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WO/2024/093476A1 |
The present invention provides a coaxial dual-rotor unmanned aerial vehicle, comprising a main shaft, an upper rotor assembly, a lower rotor assembly, an upper motor, a lower motor, and a rotor control device. The upper rotor assembly is...
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WO/2024/094352A1 |
Disclosed is an aircraft power system (800) comprising a hydraulic reservoir (801, 803), a bidirectional hydraulic pump (212) for pumping hydraulic fluid to and from the reservoir, and an electric motor (230), wherein the hydraulic pump ...
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WO/2024/093500A1 |
A full-vector survey cluster system and an operation control method therefor. The full-vector survey cluster system (8) comprises a plurality of robots. The plurality of robots comprise a survey robot (200) and at least one cable-bearing...
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WO/2024/094948A1 |
Aeronautical thruster (40) having a longitudinal axis (X) and comprising an upstream rotor row and a downstream stator row (16) having unducted blades (18). Two adjacent blades of the downstream stator row (16) have between them, about t...
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WO/2024/094351A1 |
Disclosed is an aircraft power system 800 comprising a first driveable component 120, 130 of the aircraft, and a mechanical flywheel 250, wherein the mechanical flywheel is connectable to the first driveable component such that the mecha...
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WO/2024/093481A1 |
A variable-rotating-speed rotor blade, a coaxial unmanned helicopter, and a single-rotor unmanned helicopter. The variable-rotating-speed rotor blade comprises: a blade root (10), a blade middle section (20), and a blade tip (30) which a...
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WO/2024/088114A1 |
A power plant with variable thrust direction, the power plant comprising a fan (10), a housing (20) and an adjusting mechanism (30). The housing (20) is internally provided with an air intake duct (23), a first air output duct (21) and a...
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WO/2024/091629A1 |
Embodiments relate to an aircraft control and interface system configured to adaptively control an aircraft according to different flight states by modifying one or more processing control loops. The system receives sensor data from one ...
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WO/2024/092202A1 |
An aircraft includes a first inceptor assembly. The first inceptor assembly has a first base and a first control stick extending away from the first base, the first control stick defining a first longitudinal axis that extends through th...
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WO/2024/091922A1 |
The present disclosure relates to a jetstream power generating system. The system is configured to harness the energy of jetstream forces in farms as power generating infrastructure. The system comprises an airborne element configured to...
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WO/2024/085765A1 |
Disclosed is a system and a method for projecting a solution onto a facade of a structure. The system comprises: a pump for pumping the solution; a tool for projecting the pumped solution onto the facade; a hose for connecting the pump t...
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WO/2024/082833A1 |
A multirotor electric-manned aerial vehicle, comprising: a cabin (1) for carrying people; multiple rotor support arms (2), wherein each rotor support arm has one end fixedly connected to the top of the cabin by means of a central connect...
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WO/2024/084156A1 |
The present disclosure relates to an assembly for an aircraft comprising: a compensator (5) comprising: a chassis (50) intended to be fixedly mounted on a cell of the aircraft; and an actuator (52) movably mounted on the chassis (50); a ...
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WO/2024/086324A1 |
The disclosed embodiments are directed to an eVTOL aircraft comprising a fuselage, wings mounted to the fuselage, where the wings comprise an undercambered lower surface, and an array of ducted fans mounted to the undercambered lower sur...
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WO/2024/080060A1 |
A control device (60) controls flight of an eVTOL comprising: rotating blades (13) which are driven by a drive apparatus (15) and which generate a rotational lifting force; a fixed blade for generating a glide lifting force; and a liftin...
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WO/2024/080181A1 |
Provided is a transmission device for an unmanned aerial vehicle, wherein arms that drive propellers can be positioned so as not to interfere with an air cleaner and a radiator. A transmission device for an unmanned aerial vehicle in w...
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WO/2024/077668A1 |
The present invention relates to the technical field of unmanned aerial vehicles. Disclosed are a variable topdressing device based on a six-rotor multispectral unmanned aerial vehicle and a use method therefor. The device comprises: an ...
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WO/2024/077523A1 |
An unmanned aerial vehicle (100). The unmanned aerial vehicle (100) comprises a vehicle body (10) and vehicle arm assemblies (20), wherein two vehicle arm assemblies (20) are provided, and the two vehicle arm assemblies (20) are symmetri...
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WO/2024/081182A1 |
A fluid flow powered system for generating electrical power including a rotating turbine blade comprising an outer rim, a tension airfoil central hub assembly, tension elements extending between the outer rim and the tension airfoil cent...
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WO/2024/074662A1 |
The invention relates to a method (100) for producing a spar cap for a rotor blade of a wind turbine, said method comprising the steps of: - Providing (110) a plurality of pultruded planks, said pultruded planks being a thermoplastic com...
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WO/2024/066918A1 |
A fixed-wing aircraft having vertical take-off and landing electric rotors and driven by a fuel power to fly forwards, comprising vertical take-off and landing electric rotor mechanisms (6) embedded in a fixed wing (2) or/and in an empen...
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WO/2024/067896A1 |
The invention relates to an aircraft, comprising a body, at least four arms and/or supporting surfaces arranged on the body at a respective one end and extending away from the body with a respective free end, vertical and/or lateral rudd...
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WO/2024/065917A1 |
A reconfigurable blended wing vertical take-off and landing aircraft, comprising a fuselage, wings, canards, and a cabin door. The wings are respectively arranged on the two sides of the fuselage, two rotor wing modules are respectively ...
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WO/2024/072350A1 |
A hybrid air vehicle comprising a body (2); at least one motor (3) which provides required power for flight; at least one rotor (4) extending outward from the body (2) connected to the motor (3); a plurality of blades (5) located on the ...
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WO/2024/069080A1 |
The invention relates to a system for transmitting commands to N hydraulic servo-actuators, N being an integer greater than or equal to 2, the system comprising: N mechanical systems, each mechanical system comprising: - a rotary electri...
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WO/2024/064626A1 |
The present invention provides methods and systems for remote operation of a vehicle with the capability to deal with communications jitter and intermittency. In particular, the methods and systems herein may safely predict a remote oper...
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WO/2024/062928A1 |
The present technology relates to an unmanned aircraft and a propeller in which it is possible to improve stability in a state in which a foldable unmanned aircraft propeller is opened. This unmanned aircraft comprises a propeller and a ...
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WO/2024/061016A1 |
Disclosed in the present invention are a single-encoder actuator for an aircraft and a power-on self-test method therefor. By means of a vector control algorithm, a controller controls a servo motor to rotate, and by means of a harmonic ...
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WO/2024/059189A1 |
Systems and methods relate to a vertical takeoff and landing (VTOL) platform that can include a stator and a rotor magnetically levitated by the stator. The rotor and stator can be annular, such that the rotor rotates about a rotational ...
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WO/2024/057746A1 |
An operation control unit 11 controls a flight drive mechanism 1009 so as to perform an operation by which detection values of respective sensors included in a sensor group 1007 provided to a drone 10 match target values. A detection uni...
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WO/2024/057825A1 |
[Problem] To provide a drone device for coating and a coating method capable of performing maintenance coating safely and inexpensively. [Solution] The drone body part 10 has an IMU 15 that acquires the tilt angle of a drone device 1, a ...
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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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