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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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WO/2023/156161A1 |
The invention relates to an electronic checklist system for an airplane, having a storage unit, a selection unit, an operating and display unit, and an interface unit. The storage unit is designed to store and, upon demand, provide at le...
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WO/2023/153120A1 |
Provided is an information processing device comprising: a prediction result acquisition unit that acquires a prediction result regarding the weather in the stratosphere; and a flight path determination unit that determines, on the basis...
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WO/2023/138227A1 |
A rudder pedal assembly used for controlling a flight vehicle, and the flight vehicle. The rudder pedal assembly comprises a first rudder pedal unit (11), a second rudder pedal unit (13), and a trimming return drive and damping module (1...
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WO/2023/135037A1 |
The invention relates to a movable leading-edge flap (16) comprising an aerodynamic part (19) and at least one drive and guide rail system (42), which system includes two rails (44) each extending over the entire length of the rail syste...
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WO/2023/127289A1 |
This automatic takeoff/landing system for a vertical takeoff/landing aircraft comprises: a relative wind information acquisition unit that acquires the direction of relative wind at a moving object; and a control unit that executes takeo...
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WO/2023/126919A1 |
A VTOL-type air vehicle is transitioned from forward speed mode to hover mode via a transient path in transition mode. The air vehicle includes first and second propulsion systems, and high lift, mild stall fixed wings. The first propuls...
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WO/2023/130126A1 |
Provided is an aircraft hand controls. The aircraft hand controls may comprise a set of left and right brake hand controls and a rudder hand control. The set of left and right brake hand controls may be operatively connected to the rudde...
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WO/2023/122111A1 |
In accordance with some embodiments, a system for controlling an aircraft is provided. The system can include a computing device, wherein the computing device includes at least one processor configured to control a flight path angle of t...
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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/2023/099866A1 |
A strain wave-type gearbox comprises: a flex spline component; an outer circular spline component; and a wave generator component, wherein the wave generator component is configured for adjustment of at least one dimension of the wave ge...
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WO/2023/099865A1 |
A drive arrangement for manipulating a vehicle control surface, comprises: a first drive; a second drive; an output member for connecting to the vehicle control surface; first engaging means for selectively engaging and disengaging the f...
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WO/2023/099867A1 |
A drive arrangement for manipulating a vehicle control surface, comprises: a first drive; a second drive; an output member for connecting to the vehicle control surface; first engaging means for selectively engaging and disengaging the f...
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WO/2023/099868A1 |
A drive arrangement for manipulating a vehicle control surface, comprises: a first drive; a second drive; an output member for connecting to the vehicle control surface; first engaging means for selectively engaging and disengaging the f...
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WO/2023/091114A1 |
The present invention relates to a body (2) located at an air vehicle; at least one control stick (3) extending outward from the body (2) and enabling the pilot to control tasks such as position and speed of the air vehicle; at least one...
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WO/2023/085027A1 |
This device (300) is installed in a moving object (100) and is purposed for controlling the moving object (100). The device (300) is provided with a holding part (310) and a control unit (302). The holding part (310) holds an information...
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WO/2023/086556A1 |
The subject matter of this specification can be embodied in, among other things, a method that includes controlling, by a first fluid valve, a first fluid flow to a first fluid actuator, actuating, by the first fluid actuator, an output,...
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WO/2023/079247A1 |
The invention relates to a force application device for an aircraft control stick, in which the computer is configured: a) for an angle (ANG1) smaller than or equal to a prescribed virtual stop threshold (S1, S2), to control the motor so...
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WO/2023/079965A1 |
Provided is a flight control device that performs a flight control process for flying an aircraft. If a collision between the aircraft and another craft is predicted, this flight control device performs a discovery and avoidance process ...
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WO/2023/081387A1 |
A rotary wing vehicle has a vehicle body. A gimbal assembly mounted to or within the body. A propeller assembly is mounted to the gimbal. The propeller assembly has first and second fixed pitch propellers. The gimbal assembly has a first...
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WO/2023/073629A1 |
Electromechanical drive system (1) to control a transmission shaft (2) connected to the mechanical operating systems of an aircraft, comprising an electric machine (3), a two-way transmission rotation (8) and a clutch assembly (9) wherei...
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WO/2023/075964A1 |
Systems and methods to control gain of an electric aircraft are provided in this disclosure. The system may include gain scheduling to provide stability of the electric aircraft at various dynamic states of operation. The system may incl...
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WO/2023/076060A1 |
A cable-linked brake pedal (106) assembly (100) for an airplane. The assembly (100) includes a first cable assembly (200) with a first end attached to a pilot-side brake pedal (106) and a second end attached to a first bell crank assembl...
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WO/2023/075639A1 |
An aircraft sidestick is a device that can be used for controlling different types of manned and unmanned equipment, including aerial, terrestrial and underwater equipment, as well as for controlling spacecraft in outer space and for exe...
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WO/2023/067339A1 |
A VTOL aerial vehicle (10) is disclosed, comprising: an airframe (12); one or more arms (202) coupled to the airframe (12) at a pivot (206); and three or more propulsion units, each mounted on a gimbal (16) having a gimbal axis, and each...
