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WO/2020/223722A1 |
Methods, devices, and systems for ground traffic aircraft management are described herein. One device includes a user interface, a memory, and a processor configured to execute executable instructions stored in the memory to receive airp...
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WO/2020/220190A1 |
Disclosed are an unmanned aerial vehicle control method and a related device. The method comprises: performing a flight lock operation on an unmanned aerial vehicle; acquiring an image of a user photographed by a photographing apparatus ...
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WO/2020/217004A1 |
A system for monitoring an aircraft engine, comprising: an acquisition module (3) for acquiring current measurements of physical size, referred to as input (ME) and output (MS) physical sizes, relative to the aircraft engine (15), a modu...
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WO/2020/211812A1 |
An aircraft landing method and apparatus, a storage medium and a computer device for implementing the method, and an aircraft. The method comprises: obtaining the current image of a preset take-off/landing site acquired by an aircraft in...
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WO/2020/211919A1 |
This alerting system (10) for a light aircraft includes a reception unit (12) for receiving a piece of information to be released, a release unit (40) able to generate an alert for addressing a piece of information received by the recept...
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WO/2020/201652A1 |
The invention concerns a method for monitoring at least one aircraft engine, said method comprising an acquisition (100) depending on first and second sets of measurements of respectively endogenous and exogenous variables. The method al...
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WO/2020/204273A1 |
The present invention relates to a drone device for drone sports. A drone device for drone sports according to one embodiment of the present invention comprises: a driving unit including one or more propellers to enable the drone device ...
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WO/2020/205833A1 |
A landing strobe is provided that comprises a vane extending from the landing strobe, and an actuator coupled to the vane. The actuator can be configured to move the vane from a first position to a second position upon impact of the land...
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WO/2020/195651A1 |
[Problem] To enable a flying vehicle to fly without touching a structure. [Solution] A flying vehicle of the present invention relates to a flying vehicle for capturing images of the inner wall of a substantially tubular structure, and t...
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WO/2020/198524A1 |
A system having components coupled to an aircraft in operation processes sensor- derived data, performs a localization cross-checking procedure, and dynamically generates updated analyses of the position and orientation of the aircraft. ...
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WO/2020/197416A1 |
System are described for cargo transportation comprising a container adapted for the storage of cargo and adapted for transportation by UAV. The container has features of a shell defining and interior space adapted for the containment of...
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WO/2020/190382A1 |
In an embodiment, one or more computer-readable storage medium comprising a plurality of instructions to cause an apparatus, in response to execution by one or more processors of the apparatus, to receive sounds emanating from one or mor...
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WO/2020/189493A1 |
A wind information storage unit 101 acquires and stores wind information indicating the wind speed and wind direction of wind blowing at a plurality of locations near a facility being inspected. A wind prediction unit 102 predicts, on th...
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WO/2020/182946A1 |
Disclosed is a landing gear system uplock arrangement (300, 500) comprising: a hook (310) defining a gap (314), wherein the hook is movable between a first position, at which the hook is for retaining a movable element (299, 499) of a la...
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WO/2020/179461A1 |
An unmanned aerial vehicle 1 is provided with a main body 10 having a thrust generating unit 12 for flying in midair, a vacuum suction attachment device 20 which includes suction attachment portions 21 and which is attached to the main b...
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WO/2020/170489A1 |
An unmanned aerial vehicle (100) comprises: a sensor (120) that includes at least a microphone (105) which generates audio data; and a processor (101), wherein the processor (101) identifies the quality of the target sound using the audi...
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WO/2020/171315A1 |
An unmanned aerial vehicle landing system is disclosed. According to one aspect of the present invention, provided is an unmanned aerial vehicle landing system comprising: a step in which a server receives, from a wireless terminal, pixe...
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WO/2020/170510A1 |
An unmanned aircraft (100) is provided with a processor (101) and a sensor including at least a microphone (105) for generating sound data. The processor (101) determines the quality of a target sound using sound data generated by the mi...
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WO/2020/168189A2 |
Wind speed and direction experienced by the UAV at altitude is determined by placing an accelerometer, gyroscope and compass on the UAV. A change in velocity experienced by the UAV is determined by the accelerometer. An orientation relat...
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WO/2020/160471A1 |
An aircraft weight and balance measurement system and method comprises an identification means which enables each person (12) and/or object (16) boarding an aircraft to be tracked, and their weight to be known or estimated. A processing ...
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WO/2020/153171A1 |
A flight information acquisition unit 102 repeatedly acquires the flight status of each of a plurality of drones 20 that are in flight. An unplanned flight determination unit 103 determines whether a drone 20 has deviated from a flight p...
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WO/2020/153170A1 |
An avoidance processing unit 106 determines transmission control content on the basis of risk level information, which indicates the magnitude of risk when a drone 20 is flying. The avoidance processing unit 106 uses information indicati...
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WO/2020/153172A1 |
A flight information acquisition unit 102 periodically acquires flight information of drones 20 (information indicating flight statuses, including drone positions and flight directions). An unplanned flight determination unit 103 determi...
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WO/2020/149275A1 |
[Problem] To provide a system that includes a drone for executing a prescribed task by automatic flight, and a moving body for transporting the drone, wherein the operation efficiency of the drone can be improved and work stoppages cause...
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WO/2020/149289A1 |
[Problem] To provide a system that includes a drone for executing a prescribed task by automatic flight, and a moving body for transporting the drone, wherein the operation efficiency of the drone can be improved and work stoppages cause...
