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Patent Searching and Data


Matches 1 - 50 out of 3,928

Document Document Title
WO/2021/011097A1
Aspects of the technology relate to propulsion systems for high altitude, long duration balloons, such as balloons that operate in the stratosphere for weeks, months or longer. A propeller assembly is used to provide lateral directional ...  
WO/2021/004889A1
A skew detection system for an aircraft flight control surface, the flight control surface being moveable relative to fixed structure of the aircraft by operation of a first gear rack driven by a first gear pinion and by operation of a s...  
WO/2020/259748A1
The invention relates to a device for preventing access to an area on an aircraft, having a first vertical jamb (8) and a second vertical jamb (9) for fastening to a structure of the aircraft and having a barrier element (13), which is d...  
WO/2020/264487A1
A distributed control system for a vehicle includes a configuration controller and at least three nodes communicatively coupled to the configuration controller. Each of the at least three nodes includes a memory device for storing local ...  
WO/2020/262528A1
In the present invention, a server device 20 controls a flying object 10 to cause the flying object to fly close to a transmission line and photograph the transmission line. The flying object 10 is equipped with a GPS positioning device,...  
WO/2020/263528A1
An overhead storage bin display system that includes an overhead storage bin defining a bin interior and a display member associated with the overhead storage bin. The display member is configured to display passenger related information...  
WO/2020/222718A3
The invention is related to an ULD apparatus (1) which helps loading cargo packages to ULD pallets used in air transportation, comprises a frame (2) which is in different structures according to the type of the airplane and pallet, forms...  
WO/2020/256173A1
Disclosed are a precise landing method using multiple patterns in an unmanned aerial control system, and a device therefor. Specifically, an aspect of the present invention relates to a precise landing method of an unmanned flying robot ...  
WO/2020/253974A1
Method of surface protection of fasteners by application of sealant and paint, which comprises the following steps according to the following sequence:positioning a plurality of overcoat nozzles (1) on a rack (2); painting the interior o...  
WO/2020/249840A1
The invention relates to an electromagnetic variable-radiofrequency compensator device for the protection of the blades of wind turbine towers or other movable or static structures, which comprises: two conductive connection adapters (1,...  
WO/2020/251647A1
A low visibility aid device includes a main body having a front end, a back end, a middle section and an interior space. A mounting bracket extends outward from the main body for securing the device onto a manned aircraft for use during ...  
WO/2020/247641A1
Systems and methods are directed toward determining a vehicle orientation based on sensor information. Sensors are positioned along a vehicle body that may be evaluated to determine corresponding values between matching sensor types. Whe...  
WO/2020/239881A1
The present application relates to a spark containment cap. The cap forms a sealed cavity around an end of a fastener protruding from a structure. The cap has a cap body defining an air cavity arranged to enclose the end of the fastener....  
WO/2020/239780A1
A leading-edge component for an aircraft is proposed, the component comprising at least a part of a flow body having a front skin, a hollow space at least partially delimited by the front skin and at least one separate retention device, ...  
WO/2020/230964A1
A device for displaying a flight area on the ground and an operation method therefor are disclosed. The device for displaying a flight area on the ground according to an embodiment may comprise: a light generator for projecting an image ...  
WO/2020/229749A1
This unmanned aerial vehicle has an autonomous electric power source (44A, 44B), a housing (14) whose inner volume contains electronic devices (46, 48A, 48B, 48C, 48D, 50, 52, 54, 56) that are supplied with electricity by the power sourc...  
WO/2020/229750A1
The invention relates to an unmanned aerial vehicle (10) comprising an autonomous power supply source (12), a housing (14), in the internal volume of which is arranged electronic equipment which is electrically powered by the power sourc...  
WO/2020/229778A1
The present intention relates to a method for resetting the static pressure model (mod_Ps3(PCN25R)), called "Ps3 model", upstream of a combustion chamber in a turbine engine comprising a compressor (3), the Ps3 model being used to arbitr...  
WO/2020/229751A1
The invention relates to an unmanned aerial vehicle, comprising an autonomous power supply source (44), a central housing (14), in the internal volume of which is arranged electronic equipment electrically powered by the power source and...  
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...  
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 ...  
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...  
WO/2020/168189A3
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/2020/180520A3
Apparatus to monitor the position of an aircraft landing gear.  
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...  
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...  
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...  
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 ...  
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...  
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...  
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. ...  
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...  
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...  

Matches 1 - 50 out of 3,928