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Matches 151 - 200 out of 63,000

Document Document Title
WO/2019/040714A1
A method for providing vehicle assistance to a vehicle when parking in a parking lot is provided. The method includes identifying, by the path controller, one or more available parking spaces based on the one or more images. The method i...  
WO/2019/038708A1
The invention concerns a satellite deployment system (30) for launch vehicles. Said satellite deployment system (30) comprises an outer dispenser (31) that is fitted, externally, with first releasable attachment means for releasably atta...  
WO/2019/037037A1
A propeller, comprising at least one blade (1, 2, 3), the blade (1, 2, 3) comprising a rigid body (11) and a soft edge (12) connected to the rigid body (11), the soft edge (12) extending outwards from the rigid body (11). Due to the pres...  
WO/2019/036803A1
Apparatus and methods for providing air to pneumatic loads such as an environmental control system for a passenger cabin of an aircraft or an ice protection device of the aircraft are disclosed. In one embodiment, the apparatus comprises...  
WO/2019/037452A1
A rudder device and an aircraft having same. The rudder device comprises: a rudder surface (10) connected to a stabilizing surface (100) by means of a first pivot shaft (11), the first pivot shaft (11) being parallel to an axial directio...  
WO/2019/040179A1
Various embodiments include methods that may be implemented in a processor or processing device of an aerial robotic vehicle for generating three-dimensional terrain map based on the plurality of altitude above ground level values genera...  
WO/2019/040490A1
A vehicle is provided having at least one control motor that includes a drive motor having a stationary portion and a rotatable portion, where the drive motor rotatable portion is coupled to a rotor shaft, where the drive motor is config...  
WO/2019/037036A1
An aerial device, comprising a body and, provided on the body, a plurality of vertical-lift rotors (3), a first horizontal rotor (41) and a second horizontal rotor (42), wherein an included angle is formed between the rotation axes of th...  
WO/2019/039988A1
An aircraft cleaning robot comprises a robot arm (14); a brush (34) rotatably attached to the robot arm (14) to be rotated about a brush rotation axis (R); and a controller (56) configured to control the position of the cleaning head (32...  
WO/2019/039983A1
Method for providing positioning data in a positioning node of a radio network, which positioning data is associated with a mobile device including a radio unit, the method comprising the steps of establishing a radio session for receivi...  
WO/2019/039063A1
A flight vehicle safety device (100) is equipped with a deployable body (10), an ejection mechanism, a bag-shaped member (50), and a gas generator. The deployable body (10) is wound or folded in an undeployed state, and generates dynamic...  
WO/2019/035732A1
The invention relates to space vehicles (modules) which are equipped with an artificial gravity system and have an audio-video studio integrated therein, capable of recording a sound from microphones inside spacesuits (99) and musical in...  
WO/2019/034909A1
The invention relates to a multi-rotor remote control aircraft for capturing audio and/or video signals and a method for remote controlling said aircraft by means of voice commands. In particular it concerns the mitigation of the effects...  
WO/2019/034765A1
The invention relates to a vertical takeoff aircraft (1), preferably an unmanned aerial vehicle (UAV), drone and/or unmanned aerial system (UAS), comprising: a rigid wing (5) which is oriented substantially horizontally both when hoverin...  
WO/2019/033768A1
A propeller, a power system, and an unmanned aerial vehicle, the propeller (111, 112) being used for connection to a power unit (50) and comprising a hub (150) and at least two blades (100). The at least two blades (100) may be foldably ...  
WO/2019/036361A1
Methods and system are disclosed for guiding an autonomous drone aircraft during descent to a landing target. The method features the steps of: (a) acquiring an image using a camera on the drone aircraft of an active fiducial system at t...  
WO/2019/036729A1
Techniques are provided for self-configuration of a sensor array. A methodology implementing the techniques according to an embodiment includes deploying a number of mobile sensor elements from a base unit to a region of interest. The me...  
WO/2019/034365A1
A control system (100) for a transportation vehicle (105) comprises a sensor vehicle (120) with at least one sensor (140) for scanning a surrounding area, wherein the sensor vehicle (120) is configured to move autonomously with respect t...  
WO/2019/034432A1
Disclosed is an actuation unit (15) for actuating a foldable wing tip portion (9) of a wing (3) for an aircraft (1). The object, to provide a highly compact and strong actuation unit, is achieved in that the actuation unit (15) comprises...  
WO/2019/034821A1
The present invention relates to equipment for physically and thermochemically characterising a fog of droplets of dimensions comprised between 1 and 500 ┬Ám, in a zone of measurement and comparison with a reference profile comprising il...  
WO/2019/036321A1
In some embodiments, methods and systems are provided that provide for controlling aerial and/or ground transport vehicles that are located beyond a communication range of a central control station via one or more aerial and/or ground in...  
WO/2019/036053A1
A system that includes a turbofan engine, a nacelle surrounding the engine and defining an annular bypass duct through the engine to define a generally forward-to-aft bypass air flow path, a thrust reverser movable to and from a reversin...  
WO/2019/035011A1
An airfield light includes a light assembly mounted on a base (26) and a transparent cover (30) disposed over the light assembly and secured to the base. The light assembly includes a curved LED (light emitting diode) assembly having a c...  
WO/2019/034851A1
The present invention provides a vehicle comprising: a rotor and a stator; at least one planar control surface coupled to the rotor, wherein the rotor is configured to rotate relative to the stator such that, in use, the at least one pla...  
WO/2019/035080A1
A system and method for distributing power to racing aircraft systems is provided. The system includes a race course, a power transmitter directed towards a power delivery section of the race course, the power transmitter configured to r...  
