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WO/2024/060105A1 |
The present application provides a gimbal control method. A gimbal comprises a shaft arm assembly, the shaft arm assembly is used for carrying a load device, and the shaft arm assembly comprises at least one shaft arm and a motor for con...
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WO/2024/061691A1 |
A system for cleaning a waste tank (4) in an aircraft is proposed, comprising a service device, at least one spray nozzle, and a first adaptor (12) for each of the at least one spray nozzle, wherein the service device comprises a descali...
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WO/2024/062301A1 |
Provided is a vehicle comprising a fuselage provided with at least one storage module configured each to accommodate therein unmanned aerial systems and at least one docking module configured each to detachably interact with at least one...
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WO/2024/062249A1 |
A linear actuator (100) comprising a stroke axis (102), an actuator rod (104)extending along the stroke axis. The actuator rod comprises: an actuator rod outer surface (110), and a first screw thread (108) on a portion of the actuator ro...
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WO/2024/062181A1 |
One aspect of the invention relates to a method (100) for selecting an activation logic of an inerting system (3122) of at least one fuel tank of an aircraft (31) for at least one mission of the aircraft (31), the method (100) comprising...
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WO/2024/064128A1 |
Systems, methods, and device include a vehicle for providing horizontal directional control in a first transportation mode and a second transportation mode. The vehicle is an unmanned aerial vehicle with the duct defining a ducted air pa...
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WO/2024/060987A1 |
The present invention discloses a rotary actuator integrated with a gear nonius encoder and a control method, which relates to the field of aircraft devices. The rotary actuator comprises a permanent magnet synchronous motor, a gear noni...
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WO/2024/061514A1 |
The invention relates to a system for detecting a psychological state (10) of a passenger, comprising: - at least one detection sensor (11) capable of detecting at least one physiological parameter of the passenger, in particular a physi...
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WO/2024/060971A1 |
A linear actuator integrated with a gear nonius encoder and a control method therefor. The linear actuator comprises a motor (9), a control circuit module, a gear nonius encoder, and a ball screw pair for pushing a push rod (15) to perfo...
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WO/2024/061096A1 |
Provided are an automatic cargo loading and unloading system, and a hangar comprising the automatic cargo loading and unloading system. The automatic cargo loading and unloading system comprises a cargo box (10), a first cargo conveying ...
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WO/2024/062185A1 |
The invention relates to a spacecraft stack comprising: a stack of spacecraft (1) made up of a plurality of stages which are placed one on top of the other and each comprise a number of vehicles greater than or equal to N; a lower adapte...
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WO/2024/064434A1 |
A mechanism for attachment and detachment of a fixed or controllable airfoil to an airframe includes a base adapted for attachment to a root of the airfoil and a slot beam adapted for attachment along the airframe (e.g., parallel to the ...
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WO/2024/060567A1 |
An integrated electric propulsion system for electric aircrafts. A distributed electric propulsion system and a fly-by-wire flight control actuation system which are integrated on aircraft wings can be unified, thereby providing for the ...
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WO/2024/063723A1 |
This invention relates to a triple integrated camera system for the development of an autonomous vehicle that can avoid obstacles that allows successful autonomous flight by detecting both the width and height of the surrounding objects ...
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WO/2024/060633A1 |
An aircraft wing (10) having an integrated distributed ducted fan, the aircraft wing (10) being attached to a fuselage (20) and being provided with a ducted fan power set (30), wherein the ducted fan power set (30) is provided on an inbo...
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WO/2024/062370A2 |
A system for reconfiguring (1) the layout of a boat (100) is described, comprising a first fixed component (2) of coupling and a second movable component (3) of coupling; the first component (2) is configured to be attached to a fixed el...
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WO/2024/061089A1 |
An aircraft towing apparatus, comprising a frame body (10), a driving mechanism and a connecting mechanism. The driving mechanism comprises first driving wheels (20) and second driving wheels (30) respectively rotatably connected to two ...
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WO/2024/060123A1 |
A gimbal and an unmanned aerial vehicle. The gimbal specifically comprises: a support (10), which is used for carrying a camera device (20); an electric motor (11), which is used for driving the support (10) to rotate, and comprises a st...
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WO/2024/064122A1 |
Embodiments provide a flight supervision platform including a server computer and an animated graphical user interface for simultaneously monitoring multiple autonomous aircraft. More specifically, techniques disclosed herein provide a f...
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WO/2024/064270A1 |
An aircraft propulsion system includes a core engine that includes a core flow path where a core airflow is compressed in a compressor section, communicated to a combustor section, mixed with fuel and ignited to generate a gas flow that ...
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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/2024/061148A1 |
A test frame for the strength of wings under static loads, comprising: a test frame body (100); a plurality of fixed-pulley blocks (200), the fixed-pulley blocks (200) being spaced apart on the test frame body (100); a plurality of weigh...