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WO/2023/062751A1 |
A controller according to one example of the present disclosure is provided with: a body module including an operating machine that outputs an operation signal in response to input of a user's operation for steering a drone equipped with...
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WO/2023/059178A1 |
Embodiments relate to methods, systems, and devices for performing an inspection on a telecommunication structure and/or one or more objects that are attached on the telecommunication structure. The system includes an unmanned aerial veh...
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WO/2023/055320A1 |
The present invention relates to a sensor unit (2) located on an air vehicle, which enables the measurement of air speed, engine torque and lateral acceleration of the air vehicle; a flight control computer (3) which enables a first adju...
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WO/2023/044535A1 |
An emergency interface system for an autopilot system has an actuator mechanically interfacing an actuator switch, the actuator throwing the actuator switch when operated. The actuator switch has an actuator output connected to an input ...
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WO/2023/042551A1 |
On the basis of illuminance acquired by an acquisition unit (11), a prediction unit (14) predicts an illuminance limit time (LT) at which the illuminance in an area where a drone (10) flies will be less than a threshold value, and predic...
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WO/2023/042601A1 |
In the present invention, an acquisition unit (11) acquires data indicating the results of detecting the shape of a multiple dwelling unit including a target dwelling which is the destination of a drone (10). The acquisition unit (11) al...
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WO/2023/037071A1 |
A control column (2) for a vehicle comprising a control lever (3) connected to a mechanical chain, a cup (4) and a locking device (1), the control lever (3) being oriented relative to a pivot point (6) of the control column (2), the lock...
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WO/2023/034909A1 |
A control surface restraining system for variably preventing movement of a control surface imparted by a control actuation shaft of a control actuation section of a tactical flight vehicle includes a power take-off shaft operably connect...
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WO/2023/031921A1 |
A line of sight (LOS) delivery system. The system includes a carrier device having a first collimated light source for targeting an object, a distance meter; and a second collimated light source for outputting a beam substantially parall...
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WO/2023/023697A1 |
Provided is a sensor magazine arrangement (10) for a drone (8), the arrangement (10) comprising a chassis (14) configured to receive at least a portion of a drone (8) to position a load point (26) of such drone (8) relative to the chassi...
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WO/2023/026797A1 |
Provided is an engine-carrying flight device capable of stably hovering. An engine-carrying flight device 10 can fly in a hovering state, in which altitude is maintained, and in an ascending/descending state, in which altitude is chang...
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WO/2023/027736A1 |
A torque limiter includes a housing; an input shaft which is rotatably supported in the housing; an output shaft which is rotatably supported in the housing coaxially with the input shaft; and a ball detent mechanism which is connected b...
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WO/2023/021948A1 |
In the present invention, after a drone 10 reaches the sky above a building designated as a destination of the drone 10, an inspection unit 12 inspects candidate landing positions at the destination on the basis of an image of the entire...
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WO/2023/003681A2 |
A system for flight control of an electric vertical takeoff and landing (eVTOL) aircraft. The system generally includes a pilot control, a pusher component, a lift component and a flight controller. The pilot control is mechanically coup...
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WO/2023/286186A1 |
In order to deal with suspicious aircraft, which are unmanned aircraft that are not authorized to fly in a surveillance airspace, while preventing adverse effects on authorized aircraft, which are unmanned aircraft that are authorized to...
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WO/2023/282124A1 |
A drone 10 comprises: a detection unit 12 that, after a flying vehicle is located over a structure specified as a destination, detects, on the basis of an image of a site including the structure captured by the flying vehicle, the struct...
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WO/2023/277847A1 |
The present invention relates to a console (C) provided in air vehicles; at least one control stick (2) located on the console (C), providing mission input to the air vehicle by the user; at least one bracket (3) allowing the control sti...
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WO/2023/274914A1 |
In order to reduce maintenance work and to improve long-time reliability, the invention provides a health monitoring method for checking a functionality of a flight control surface driving apparatus (104) using at least one load sensor (...
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WO/2023/277723A1 |
The claimed invention relates to aviation and concerns command posts for manually controlling an aircraft, in particular a single-rotor helicopter. In one of the possible design embodiments, the invention is envisaged as follows. A yoke ...
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WO/2023/274913A1 |
In order to reduce maintenance work and to improve long-time reliability, the invention provides a health monitoring method for checking a functionality of a flight control surface driving apparatus (104) using at least one load sensor (...
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WO/2023/276640A1 |
Provided is a flying object control system comprising an area-forming part that forms a prescribed area relative to a grip, a detection unit that detects a displacement of the prescribed area formed by the area-forming part, and a contro...
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WO/2023/276454A1 |
The control device according to the present invention comprises a processor and a memory that is connected to or built into the processor. The processor carries out, when the processor causes a rotary drive device on which a distance mea...
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WO/2022/263777A1 |
The invention relates to an aircraft flight compensator comprising a friction module (8) that has variable friction and is coupled on one side to a drive shaft (11) and on the other side to an output shaft (13) via a kinematic chain (12)...
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