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Matches 1 - 50 out of 3,827

Document Document Title
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...  
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...  
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...  
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...  
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...  
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...  
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...  
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...  
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 ...  
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...  
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...  
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...  
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...  
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...  
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...  
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);...  
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, ...  
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...  
WO/2020/136429A2  
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...  
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),...  
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...  
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...  
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),...  
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...  
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...  
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 ...  
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...  
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...  
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 ...  
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...  
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...  
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 (...  
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...  
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...  
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...  
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 ...  
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...  
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...  
WO/2020/115440A1
The invention relates to a computing environment system for monitoring aircraft engines, said system being connected to a cluster of servers, said system comprising: - an application interface (13) configured so as to receive user codes ...  
WO/2020/116492A1
[Problem] Through cooperative operation of a drone and a movable body which is movable with the drone loaded thereon and at which takeoff and landing of the drone is allowed, high safety can be maintained even when the drone performs aut...  
WO/2020/116826A1
The present invention relates to a fall prevention device for a drone, for preventing damage from an impact caused by falling of an unmanned aerial vehicle such as a drone, wherein the fall prevention device is coupled to a drone which i...  
WO/2020/116396A1
[Problem] Through cooperative operation of a drone and a movable body which is movable with the drone loaded thereon and at which takeoff and landing of the drone is allowed, high safety can be maintained even when the drone performs aut...  
WO/2020/116442A1
[Problem] To provide a configuration in which a drone and a moving body that can move with the drone loaded thereon and that enables the drone to take off therefrom and land thereon operate together, and a high degree of safety can be ma...  
WO/2020/116496A1
[Problem] To provide a system in which a drone and a moving body that can move with the drone loaded thereon and that enables the drone to take off therefrom and land thereon operate together, and a high degree of safety can be maintaine...  
WO/2020/116443A1
[Problem] To cooperatively operate a drone and a movable body which can move while loading the drone thereon and on which the drone can take off and land, and to be capable of maintaining high safety even when the drone autonomously flie...  
WO/2020/116493A1
[Problem] To achieve coordinated operation of a drone and a moving body which can move with the drone loaded thereon and from which the drone can take off and land, and to maintain a high degree of safety even when the drone flies autono...  
WO/2020/116341A1
[Problem] To enable a high level of safety to be maintained even when a drone and a moving body, which is capable of moving with the drone carried thereon and on which the drone can takeoff and land, operate in cooperation and the drone ...  
WO/2020/116392A1
[Problem] Through cooperative operation of a drone and a movable body which is movable with the drone loaded thereon and at which takeoff and landing of the drone is allowed, high safety can be maintained even when the drone performs aut...  
WO/2020/113388A1
Disclosed are a control assembly (100) and an aircraft (200). The control assembly (100) comprises a bearing plate (11), a central plate (12), a flight control plate (13), a vibration reduction mechanism (14), and a communication connect...  

Matches 1 - 50 out of 3,827