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WO/2024/061147A1 |
A cargo hold applied to an unmanned aerial vehicle, the cargo hold comprising a cargo hold door (700), and the cargo hold door being connected to the cargo hold of the unmanned aerial vehicle. The cargo hold also comprises a cable releas...
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WO/2024/056866A1 |
The present invention concerns a device for a multicopter that allows the multicopter to move without tipping over. This device generates propulsion according to the x- and/or Y-axis using the air displacement of the drive propellers and...
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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/2024/058566A1 |
The present invention relates to a way to prevent the deterioration of batteries in drones, and in particular, provides a power distribution circuit for preventing the deterioration of a battery due to an instantaneous high output power ...
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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/2024/058872A1 |
A waterproof UAV that records camera footage while traveling through air and while submerged in water. The UAV alters speed and direction of propellers dependent on the medium that the UAV is traveling through to provide control of the U...
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WO/2024/056878A1 |
The invention relates to a glazed system (100, 200, 300) comprising a glass panel (110) comprising structural plies (111, 112), the glass panel being clamped in place by a structure. Said glazed system further comprises: - at least one b...
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WO/2024/056971A1 |
The present application relates to a method for calibrating a model for estimating a torque supplied by an electric machine (10), which comprises the following steps: (E1) measuring an electric current in the electric machine (10) for an...
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WO/2024/055499A1 |
An anti-false-touch safety switch (7), a locking mechanism (100), and a locking system, relating to the technical field of aviation machinery. The anti-false-touch safety switch (7) comprises: a rotary locking member (71), used to be in ...
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WO/2024/058619A1 |
The present invention relates to an airship capable of easily switching directions, the airship comprising an aerial vehicle (mother ship) formed in a disc or polygonal shape provided with a jet engine, a rotating body having a jet engin...
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WO/2024/056879A1 |
The invention relates to a glazed system (100, 200, 300) comprising a glazing (110), for example a laminated glazing, comprising structural folds (111, 112), the glazing being clamped in place by a structure. Said glazed system further c...
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WO/2024/056836A1 |
The present disclosure relates to vertical takeoff and landing aerial vehicles configured to transport a payload. The vehicle comprises a main lifting body and a propulsion assembly coupled to the main lifting body. The main lifting body...
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WO/2024/059347A1 |
A system having components coupled to an aircraft that measure the navigational state and state uncertainty of an aircraft. To do so, the aircraft captures an image of its surrounding environment including an object of interest and appli...
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WO/2024/058620A1 |
The disclosure relates to a 5G or 6G communication system for supporting a higher data transmission rate. A UE in a 5G or 6G communication system for supporting a higher data transmission rate that may efficiently report a flight path of...
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WO/2024/057287A1 |
A deployable boom mechanism, such as for a spacecraft, has a boom and a boom drum. The boom can be wound onto the boom drum. The boom drum is rotatable in a deployment direction to deploy the boom by unwinding it from the boom drum. A dr...
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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/2024/057034A1 |
The present disclosure comprises a portable support (1) positionable on a seat (5). The support (1) comprises a frame (2) and a flexible material (3) extending across the frame (2). The frame (2) is configured to support the flexible mat...
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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/2024/058565A1 |
The present invention relates to a method for preventing drone battery degradation, and in particular, provides: an apparatus for preventing battery degradation caused by a momentary high output exceeding the rating of the battery, where...
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WO/2024/059215A1 |
A method includes receiving configuration data for an unmanned aerial vehicle (UAV) simulation system, the configuration data indicating at least one base location specification, at least one aircraft specification, and at least one virt...
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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/2024/058887A1 |
The present invention is directed to systems and methods for aerially detecting and identifying explosives on the ground, and more specifically systems and methods for detecting and identifying landmines and unexploded ordnance (UXO) on ...
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WO/2024/056959A1 |
The invention relates to a propeller blade or vane (10) for a turboprop engine, made from composite material and comprising a matrix-densified fibrous reinforcement, the propeller blade or vane comprising, in the direction of its span (D...
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WO/2024/055069A1 |
Provided is a hybrid aerial hydro drone (10) comprising a body (12) with a plurality of hydraulic thrusters (14) supported on an outer surface of the body (12) and configured to propel said body (12) in a marine environment. Drone (10) a...
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WO/2024/059230A1 |
An aircraft boarding vehicle to transport passengers between airport gate area and to a front door or a rear door of an airplane positioned on a tarmac of an airport without impeding ground transportation and plane traffic having a passe...
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WO/2024/055506A1 |
The present invention relates to the field of aviation machinery. Provided is a locking mechanism used for a helicopter tail cabin door. The locking mechanism comprises: two lock box assemblies, respectively installed on two sides of a t...
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WO/2024/056195A1 |
The present invention concerns a device for a multicopter that allows the multicopter to move without tipping over. This device generates propulsion according to the x- and/or Y-axis using the air displacement of the drive propellers and...
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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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