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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/2024/094351A1 |
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/2024/087990A1 |
An aircraft and a control surface hinge structure thereof. The hinge structure comprises a stabilizer hinge (1) and a movable-surface hinge (2), which are arranged opposite each other, wherein the stabilizer hinge (1) comprises a stabili...
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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/2024/084953A1 |
The present disclosure relates to an information processing device, an information processing method, and a program with which improved sound collection can be achieved. An information acquisition unit acquires information necessary for ...
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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/2024/080060A1 |
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/2024/069103A1 |
The invention relates to a control device including a mechanical seal (24) which guides the rotation of a control lever (22) relative to a frame (20) about two pivot connections of orthogonal axes. The mechanical seal (24) comprises, for...
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WO/2024/069788A1 |
[Problem] To ensure safety during aerial photography. [Solution] A mobile body system 1 comprising a mobile body 100 that flies in a subject area F and a flight mode switching unit 330 for switching flight modes M102 and M105 in which fl...
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WO/2024/073373A1 |
Rudder pedal input control devices (100, 200, 300, 400A, 400B, 500, 600) are described that utilize a straight-line mechanism and rotary joints to achieve straight line motion in a compact volume. The devices include bar linkages (106, 1...
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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/2024/062249A1 |
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/2024/060987A1 |
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/2024/060971A1 |
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/2024/060123A1 |
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/2024/061016A1 |
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/2024/057746A1 |
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/2024/052616A1 |
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/2024/048101A1 |
An aircraft automatic control system according to an embodiment of the present invention comprises: a measuring unit which measures, as forecast information, a difference between a wind speed actually being experienced by the aircraft, a...
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WO/2024/044289A1 |
Controlling navigation of an autonomous unmanned aerial vehicle (UAV), commonly known as a drone, involves mathematical modeling and the resulting estimations. The autonomous UAV has one or more rotors, a wind sensor, and a controller fo...
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WO/2024/039824A1 |
Systems and methods for flight control on an electric aircraft. The system includes a propulsor configured to generate lift to propel an electric aircraft, a pilot input mechanically coupled to the electric aircraft, a sensor communicati...
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WO/2024/039423A1 |
A linear actuation system includes a pin pivotably coupled to an output rod of a linear motion actuator and a rotatable output shaft that includes a bushing therein. The pin can be configured to slide in and out of the bushing in respons...
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WO/2024/038811A1 |
A conveyance control method according to one aspect of the present disclosure is a method for lifting and conveying cargo via a plurality of flexible cables by using a plurality of unmanned aerial vehicles, each of which is capable of ge...
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WO/2024/032907A1 |
An electric vertical take-off and landing aircraft comprises a fuselage (1) and a tilt wing (7). The tilt wing (7) is tiltable relative to the fuselage (1) in a range of tilt wing angles. Control surfaces (13) are arranged at the tilt wi...
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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/2024/013482A1 |
The present invention relates to an Electronic Unit (1), EU, for a tactile cueing apparatus for a vehicle. The tactile cueing apparatus augments feel for an operator of the vehicle. The EU comprises a first channel (307A, 407A). The firs...
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WO/2023/248591A1 |
This flight management system comprises: a management device including a processing circuit configured to manage operational authority of a plurality of aircraft; and an operating terminal including an operation interface operated by an ...
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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/2023/238350A1 |
The present invention efficiently acquires local wind conditions to safely operate an unmanned aircraft. This operation assistance system for unmanned aircraft is configured using an optical analysis unit, an information processing devic...
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WO/2023/238208A1 |
[Problem] To provide an aerial photography system, an aerial photography method, and an aerial mobile body management device that can facilitate the smooth running of a contest, an event, or other activities. [Solution] An alarm control ...
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WO/2023/233857A1 |
A control device according to an embodiment of the present invention controls a user-wearable flight device and comprises a processing unit that acquires state data related to the state of the flight device and manipulation data related ...
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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/2023/229702A1 |
A drive mechanism for actuating a control surface of a vehicle that moves through a fluid medium. The mechanism directly translates the rotational motion provided by an input drive to a control surface that is used to direct the vehicle....
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WO/2023/218674A1 |
This flying body comprises: a communication device; a receiver that acquires a current position; a flight controller that controls flight and is able to transmit current position information by using the communication device; a plurality...
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WO/2023/209335A1 |
According to an aspect of the present invention, there is provided a control unit in an active inceptor configurable to generate force feedback in a linked active inceptor system, comprising: a first connection configured when an operati...
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WO/2023/203673A1 |
A flying object control system (A) that causes a plurality of flying objects (B) to fly as a group comprises a flight command generation unit that generates flight commands for causing the plurality of flying objects (B) to fly as a grou...
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WO/2023/204390A1 |
The present invention transmits signals from two signal sources to form a planar surface and a curved surface, and guides an aircraft using a curve generated by intersection of the two surfaces as a take-off and landing path of a vertipo...
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WO/2023/203668A1 |
[Problem] To provide an aerial vehicle capable of appropriately performing work when the aerial vehicle is to be utilized in various work. [Solution] Provided are an aerial vehicle 2, a work device 3 capable of carrying out designated wo...
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WO/2023/198507A1 |
The invention relates to a system (9) for controlling actuators in an aircraft, the system comprising at least a first actuator (2-a) and a second actuator (2-b) each comprising: - a movement member (3-a, 3-b); - at least one measurement...
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WO/2023/200852A1 |
Principles described herein allow for wings to be optimized for aerodynamic and structural efficiency while reducing planform compromises required to address wing tip stall problems. All-moving outboard wings allow the outboard wing loca...
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WO/2023/189534A1 |
[Problem] To provide an unmanned mobile object that makes it possible to detect another mobile object with high reliability. [Solution] A drone 10, which is an unmanned mobile object according to an embodiment of the present invention, i...
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WO/2023/188271A1 |
This aircraft comprises a communication unit for connecting to the internet, and a control unit that controls the communication unit such that data is transmitted to a monitoring device through the internet. The communication unit, when ...
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WO/2023/190847A1 |
This aircraft comprises: a first communication unit that performs first wireless communication; a second communication unit that performs second wireless communication different than the first wireless communication; and a control unit t...
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WO/2023/188270A1 |
This aircraft comprises a first communication unit that performs first wireless communication, a second communication unit that performs second wireless communication different from the first wireless communication, and a control unit th...
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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/2023/165951A1 |
The invention relates to a movement transmission device (10) for a mechanism for actuating and/or opening and/or closing and/or locking and/or unlocking a door or a flap of a mechanical movement control device of an aircraft, the device ...
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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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