WO/2019/033769A1
Disclosed in the present application are a folding propeller, a power assembly, and an unmanned aerial vehicle. The folding propeller comprises: a propeller hub, at least two blade assemblies, and a connector for pivoting the propeller h...  
WO/2019/035014A1
Provided herein is technology related to embodiments of methods, systems, and apparatuses for deploying a drone swarm to target and/or capture remote objects through the use of a rotating subset of the drone swarm with nodes configured t...  
WO/2019/034843A1
The present invention provides an actuating system, comprising:a rotatable member rotatable relative to a fixed member;at least one actuator coupled to the rotatable member and to the fixed member; and a planar control surface coupled to...  
WO/2019/034908A1
The invention relates to an assembly and a method for powering an electric aircraft (200) by means of supplementary energy-supplying means. The electric energy delivered by such means reduces the energy drawn from the battery and recharg...  
WO/2019/036011A1
A vertical takeoff and landing (VTOL) aircraft is configured with a front set of propellers mounted to a front wing and an aft set of propellers mounted to an aft wing wherein the propellers may be repositioned by rotating them around a ...  
WO/2019/033691A1
Disclosed are a high-speed flying method for an unidentified flying object and a power deflection ring wing aircraft. The method is a method for generating a driving force in the horizontal direction by means of a saucer-shaped aircraft ...  
WO/2019/034906A1
The invention relates to a remotely controlled multirotor aircraft having a frame (1) that comprises a first and a second peripheral portions (12), to which at least one first and one second motor can be respectively coupled, and a centr...  
WO/2019/036462A1
A protective assembly (100) comprises a first region (102) formulated and configured to provide protection from alpha, beta, and electromagnetic radiation and comprising a composite of particles and polymer; a second region (104) formula...  
WO/2019/035378A1
A spacecraft (100) includes a principal airframe (6), a parachute (1), which is an air brake structure, and a jetting nozzle (5). The air brake structure is provided farther on one side in a traveling direction with respect to the princi...  
WO/2019/034907A1
The invention relates to a remotely controlled multirotor aircraft (0) for acquiring images and an interface device (3, 4) for controlling said aircraft, wherein said aircraft comprises receiving means adapted to receive a direction and/...  
WO/2019/030425A1
Various communication systems may benefit from an improved exchange of information pertaining to an unmanned aerial vehicle (UAV). For example, certain communication systems may benefit from the transmittal of information related to a pl...  
WO/2019/032167A1
Various embodiments include a drone having a landing control device that is configured to rotate wings into an auto-rotation descent configuration causing the drone to enter a nose-down attitude and spin about a long axis of the drone, a...  
WO/2019/030950A1
A control system for controlling an operation of a spacecraft. A model predictive controller (MPC) produces a solution for controlling thrusters of the spacecraft. The MPC optimizes a cost function over a finite receding horizon using a ...  
WO/2019/029551A1
An aerial system (12) includes a body (20), a lift mechanism (40) coupled to the body (20), a processing system (22), and at least one camera (52A, 52B). The aerial system (12) also includes a first motor (90) configured to rotate the at...  
WO/2019/032865A1
An aerial vehicle comprises: an electric power supply device, a motive power device, and a protective device disposed in an aerial vehicle body. The electric power supply device is configured to supply electric power to the motive power ...  
WO/2019/029387A1
An aircraft and an arm assembly (10) and frame thereof, the arm assembly (10) comprising: an elastic locking member (100), a fixing seat (200) and an arm (300); the arm (300) is rotatably connected to the fixing seat (200) such that the ...  
WO/2019/030634A1
A cabin furnishing element (100) for a cabin, such as a cabin of an aircraft, includes a panel (102) having a panel body. The panel body includes an illumination surface (106) having an illumination zone (110), and defines a lighting rec...  
WO/2019/030820A1
In order to more reliably land a flying vehicle at a desired location, the flying vehicle is provided with: a determination means which determines whether the flying vehicle is taking off and ascending from a take-off point, or is descen...  
WO/2019/029026A1
A propeller, comprising a propeller hub (10) and propeller blades (20). The propeller blades (20) are connected to the propeller hub (10); at a position whereof the distance to the center of the propeller hub (10) is 40% of the radius of...  
WO/2019/032091A1
A system that includes a computer and an unmanned aerial vehicle (UAV) is described. The computer may be programmed to receive, from the UAV, image data of a vehicle parking region; to process the data by identifying an actuation of a UA...  
WO/2019/030787A1
Structured set (10) suitable to make modular satellite structures (20), flat or three- dimensional, which is able to shield electromagnetic fields and/or variations in temperature in orbit, comprising a plurality of structural elements (...  
WO/2019/030020A1
The invention relates to an aircraft (100), comprising a drive unit (10) and a fuselage unit (20). The drive unit (10) has a first rotor (11) for providing a thrust on the aircraft (100). The fuselage unit (20) extends along an axis of r...  
WO/2019/030832A1
The present invention achieves a mechanism for an unmanned aerial body to receive power via contactless charging, while mitigating adverse effects on the performance of the unmanned aerial body. This unmanned aerial body comprises: a pla...  
WO/2019/030455A1
The invention proposes a method for building a rigid structure (1) comprising a framework (10) in space, characterized in that it comprises: the production of at least two reinforcing elements (12) from a reel of wire or metal strip, and...  
WO/2019/030116A1
The invention relates to a safety system for an unmanned flying object (1), flown by a user on the ground, the safety system making it possible to reduce the risks of the flying object (1) falling in the event of failure. The safety syst...  

Matches 151 - 200 out of 63,000