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Matches 1 - 50 out of 55,262

Document Document Title
WO/2017/025704A1
An unmanned aerial vehicle (2) comprising: a fuselage (4); and a wing (6) comprising a central wing section (12) pivotably mounted to the fuselage (4) and a pair of outer wing sections (14a, 14b) pivotably mounted to the central wing sec...  
WO/2017/025060A1
A fixed-wing aircraft capable of taking off and landing vertically, and a flight control method therefor. The fixed-wing aircraft comprises an aircraft body (10). The aircraft body (10) is provided with fixed wings (11) and a propeller (...  
WO/2017/024391A1
An auxiliary power unit for an aircraft includes a rotary intermittent internal combustion engine drivingly engaged to an engine shaft, a turbine section having an inlet in fluid communication with an outlet of the engine(s), the turbine...  
WO/2017/025884A1
A method including retrieving a multi-dimensional map (30) from a navigation system memory (27); determining an aerial route (64) between two locations (60, 62) based at least partially upon the multi-dimensional map (30); and storing th...  
WO/2017/027629A1
Systems and methods in accordance with various embodiments of the invention implement textured metasurfaces that can provide for enhanced thermal emissivity. In one embodiment, a lightweight solar power generator includes: at least one p...  
WO/2017/025288A1
The invention seeks to get around the problems of mass and complexity of pylons made up of assembled box sections. In order to do so, the invention effectively proposes organizing the engine - wing interface around a substantially unifor...  
WO/2017/024392A1
An aircraft heating assembly including an internal combustion engine having a liquid coolant system distinct from any fuel and lubricating system of the engine and including cooling passages in the internal combustion engine for circulat...  
WO/2017/025778A1
This disclosure relates to a satellite attitude control apparatus, comprising a spherical inertial body (1), which is arranged to be rotated in space in a desired rotational mode, one or more rotational feedback sensors. The apparatus fu...  
WO/2017/027406A1
A refrigeration system for cooling a plurality of compartments includes a chiller and a duct providing fluid communication between the chiller and a plurality of compartments. The refrigeration system additionally includes a plurality of...  
WO/2017/025691A1
The invention concerns an artificial satellite comprising one face from the North face and the South face supporting at least one main radiator (42, 44) having an outer face turned towards space and an inner face opposite the outer face....  
WO/2017/025497A1
The invention relates to a processing station for aircraft structural components, comprising a portal processing machine (3), a clamping frame (4) for fastening at least one component (2), and a holding device arrangement (5) for receivi...  
WO/2017/024389A1
An auxiliary power unit for an aircraft includes a rotary intermittent internal combustion engine, a turbine having an inlet in fluid communication with an outlet of the engine, the turbine compounded with the engine, a compressor having...  
WO/2017/027079A1
A device for obtaining surveillance information from an aerial vehicle. The device includes a camera configured to obtain image data based on a position of the vehicle, a transceiver configured to receive operator controls and output the...  
WO/2017/024390A1
An auxiliary power unit for an aircraft, including an internal combustion engine having a liquid coolant system, a generator drivingly engaged to the internal combustion engine and having a liquid coolant system distinct from the liquid ...  
WO/2017/026354A1
Provided are a loss prevention device that makes it possible to efficiently search for and retrieve an unmanned aircraft that has gone missing, an unmanned aircraft that is provided with the loss prevention device, and an unmanned aircra...  
WO/2017/027617A1
A space-based solar power station, a power generating satellite module and/or a method for collecting solar radiation and transmitting power generated using electrical current produced therefrom is provided. Power transmitters can be coo...  
WO/2017/024394A1
An engine assembly for an aircraft, including an internal combustion engine having a liquid coolant system in fluid communication with a heat exchanger, an exhaust duct in fluid communication with air passages of the heat exchanger, a fa...  
WO/2017/027087A1
Trailing edge components (23), aircraft structures comprising such trailing edge components, and methods of manufacturing such trailing edge components are provided. A trailing edge component (23) includes a first skin (24) comprising a ...  
WO/2017/027780A1
A drone comprises at least one propeller for generating lift and an article containment area for containing an article to be carried by the drone. The floor of the article containment area comprises a dynamic support surface for supporti...  
WO/2017/026337A1
Provided is a flight control device that prevents an unmanned aircraft from deviating from a predetermined allowed flight area and that can forcibly prevent deviation from said allowed flight area even when there is an abnormality in the...  
WO/2017/024623A1
The present invention relates to the technical field of aircrafts, and provides a variable pitch rotorcraft and multirotor. The variable pitch rotorcraft comprises: a power unit having an output axis, at least two propellers and a transm...  
WO/2017/027633A1
Many embodiments of the invention include stacked power amplifier configurations that include control circuitry for sensing the operational characteristics of the power amplifiers and adjusting the current drawn by one or more of the pow...  
