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Matches 1 - 50 out of 3,134

Document Document Title
WO/2018/066043A1
Provided is a delivery rotary-wing aircraft capable of stably landing on a destination free of influence from an updraft occurring in a region, such as tall buildings. This rotary-wing aircraft comprising a plurality of rotary wings, a c...  
WO/2018/061280A1
A flight restriction setting system according to an embodiment comprises a damage detection unit and a flight restriction calculation unit. The damage detection unit detects damage that occurred on a structure that constitutes an aircraf...  
WO/2018/064657A1
An unmanned aerial vehicle (UAV) landing system is disclosed. The UAV landing system includes a memory; an imaging device; and a processor in communication with the memory and imaging device, wherein the processor is configured to: acqui...  
WO/2018/053994A1
Embodiments include devices and methods for adaptive image processing in an unmanned autonomous vehicle (UAV). In various embodiments, an image sensor may capture an image, while a processor of the UAV obtains attitude information from o...  
WO/2018/055827A1
A damage detection system according to an embodiment comprises a physical quantity detection unit, a flight condition changing unit, and a damage detection unit. The physical quantity detection unit detects the physical quantity of a str...  
WO/2018/051572A1
[Problem] To achieve a stable airspeed control that takes remote turbulence into account. [Solution] This aircraft speed information providing system is provided with: an airspeed measurement device that measures the present airspeed of ...  
WO/2018/048774A1
Described herein are methods and systems to dampen oscillations of a payload coupled to a tether of a winch system arranged on an unmanned aerial vehicle (UAV). For example, the UAV's control system may dampen the oscillations by causing...  
WO/2018/045413A1
There is provided a system for determining real-time parameters of an aircraft, the system comprising: at least two sensing apparatus, each of the at least two sensing apparatus including a plurality of in-ground sensors; and at least on...  
WO/2018/045661A1
An information protection method for an unmanned aerial vehicle, the unmanned aerial vehicle comprising an ARM controller (1) and an information protection module (4). The method comprises: an ARM controller (1) transmitting, back to a c...  
WO/2018/048627A1
Some embodiments provide an aerial monitoring system to monitor a geographic area, comprising: a unmanned aerial vehicle (UAV) comprising: a plurality of lift motors to drive a propeller; a substructural support supporting the lift motor...  
WO/2018/042927A1
[Problem] To provide a mechanism of radio communication for a device that flies around freely in a three-dimensional space. [Solution] A circuit provided with: an acquisition unit that acquires information relating to a flight; and a mea...  
WO/2018/044243A1
This invention is system designed in particular to separate the plane's black box (data recording box) in case of being exposed to an accident that causes its drowning in the sea, ocean, or, elsewhere waters, yet in a following step to t...  
WO/2018/041253A1
A black box control method comprises: acquiring current flight data of an aircraft, wherein the flight data comprises a collision signal, a loss-of-control signal, and a stall signal; determining, according to the flight data, whether th...  
WO/2018/038441A1
An electronic device is provided. The electronic device includes a gimbal; a first camera; a second camera to detect a point of interest on ground; at least one sensor; a first motor; a second motor to operate the first camera and the se...  
WO/2018/032264A1
An unmanned aerial vehicle machine body anti-collision structure, comprising a machine casing (1), an inner side wall of the machine casing (1) being fixedly provided with a buffer box (2), a side wall of the machine casing (1) being pro...  
WO/2018/030651A1
Disclosed is an unmanned aerial vehicle comprising: a main body; a plurality of propeller connection parts extending from at least one side surface of the body at a specified length; a plurality of propellers respectively connected to th...  
WO/2018/030880A3
An unmanned aerial vehicle according to an embodiment of the present invention comprises: a storage unit for storing information on a virtual fence (geo-fence) area, and flight approval information or photographing-approval information o...  
WO/2018/030880A2
An unmanned aerial vehicle according to an embodiment of the present invention comprises: a storage unit for storing information on a virtual fence (geo-fence) area, and flight approval information or photographing-approval information o...  
WO/2018/024310A1
It is an integrated system that (RECORD) registers the events on the plane (video/audio) and stored on the hard disk to get to know the truth of what happened on the aircraft in emergency situations and disasters and we can also get a li...  
WO/2018/024069A1
Provided are a method, device and system for guiding an unmanned aerial vehicle to land. A navigation apparatus in an unmanned aerial vehicle issues a landing instruction to the ground, so that a landing platform receiving the landing in...  
WO/2018/022021A1
Apparatus, method and storage medium associated with UAV assisted emergency responses are disclosed herein. In embodiments, an UAV may comprise a flight controller to control at least one or more engines of the UAV to navigate the UAV to...  
WO/2018/018710A1
An unmanned aerial vehicle and a flight level control method utilized in an unmanned aerial vehicle. The unmanned aerial vehicle comprises an infrared emitter module (10) and an infrared receiver module (11). The method comprises: acquir...  
WO/2018/020303A1
The invention relates to a display for 3D aircraft visualisation and flight path features. The display system is for use on the flight deck of an aircraft and comprises a display operable for graphical display of data, and a processor op...  
WO/2018/016793A1
The present invention relates to a drone control device using a composite sensor and a method therefor. A method for controlling a drone by using a drone control device, according to the present invention, comprises the steps of: receivi...  
WO/2018/012768A1
Disclosed are a system and method for sensing and controlling the crash of an unmanned aerial vehicle. The system includes a crash sensing device detachably mounted on an unmanned aerial vehicle and configured to sense a crash situation ...  
