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Matches 101 - 150 out of 58,580

Document Document Title
WO/2018/002514A1
Part comprising a wall which comprises a first zone (541), a first zone (541) and the second zone (542), a network of riblets being formed on the first zone (541), the second zone (542) and also on the transition zone (54t) so as to redu...  
WO/2018/004500A1
With the present invention, there is provided a carriage system (S), which is suitable for use in an air vehicle, and which is capable of safely carrying at least a load by being attached thereto. Said carriage system (S) comprises a ret...  
WO/2018/000696A1
Disclosed is an unmanned aerial vehicle comprising a body (10), wherein the body (10) is provided with an image collection apparatus, the image collection apparatus comprises multiple cameras (13), the cameras (13) are fixed on a surface...  
WO/2018/002682A1
A vessel (1) designed for enclosing at least one sensor (10) is arranged within a fuel tank. The vessel is provided with a fuel inlet (50) connected to a refuelling arrangement of the tank, and with through-holes (20, 30) for the fuel to...  
WO/2018/001967A1
The invention relates to a device for storing and extending a hose for supplying conditioned air to an aircraft on the ground or to any other interior space, said device comprising: a rigid pipe (2) extending from a first end to a free s...  
WO/2018/004798A1
System and techniques for unmanned aerial vehicle navigation are described herein. A plurality of transmission beams may be established. Here, each beam in the plurality of transmission beams is a focused photonic propagation directed to...  
WO/2018/002855A1
Apparatus and method for conditioning engine-heated air onboard an aircraft including a heat exchanger (140) at least partially disposed in a pylon structure (118) for supporting an engine (134) of the aircraft. The pylon heat exchanger ...  
WO/2018/005364A1
A system and method for communicating with deep space spacecraft are provided. A near-Earth space based communications system satellite, which may be deployed in a deep space stable-looking orbit around the Earth, provides two-way commun...  
WO/2018/004493A1
This invention relates to high efficiency double pitch angle propellers, and is such that it has a propeller hub (2, 7); and two or more propeller blades (1, 6) with aerofoil-shaped cross-section (1a, 6a) fixed around the periphery of th...  
WO/2017/222249A1
The present invention relates to a gimbal assembly for a drone, comprising: a first unit mounted on a flight body of a drone to be able to rotate forward/backward, an operation space being formed in the middle of the first unit; a second...  
WO/2017/220940A1
Disclosed is an annular shroud (10) for a bladed wheel (80), comprising an axially extending annular wall (10A) that has a plurality of axially extending slots (12), each of said slots (12) being designed to accommodate a leading edge (8...  
WO/2017/220130A1
A method (50) of route directing performed in an unmanned aerial vehicle (8a) is provided. The unmanned aerial vehicle (8a) comprises a communication module (9a) for wireless communication with an access node (2a, 2b) of a communications...  
WO/2017/221859A1
[Problem] The present invention addresses the problem that functional components for causing multiple moving bodies to operate in a coordinated manner have to be designed individually in conformity to functional components for causing th...  
WO/2017/222642A1
Embodiments include devices and methods for determining a spin direction of a motor (125) of an unmanned aerial vehicle (UAV 100). A processor (160) of the UAV applies a first power to the motor in a first direction. The processor determ...  
WO/2017/222848A1
Examples of devices, systems, and methods to manage aircraft water and waste servicing are disclosed. In one example, an aircraft water and waste controller has a network interface to receive water and waste data from water and waste dev...  
WO/2017/219295A1
An unmanned aerial vehicle (UAV) (100). The UAV (100) comprises a central body (105). The UAV (100) also comprises a plurality of landing gears (120) that are extendable from and movable relative to the central body (105). The plurality ...  
WO/2017/221560A1
[Solution] A flight control unit 201 causes one or a plurality of unmanned aerial vehicles 12 to fly along a flight path in a prescribed area. When a wireless device 11 of the unmanned aerial vehicle 12 detects a close-range wireless rad...  
WO/2017/219201A1
An unmanned aerial vehicle (100). The unmanned aerial vehicle (100) comprises an unmanned aerial vehicle main unit (1), multiple rotors (2), and a parachute (4). The unmanned aerial vehicle main unit (1) is connected to the rotors (2). T...  
WO/2017/222826A1
Provided are aerodynamic articles and related methods that use an aerodynamic body with a microstructured surface thereon. The microstructured surface has a plurality of parallel primary ridges defining major capillary channels, and opti...  
WO/2017/219200A1
An unmanned aerial vehicle (100) comprising an unmanned aerial vehicle main unit (1), multiple rotors (2), a telescoping rod (4), and a photographing device (5). The unmanned aerial vehicle main unit (1) is connected to the rotors (2) an...  
WO/2017/223065A1
A power supply system and related method for providing a regulated DC output from an unregulated AC input includes a Vienna rectifier (2) having power factor correction circuitry (29) and a series resonant DC to DC converter (5) to provi...  
WO/2017/219057A1
The invention relates to a self-propelling transport vehicle (1), comprising: a chassis (3) which extends with respect to the length (4) thereof in a direction of travel (7) and extends with regard to the width (5) thereof transversely w...  
WO/2017/220803A2
A surface treatment apparatus comprising a support frame, said support frame comprising one or more lift generating portions arranged in use to cause vertical movement of the support frame and one or more biasing portions arranged in use...  
WO/2017/221123A1
The present disclosure provides methods and system for managing gust loading in an aircraft. A deflection angle of one or more spoilers of the aircraft is monitored. When the spoiler deflection angle is above a first threshold value, one...  