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WO/2020/145485A1 |
A drone including a vertical wing serving as a landing support according to an embodiment of the present invention comprises: a main body part of the drone; at least one pair of horizontal wing parts formed on the main body part so as to...
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WO/2020/144221A1 |
An aircraft moveable element monitoring system is provided. An exemplary aircraft moveable element monitoring system includes a signal generator (108), a signal transmitter coil (110) electrically connected to the signal generator (108);...
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WO/2020/140145A1 |
Methods and systems for multiple-buffered display rendering without the use of hardware or software interrupts. In a first repeating process, a processor writes data for a frame a selected frame buffer and, upon completion of the frame, ...
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WO/2020/138703A1 |
The present invention relates to an electromagnetic exploration system based on an airship with adjustable depth of investigation, in which a transmission coil (transmitter loop) and a reception coil (receiver loop) are arranged in two i...
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WO/2020/136429A2 |
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WO/2020/136752A1 |
The purpose of the present invention is to provide an unmanned aerial vehicle which, during an emergency of the aircraft, can quickly alert the people below of the emergency. This unmanned aerial vehicle 1 is provided with: an aircraft 2...
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WO/2020/137105A1 |
In a flying object (10), a PCU (32) has a plurality of operation modes in which an engine (16) and/or a motor generator (18) is used as a driving source for a pusher propeller (12). In accordance with the state of the flying object (10),...
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WO/2020/137554A1 |
[Problem] To control flight on the basis of the angle of attitude of an aircraft so as to adjust the points at which a chemical agent is dropped and achieve the proper effect of the chemical agent on cultivated land. [Solution] A chemica...
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WO/2020/136703A1 |
According to the present invention, a detection means (400) of an unmanned aerial vehicle control system (1) detects an object at a location where at least one of landing and takeoff of an unmanned aerial vehicle (20) is performed. A typ...
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WO/2020/137104A1 |
In a flying object (10), a PCU (32) has a plurality of operation modes in which an engine (16) and/or a motor generator (18) is used as a driving source for a pusher propeller (12). In accordance with the state of the flying object (10),...
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WO/2020/139466A1 |
Herein is disclosed an unmanned aerial vehicle light flash comprising a support structure; a camera coupled to the support structure and configured to take a photograph; one or more processors coupled to the support structure and configu...
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WO/2020/137103A1 |
In a flying object (10), a PCU (32) has a plurality of operation modes in which at least one of an engine (16), a first motor generator (17), and a second motor generator (19) is used as a driving source for a pusher propeller (12). In a...
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WO/2020/129315A1 |
[Problem] To reduce the influence of uncertainty on arrival time while suppressing deterioration in fuel efficiency and comfort by reducing the number of times speed is adjusted, and the like. [Solution] An information processing device ...
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WO/2020/127710A1 |
A configuration system (80) arranged to configure an aircraft in a single-pilot mode and a two-pilot mode, comprising: - acquisition means (84) and authentication means (83) arranged to acquire and authenticate a configuration order that...
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WO/2020/127703A1 |
Piloting device arranged to be integrated into a preexisting aircraft which comprises original systems comprising a flight control system and an autopilot system, the piloting device being separate and autonomous in relation to the origi...
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WO/2020/127704A1 |
An alternative piloting system (1) arranged to be integrated in a pre-existing aircraft that includes original systems comprising a flight control system (2) and an autopilot system (6), the alternative piloting system comprising: • a ...
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WO/2020/127702A1 |
An acquisition and analysis device (30) designed to be integrated into a pre-existing aircraft that has original systems comprising pilot commands able to be actuated by a pilot of the pre-existing aircraft and an autopilot system, the a...
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WO/2020/128793A1 |
Fiber-reinforced composites is provided. The composites include a plurality of prepreg layers, each comprising a polymeric resin and a plurality of fibers disposed therein; and at least one electrically-conductive layer at least partiall...
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WO/2020/127706A1 |
A method for piloting a pre-existing aircraft comprising the following steps: - integrating an alternative piloting system (1) into the pre-existing aircraft; - connecting the aircraft (200) and a ground station in which a ground pilot (...
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WO/2020/130333A1 |
The present invention relates to a vertical take-off and landing type hybrid drone comprising: a pair of front rotary rotors, which are formed on a fixed blade, perform a vertical rotation operation so that vertical taking-off and landin...
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WO/2020/129254A1 |
The present invention provides a flight device that reliably attaches a protective member to a flying body. This flight device 1 has: a flying body (drone) 2 having a main body 11 and at least one propeller held by the main body; a plu...
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WO/2020/122636A1 |
A movable device according to the present invention comprises: at least one lift generating unit for generating a pressure difference between opposite sides thereof to generate a lift force; a movable device body connected to the lift ge...
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WO/2020/121972A1 |
A moving body lamp 100 is a moving body lamp for a moving body configured to be capable of flying. The moving body lamp 100 is provided with: a spot lamp 120; a detecting unit 160 for detecting an object to be irradiated, present around ...
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WO/2020/118433A1 |
A method for detecting and reporting anomalies in operation of an aircraft. The method including the steps of: receiving real time data indicative of the operation of the aircraft, the real time data including at least one of the followi...
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WO/2020/121664A1 |
In a server device 20, an acquisition unit 21 acquires, via a network 2, information generated by each of a first detection unit 31 and a second detection unit 11. A specification unit 22 specifies wind conditions and flight conditions o...
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