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WO/2022/113087A1 |
Rotorcraft including a fuselage and at least three rotor system arms each having a rotor system. Each rotor system includes a mast having at least two rotor blades and an electric rotor motor. At least one rotor system arm includes a sup...
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WO/2022/101891A1 |
This fuel calculation device comprises: a remaining fuel amount calculation unit that periodically calculates and stores an approximate value of the remaining fuel amount on the basis of the measurement value of the remaining fuel amount...
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WO/2022/101894A1 |
An aircraft position control system that maintains an aircraft at target coordinates in the air with respect to a swaying target landing point, said system comprising: an acceleration correction processing unit that, on the basis of the ...
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WO/2022/100891A1 |
The invention relates to an aircraft comprising a display screen (7) and at least one turbomachine (2), each turbomachine (2) comprising a motor (10), the aircraft (1) comprising the following elements associated with each turbomachine (...
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WO/2022/101892A1 |
This automatic landing system for a vertical take-off and landing aircraft comprises: a camera mounted on a vertical take-off and landing aircraft; a relative positioning acquisition unit that performs image processing on an image obtain...
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WO/2022/101895A1 |
An aircraft position control system that causes the position of an aircraft to adapt to the movement of a target landing point caused by swaying, said system comprising: a sway amount estimation processing unit that estimates the amount ...
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WO/2022/102091A1 |
This anti-lightning strike structure for a flying vehicle comprises: a lattice-shaped conductor 11 that surrounds a flying vehicle 100 so as to be spaced apart therefrom in order to not interfere with flight; an attachment part 12 that i...
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WO/2022/094137A1 |
An apparatus and method for detecting a collision of an aerial vehicle and recovery from the collision is disclosed. An apparatus for use in an aerial vehicle includes an arm, a flexible member and a sensing system. A processor is config...
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WO/2022/085259A1 |
A terminal control device 300 of a client 30 of an image provision system 1: stores location information of construction stakes 41-45; when an operator selects construction stake 42 among the construction stakes 41-45, transmits a flight...
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WO/2022/080512A1 |
The present application relates to a control stick for a military aircraft, a system for managing health information regarding a pilot, a military aircraft, and a simulator for a military aircraft. According to the control stick for a mi...
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WO/2022/076288A1 |
The present disclosure provides compositions, articles thereof, and methods of forming compositions. In at least one aspect, a composition includes (1) an epoxy, (2) an amino or amido hardener, (3) a polyaniline, (4) a dopant selected fr...
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WO/2022/074470A1 |
A simplex Flight Control Computer (FCC) to be used in a flight control system comprising the simplex Flight Control Computer and at least one neighboring flight control computer is disclosed. The simplex flight control computer comprises...
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WO/2022/071891A1 |
The present invention relates to a system for detecting a foreign object on a runway. The system includes a thermal camera having a first field of view and adapted to capture a thermal image of an area of interest on the runway, a visibl...
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WO/2022/071104A1 |
A motor-driven movable body (510) comprises an output shaft (531) and a plurality of motors (571, 572) for driving the output shaft. This motor-driven movable body executes multiple drive control for assigning at least two of the plurali...
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WO/2022/067545A1 |
An unmanned aerial vehicle (1000), the unmanned aerial vehicle (1000) comprising a fuselage (900), an obstacle avoidance sensor (800), and a bracket (100). The bracket (100) is capable of moving relative to the fuselage (900) such that t...
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WO/2022/071894A1 |
A system for detecting a foreign object on a runway, the system including a thermal camera comprising a first field of view and adapted to capture a thermal image of a first view of an area of interest on the runway from one side of the ...
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WO/2022/071103A1 |
A plurality of motors (71, 72, 73, 74) that drive output shafts (31, 32) and a plurality of batteries (21, 22) are connected so that power is supplied from the batteries to motor sets constituted of motors that respectively drive separat...
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WO/2022/058687A1 |
Disclosed is an aeronautical conveying and release device, actuated by a cartridge, comprising a housing provided in a body 60 comprising a recess having an open end and a bottom, a cartridge adapter 62 capable of closing the recess and ...
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WO/2022/059846A1 |
The present invention relates to a system and a method for controlling leader-following flight in an aerial vehicle swarm flight. The system for controlling leader-following flight in an aerial vehicle swarm flight according to the first...
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WO/2022/053527A1 |
The invention relates to an aircraft radome (1) comprising a composite structure (10) comprising, or according to the circumstances configured to define, at least one housing (20) extending along the radome from a base (2) of said radome...
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WO/2022/040904A1 |
An unmanned aerial vehicle cruise device for port safety monitoring, relating to the technical field of port safety. The unmanned aerial vehicle cruise device comprises an unmanned aerial vehicle body (1) and a camera (2); the top end of...
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WO/2022/045539A1 |
The present invention relates to an aircraft wing. The aircraft wing comprises: a lightning protection apparatus which is installed on the surface of the aircraft wing to transmit the electrical energy of lightning to the surroundings wh...
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WO/2022/038385A1 |
Disclosed is a ground movement system for a helicopter having a fuselage and rotor blades fixed to the top of the fuselage, the ground movement system comprising at least three wheels secured below the fuselage of the helicopter, the whe...
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WO/2022/038383A1 |
Disclosed is a pilot aircraft system control input arrangement for a light aircraft having primary flight controls, the pilot aircraft system control input arrangement integrated into an armrest for a pilot's seat, the armrest providing ...
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WO/2022/038227A1 |
In order to control a flow of persons and to implement distancing rules in a cabin (1) for an aircraft, a cabin (1) having a first monitored region (11) and a second monitored region (14) is provided. The cabin (1) has a monitoring assem...