WO/2018/011791A3
A device, system and method is provided for obtaining and processing turbulence data via communication devices located on-board airplanes. Turbulence data obtained by a plurality of communication devices may be received during flights on...  
WO/2018/010757A1
This Invention relates to a device and a method for protecting and locating the flight recorder(s) data; able to automatically eject of a fallen aircraft, guiding the rescue teams to its location and the location of the wreck of the miss...  
WO/2018/006120A1
A vehicle security system, particularly for aircraft, comprises at least one first actuator in a cockpit of the vehicle operable to control a cockpit door lock and a plurality of second actuators in a passenger section of the vehicle ope...  
WO/2018/001653A1
The invention relates to a lightning protection system for, e.g., a non-static industrial installation, such as a wind turbine, and to a method for producing a lightning protection system. By means of the invention, a highly effective co...  
WO/2018/005416A1
A dual curable thiol-ene composition comprising a polythiol, an unsaturated compound, a photoinitiator, an organic hydroperoxide (thermal initiator) and optionally a nitrogen-containing base, such as e.g. an N-heterocyclic compound (toge...  
WO/2018/002878A1
An aircraft avionic system for use in an equipped aircraft includes a controller and a display. The controller provides output data to the display, with the output data producing visual images on the display. An angle of attack data sour...  
WO/2018/005529A1
A temperature monitoring unit may be removably installed inside an aircraft wing structure for monitoring temperature conditions along the span of the wing. The wing structure has a temperature-sensitive device (162) for monitoring a tem...  
WO/2017/219203A1
An unmanned aerial vehicle (100). The unmanned aerial vehicle (100) comprises an unmanned aerial vehicle main unit (1), multiple rotors (2), a telescoping rod (4), a photographing device (5), and a parachute (7). The rotors (2) provide t...  
WO/2017/222628A1
An engine communication system for aircraft engines having a nacelle with two cowlings extending annularly about the aircraft engine and defining a radially outward surface thereof, and at least one sensor positioned radially inward from...  
WO/2017/216972A1
The present invention allows an unmanned aircraft to fly while avoiding a flight prohibited area, which changes depending upon the movement of a mobile unit. This unmanned aircraft control system (1) includes: a mobile unit position acqu...  
WO/2017/216119A1
A system for monitoring an aircraft device (1), comprising a master electronic module and a slave electronic module each equipped with first wireless communication means (5), the slave electronic module further comprising measurement mea...  
WO/2017/218172A1
Various systems and methods for disabling UAVs are presented. An interrogation system may transmit an identifier request message to a UAV. The interrogation system may receive, in response to the identifier request message, a response me...  
WO/2017/218332A1
A ventilation louver (10) includes a first plate (52) defining a first opening (74) therein for permitting fluid flow along a first direction (128), a second plate (54) defining a vane (82) therein, the vane at least partially covering t...  
WO/2017/213392A1
Disclosed is a drone. The present invention includes a plurality of propellers creating a lift to prevent inclination and overturn of the drone due to a lift difference generated from uneven ground, a power driving unit providing a rotat...  
WO/2017/195133A1
A method of and a system for displaying an aircraft control input. The method comprises accessing a first indication indicative of an aircraft control input, the aircraft control input being associated with an orientation and an amplitud...  
WO/2017/195963A1
The present invention relates to a wind power generation system using an airship, wherein wind power generation is performed by means of an airship which uses the strong wind of jet streams, the generated electric power is converted into...  
WO/2017/192348A1
System for reducing likelihood of an aircraft-induced lightning strike on an aircraft (10). The system includes a plurality of electric field sensors (12) distributed on surfaces of the aircraft to monitor continuously the electrical env...  
WO/2017/191810A1
The present invention addresses the problem of providing a flight altitude correction system and a flight altitude correction method with which turbulence in the flight altitude of an unmanned air vehicle due to air pressure changes can ...  
WO/2017/189325A1
Systems and methods for obstruction detection during autonomous unmanned aerial vehicle landings, including unmanned aerial vehicles equipped with at least one video camera, an image processor that analyzes a teed from the video camera t...  
WO/2017/188587A1
An aerial vehicle having incline-controllable wings, according to one embodiment, can comprise: a body; a thrust part connected to the body and having a propeller and a rotary shaft; and the wings respectively arranged at both sides of t...  
WO/2017/184439A1
An aircraft, such as an unmanned aircraft, can include a forward propulsion system comprising one or more engines and one or more rotors coupled to a corresponding engine; a vertical propulsion system comprising one or more vertical prop...  
WO/2017/184327A1
An unmanned aerial robotic vehicle (UARV) that can fly to an object such as a palm tree, hover in place adjacent to the object, mount itself securely and releasably to a mounting location on the object using a mounting mechanism, and whi...  
WO/2017/182836A1
A control stick pivot (200) comprises a primary pivot bearing (210), a redundant pivot bearing (220), and a detection component for detecting malfunction of the primary pivot bearing. The redundant pivot bearing is provided on one side o...  
WO/2017/180840A1
A system for calculating maintenance predictions and making improvements to performance deficiencies to one or more components in an on-board inert gas generating system (OBIGGS) is described. The OBIGGS components include an ozone conve...  
WO/2017/174911A1
The invention pertains to a luminous display device (14) designed to be fixed on the fairing of an aircraft, the device comprising: -an electroluminescent film (140); -an electrically conducting protection film (142), designed to be inse...  

Matches 1 - 50 out of 3,134