO/2024/018392A1 |
A rotorcraft type UAV drone comprises a main body (1) which supports at least one rotor (2, 4) with blades (6) and at least one compressor (18, 20), integrated with each other and operated by the same driving force (10, 12), to generate ...
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WO/2024/018459A1 |
The present disclosure provides a thrusting assembly for mounting on an aerial platform and configured for generating thrusting power to allow a controllable accelerated air mass flow in and out the thrusting assembly. The thrusting asse...
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WO/2024/020362A1 |
In one embodiment described herein is a mast moment sensor system for a rotorcraft comprising a rotor shaft bearing strain sensor. In some embodiments the mast moment sensor system is configured to compute a rotor mast moment using the r...
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WO/2024/018137A1 |
The invention relates to a hybrid propulsion system (2) comprising: a turbine engine (3) comprising a high-pressure spool (4) and a low-pressure spool (5), the low-pressure spool (5) comprising reduction gear (11), the reduction gear (11...
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WO/2024/017420A1 |
The invention discloses an oval folding fixed wing household small manned aircraft, which comprises an oval folded fixed wing flight system, a cabin, a chassis, etc. The oval folded fixed wing system comprises an oval fixed wing lower ed...
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WO/2024/014086A1 |
The present invention provides a payload management apparatus that calculates a weight that can safely be loaded on an aircraft of the rotary wing type, suppresses a decrease in transport efficiency, and increases flight safety of the ai...
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WO/2024/012000A1 |
A linear multi-rotor plant protection unmanned aerial vehicle structure based on tilt rotors and a control method therefor. The structure comprises main lifting power structures, tilt power structures and a main rack structure, wherein t...
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WO/2024/013392A1 |
The invention relates to a vertical take-off aircraft (1) which is designed as a tail-sitter and, after the take-off, transitions in full from the substantially vertical hover attitude into the horizontal attitude, comprising: an aircraf...
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WO/2024/007061A1 |
The inventions will find application in aviation, particularly for passenger and cargo transport, in emergency medical care, etc. The aircraft comprises a frame 2 with casing 3 and at least one engine 4 mounted to the frame 2, and at lea...
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WO/2024/004158A1 |
Provided is an unmanned aircraft that has horizontal wings and that is compact overall. An unmanned aircraft 100 comprises: an unmanned aircraft body 101; a plurality of rotors 104A, 104B and 104C which each have a rotary shaft extendi...
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WO/2024/004443A1 |
A locking device (100) can transition between a locked state and an unlocked state. The locking device (100) comprises a lock pin (101), a solenoid (110), and a pressing unit (120). The lock pin (101) can be moved between a locked positi...
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WO/2024/000855A1 |
A gyroscope assembly, a turbine blade, an impeller, and a wind power generator set. The turbine blade comprises a blade body (10), a web (11), and a gyroscope assembly. The blade body (10) has an inner cavity; the web (11) is fixedly dis...
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WO/2024/001143A1 |
A ducted fan (2), an aircraft and an attitude control method and system therefor, and a related apparatus. The ducted fan (2) comprises: a first ducted fan unit (201) comprising a first fan assembly (21) and a first duct (22), which is a...
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WO/2024/006164A1 |
An aircraft has a boom, a propulsion assembly coupled to a first end of the boom, and a first wing coupled to a second end of the boom. The first wing can be coupled to the boom by a (first) articulated joint. The propulsion assembly can...
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WO/2024/006078A1 |
Systems and methods for protecting an aerodynamic structure, e.g., a wind turbine blade, rotor blade, aerodynamic aerostructure, etc., are provided. Long fiber reinforced composites having a helicoidal architecture with material aligned ...
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WO/2023/246948A1 |
A new foldable convenient manned aircraft comprises a fuselage, four arms arranged on the fuselage, a rotor motor, a rotor and an anti-collision radar which are symmetrically arranged on the outer end of each arm, four anti-collision air...
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WO/2023/249652A1 |
A peripheral propulsion system having a propulsion unit (3), an upper section (36), and a lower section (37). The propulsion unit (3) has a motor (31), a motor engagement section (34), an extension (32) coupled to the motor engagement se...
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WO/2023/246424A1 |
An electrically controlled variable pitch propeller, and a multirotor and a control method therefor. The electrically controlled variable pitch propeller comprises a main shaft (10), a variable pitch blade (20) and a brake module (30), w...
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WO/2023/248746A1 |
This compound helicopter comprises a fuselage, a pair of main wing parts, a main rotor, a first side propeller, and a second side propeller. The main wing parts are provided so as to extend in the left-right direction of the fuselage. Th...
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WO/2023/242448A1 |
A lift module capable of achieving vertical flight in fixed-wing aircraft and generating low aerodynamic drag during horizontal flight, comprising essentially: a structural compartment (40); and two lids (41A) and (41B) hinged by means o...
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WO/2023/243299A1 |
The present invention provides a flying device capable of effectively cooling an engine during flight. A flying device10 according to the present invention comprises an airframe 19, a rotor 14, an engine 30, and a cooling unit 11 for c...
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WO/2023/238631A1 |
A control method according to the present technology controls the pitch angle of a gimbal, which is provided to a flying body and capable of rotating a camera in the pitch direction and the roll direction, in a manner which is independen...
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WO/2023/239886A1 |
Systems and methods for a hub system are disclosed. The hub system includes: a motor (102) operably coupled to a first correlated magnet (204), wherein the first correlated magnet (204) defines a first attachment surface having one or mo...
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WO/2023/238194A1 |
This drone with a Faraday cage comprises: a conductor 30 which is in a grid form, exposes propellers 11 to the outside, and surrounds a drone body 10 (control unit); a lightning rod 31 which is arranged on the conductor 30 and is used to...
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WO/2023/238834A1 |
This fall trajectory control system (1) comprises: a drone (2) provided with an imaging unit that captures images at least vertically downward, and a drop object holding part capable of holding a drop object (6) and releasing the state o...
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WO/2023/238289A1 |
[Problem] To provide a VTOL aircraft capable of improved flight efficiency and preventing a reduction in takeoff and landing performance. [Solution] A VTOL aircraft 100 comprising a main wing 21, a first rotary wing part 11, and a second...
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WO/2023/234226A1 |
A mobile object 1 according to the present disclosure is provided with a body unit 10 which is formed as a first polyhedron, and a rotary blade module 20 which is positioned at each vertex of the first polyhedron and is mounted to the bo...
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WO/2023/233717A1 |
An unmanned rotorcraft 1 comprises a non-moving landing leg 60 that is fixed to a vehicle body 50. The landing leg 60 includes a ground-contact part 61 that is for making contact with the ground and a frame part 63 that connects the grou...
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WO/2023/233870A1 |
An estimation unit (12) estimates whether a person is present inside a door on the basis of sound data acquired by an acquisition unit (11). The wording "inside a door" refers to a place where a user takes off his or her shoes in an entr...
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WO/2023/234043A1 |
This flight control device performs a flight control process for causing eVTOL to fly. The flight control device determines whether to maintain eVTOL in a stable orientation in steps (S104-S106) of the flight control process. In a step (...
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