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WO/2022/034001A1 |
The invention relates to a method for operating an aircraft (1) which takes off and lands vertically. The mass (m) of the aircraft (1) is determined by a controller (2). For this purpose, a vertical shear force (F_v) of a drive (5) of th...
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WO/2022/034681A1 |
The object of the present invention is to provide an unmanned aircraft that is capable of takeoff and landing on water while suppressing height in the vertical direction. An unmanned aircraft 1 flies with thrust produced by the rotation ...
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WO/2022/034966A1 |
The present invention relates to an unmanned aerial vehicle for water surface observation. In an embodiment, provided is an unmanned aerial vehicle for water surface observation, the unmanned aerial vehicle comprising: a location measure...
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WO/2022/023574A1 |
A wake produced by a leader aircraft and experienced by a follower aircraft is sensed by repetitively carrying out the following two operations in an iterative manner. Measurements carried out by the follower aircraft are estimated (311)...
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WO/2022/018065A1 |
The invention relates to a device and a method for assisting aircraft guidance. The aircraft guidance assistance method is operated by an aircraft computing platform and comprises the steps: - acquiring state variables characterising an ...
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WO/2022/016908A1 |
A helicopter air separation type emergency flight data recording system, comprising: an emergency state analysis system, an ejection system and a cushioning/floating system, wherein the emergency state analysis system is used for determi...
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WO/2022/019432A1 |
A UAM-dedicated navigation system and an UAM-dedicated navigation system operation method are disclosed. A UAM-dedicated navigation system according to one embodiment of the present invention may comprise a UAM navigation device for tran...
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WO/2022/014597A1 |
A monitoring system according to one embodiment of the present disclosure comprises: a sensor that measures a physical quantity at one or a plurality of measurement points of a structure body; a calculation device that acquires the measu...
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WO/2022/014815A1 |
The present invention relates to a drone having a sub rotor. The present invention comprises: a drone body; a plurality of main rotors for generating flight driving force so that the drone body flies; one or more sub rotors for generatin...
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WO/2022/006905A1 |
A separable aircraft protection device, method and system. The separable aircraft protection device comprises: a protection device (11), and an unmanned aerial vehicle flight module (12), a fixing module (13), and a control module (14) s...
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WO/2022/009400A1 |
A wind detection device (14) configured so as to be equipped with: a speed vector calculation unit (21) for obtaining a received signal of electromagnetic waves reflected by the atmosphere inside a monitoring region which includes the fl...
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WO/2022/000198A1 |
An unmanned aerial vehicle and a protective device suitable for the unmanned aerial vehicle. The protective device comprises a plurality of first protective assemblies (10) adapted to be connected to rotor assemblies (91) of the unmanned...
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WO/2022/005420A1 |
The present invention relates to at least one screen (2) which is provided in air and/or space vehicles and displays graphic and/or video images created with flight data of the air and/or space vehicles; at least one data source (3) cont...
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WO/2022/003792A1 |
A control device (900) is provided with an acquisition unit (910) that acquires information representing the weather related to a port, which is the location where a flight vehicle is scheduled to land, and a control unit (930) that caus...
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WO/2021/260497A1 |
The present invention relates to a protective foldable cage (100) adapted to flying drones. It comprises several ribs linked at their extremities by a ring and comprising on their length several connexion points allowing strings to join ...
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WO/2021/260355A1 |
A method (100) of forming a graphene-infused carbon fibre composite, the method comprising providing (102) graphene particles having a mean particle diameter less than 10 microns; providing (104) the graphene particles in a solvent to fo...
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WO/2021/250746A1 |
[Problem] To provide a flying object with which the falling body can be adjusted to a predetermined orientation and a parachute can be deployed more normally. [Solution] The present disclosure relates to a rotorcraft. The rotorcraft acco...
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WO/2021/250793A1 |
Provided are: a flight vehicle that is capable of coping with foreign objects inside a motor or in the vicinity thereof; a flight vehicle system; a flight vehicle control method; and a manipulator. A motor control unit (200) of this flig...
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WO/2021/244544A1 |
An unmanned aerial vehicle (10) fault detection method, an unmanned aerial vehicle (10), and an unmanned aerial vehicle system (100). The unmanned aerial vehicle (10) fault detection method comprises: obtaining flight state information o...
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WO/2021/234023A1 |
The invention relates to a passenger service unit (3) that is intended to be implanted into a transport vehicle so as to be associated with at least one passenger, the service unit comprising at least one sub-assembly (13) having at leas...
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WO/2021/233949A1 |
Disclosed is landing gear (100) of an aircraft (1000) comprising a pair of wheels (5) between which an electric actuator (10) at least partially covered with a lightning arrester cowl (20, 40) is placed, the lightning protection cowl (20...
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WO/2021/228923A1 |
Disclosed is a method for guiding the pilot of an aircraft for the alignment manoeuvre, comprising: determining, at a first instant, an occurrence close to the alignment manoeuvre and triggering the display of a first symbol (30) on the ...
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WO/2021/218168A1 |
A rotor wing protection mechanism (100) and an aircraft (200), the rotor wing protection mechanism (100) comprising a cover body outer frame (10), a fixed base (20) and a plurality of connecting bones (30), wherein the cover body outer f...
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WO/2021/222183A1 |
An aircraft comprising a first power supply such as a battery, avionics including a plurality of sensors that provide aircraft parameter information, a transceiver and a gateway. The gateway includes a processing system and is coupled to...
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WO/2021/217459A1 |
A movable platform control method, a movable platform, a control terminal and a system. The movable platform comprises a battery. The method comprises: obtaining a corresponding relationship of a battery state of power (SOP) value and a ...
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