WO/2017/223458A1
Embodiments relate to methods and apparatus to swiftly and accurately deliver a medical treatment kit via an Unmanned Aerial Vehicle and mechanisms and systems for monitoring a medical emergency via an Emergency Control Center and provid...  
WO/2017/222542A1
An unmanned aerial vehicle may include a flight control circuit configured to control flight of the unmanned aerial vehicle and to provide a flight path based at least on an actual position of the unmanned aerial vehicle and a desired ta...  
WO/2017/221872A1
This expandable antenna is provided with a plurality of ribs which are arranged with a regular angular pitch around the outer circumference of a hub, and a metal mesh which is suspended between a plurality of adjacent ribs, wherein: each...  
WO/2017/221235A1
A centering system for positioning an Unmanned Autonomous Vehicle (UAV) is provided with two or more supporting extremities rigidly connected thereto, comprising a pair of displaceable positioning elements provided with surfaces sloped r...  
WO/2017/221387A1
Provided is an unmanned aircraft with high space efficiency in storage, such that flight disturbances and noise caused by vibrations of rotors are minimized. To address this, the unmanned aircraft comprising a plurality of rotors which, ...  
WO/2017/222152A1
The present invention relates to an electronic apparatus and a method for operating the same according to various embodiments. The electronic apparatus comprises: a moving module comprising a motor; an audio module comprising a first noi...  
WO/2017/221236A1
A payload exchange facilitating connector module, comprises : a) a structure secured to a payload; b) a locking member operatively connected to said structure! c) a locking initiating element that is settable in force transmitting relati...  
WO/2017/219199A1
An unmanned aerial vehicle. The unmanned aerial vehicle comprises an unmanned aerial vehicle main unit (1), multiple rotors (2), and a photographing device (4). The unmanned aerial vehicle main unit (1) is connected to the rotors (2) and...  
WO/2017/219256A1
A flying cleaning device capable of wall-climbing comprises an aircraft main engine, a wall-climbing assembly, a start-stop assembly, a cleaning assembly and a control module; the wall-climbing assembly comprises a first suction cup (32)...  
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/2017/219202A1
An unmanned aerial vehicle (100) comprising an unmanned aerial vehicle main unit (1), multiple rotors (2), a photographing device (4), and a parachute (6). The unmanned aerial vehicle main unit (1) is connected to the rotors (2) and to 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/2017/220931A1
The invention relates to an assembly of a fixed internal structure (54) of a turbojet engine nacelle (2) and thermal protection panels (640, 642), said fixed internal structure (54) comprising an inner face (540), on which the thermal pr...  
WO/2017/219255A1
Unmanned aerial vehicles with tilting propellers, and associated systems and methods are disclosed herein. A representative unmanned aerial vehicle (UAV) apparatus includes an airframe(110), a plurality of spherical motors(120) carried b...  
WO/2017/223531A1
An unmanned aerial system (UAS) may comprise an unmanned aerial vehicle (UAV) configured to search and recover persons and things, collect and produce data of an emergency situation for display on a vehicle navigation system, or explore ...  
WO/2017/221867A1
[Problem] To provide a moving device which moves from the current location if it is determined that communication between a communication device and an external communication device is not established and which transmits user-related inf...  
WO/2017/221122A1
The present disclosure provides methods and system for controlling the operation of a fly- by-wire aircraft. One or more yaw commands are received from an operator control, and one or more actual induced rolls rates are determined based ...  
WO/2017/215200A1
A wirelessly-chargeable unmanned aerial vehicle, comprising a body (10), a wing (20), a bionic mechanical leg (30), and a receiving device (50) provided on the body. The receiving device is used for receiving energy emitted by an energy ...  
WO/2017/216689A1
Ducts and methods for directing a flow of air from air-cooled devices onboard aircraft are disclosed. An exemplary method disclosed comprises: receiving air carrying heat extracted from the device, directing the air away from the device,...  
WO/2017/217470A1
The present invention makes it possible for sounding of an inspection location on an outer wall of a building or the like to be performed using a simple operation. A user interface device accepts an input for designating an inspection lo...  
WO/2017/216468A1
The invention relates to a gasket (80) designed to be inserted between two parts of a propulsion unit (1) of an aircraft, said gasket (80) comprising a base (84) and a cylindrical tubular part (82), the base (84) and the tubular part (82...  
WO/2017/214985A1
Disclosed is a retaining device (300), comprising a support base (30) and a driving member (50) for driving the support base (30) to move, wherein the support base (30) is used for retaining an electronic apparatus (200). The retaining d...  
WO/2017/216462A1
The invention concerns an assembly comprising: a fuel supply circuit (15, 15a, 15b) configured to supply fuel to a turbine heat engine, an electronic module (14, 14a, 14b), a power source (13, 13a, 13b) for supplying power to the electro...  
WO/2017/215462A1
A reusable air-launched carrier rocket which has no landing leg, is mounted on a centerline pylon of a supersonic fighter or bomber, and has a length that is not limited by a front landing gear (4) of a carrier. The rocket is provided wi...  
WO/2017/216760A1
Described is a safety system and method for tracking suspected intruders at a premises by a drone (4). After triggering of an alarm signal by a surveillance system (3), a drone is dispatched from a central operations unit (2) to the surv...  
WO/2017/218801A1
A hypersonic aircraft having a homopolar motor with high temperature superconducting (HTS) non-insulated (NI) coil magnets is described. In some implementations, the HTS NI coil magnets can have a graded resistance design. In some implem...  

Matches 101 - 150 out of 58,580