WO/2017/021142A1
The invention is directed to an installation system (1) for installing at least one auxiliary device (2a-f) overhead and/or at a sidewall area in a fuselage (3) of an aircraft (4). The installation system comprises at least one in princi...  
WO/2017/020881A1
The invention relates to a guide carriage (15) for an engine component (16c), in particular for a fan module of a gas turbine (10), comprising a base element (75), on which there is arranged a supporting device for (77) holding the engin...  
WO/2017/020882A1
The invention relates to an assembly system (12) for assembling, disassembling and/or maintaining a gas turbine (10). The assembly system (12) comprises a first guide carriage (14a) for holding a first engine component (16a), in particul...  
WO/2017/021001A1
The invention relates to a canopy for a paraglider, parachute, flexkite, or surfkite canopy, consisting of an upper sail (12) and a lower sail (14), and of profile ribs forming a profile, characterised in that at least two separate press...  
WO/2017/023788A1
A latch (10) including a housing (12) having side members (18, 20) each having an elongated slot (22), a bolt (46) mounted rotatably to the housing (12) and positioned between the side members (18, 20) of the housing (12), a trigger (64)...  
WO/2017/021608A1
The rotor of a hybrid aerodyne, intended to produce lift by means of the rotation of same in the vertical flight phase and then to be immobilised and stored longitudinally in the cruise flight phase, comprises at least two single-blade p...  
WO/2017/022993A1
The present invention relates to a method providing various pieces of green information required for putting to a golfer terminal by making information on a green of a golf course into a database in advance, enabling a drone to photograp...  
WO/2017/021722A1
A method of producing part of an aircraft (2) comprising: providing a frame (4) having a first surface (10), a second surface (12), and one or more side edges (14) between the first and second surfaces; mounting the frame (4) to a first ...  
WO/2017/021191A1
A propulsion system for small artificial satellites comprises a plurality of engines (2) fixable to a frame (101) of a satellite (100); a control unit (3) connected functionally to the engines (2) for sending at least one activation sign...  
WO/2017/021918A1
The invention concerns a convertible aircraft comprising a fuselage (F), a pair of wings (A1, A2) disposed to either side of the fuselage (F), at least one ducted rotor (1) installed in a horizontal position at one of the ends of the fus...  
WO/2017/023410A1
A flight path of a physical aircraft vehicle is planned. A virtual three-dimensional model of a physical environment is provided. A placement indicator is tracked within the virtual three-dimensional model of the physical environment. Tr...  
WO/2017/021758A1
The invention relates to the field of aerospace and describes a carrier aircraft device intended for carrying aircraft and spacecraft into the atmosphere for the subsequent launch thereof (so-called air launch). The carrier device makes ...  
WO/2017/022058A1
This location management device 10 is a device for managing the location of an unmanned aerial vehicle 20. First, the location management device 10 is positioned in the sky over the flight airspace 40 of the unmanned aerial vehicle 20, a...  
WO/2017/020763A1
An unmanned aerial vehicle comprises an aerial vehicle body (1), the aerial vehicle body (1) comprising a fuselage (2) and a storage device (4); aerial vehicle arms, the aerial vehicle arms comprising at least two front aerial vehicle ar...  
WO/2017/021537A1
The invention relates to a cable winch (100) for an aircraft or vehicle. The cable winch (100) has a central module (110), which can be or is attached to the aircraft or vehicle. The central module (110) is shaped in such a way that the ...  
WO/2017/022805A1
The present invention establishes a technology for accurately monitoring and managing small aircraft that frequently fly. A small aircraft 1 is provided with: an aircraft ID storage unit 201 that stores an aircraft ID that uniquely ident...  
WO/2017/021628A1
The invention particularly relates to an acoustic attenuation structure for a propulsion assembly of an aircraft, comprising an acoustically reflective wall and a sandwich panel, the sandwich panel comprising a honeycomb structure surrou...  
WO/2017/022179A1
This control unit (11) of an unmanned flying body (1) determines whether or not the unmanned flying body (1) lies outside the visual field range in which an operator can visually observe the unmanned flying body. Upon determining that th...  
WO/2017/021955A1
The presently disclosed subject matter is related to avoidance of violation of a flight constraint by an autonomously controlled aircraft. Responsive to information indicative of a flight constraint, a bank angle which allows the aircraf...  
WO/2017/023954A1
One embodiment of a sanitary airplane seat back barrier system with contiguous material forming a tray table cover [top (30), sides (32), and bottom], and contiguous material to form a seatback pocket protector (20) and seatback cover (2...  
WO/2017/022994A1
The present invention relates to a method for providing various pieces of green information required for putting to a golfer terminal by making information on a green of a golf course into a database in advance, enabling a drone to photo...  
WO/2017/020225A1
The present invention relates to an unmanned helicopter. The unmanned helicopter comprises a fuselage. Two arms are respectively disposed on each of two sides of the fuselage. One end of each arm is connected to the fuselage, and the oth...  
WO/2017/021391A1
The invention relates to a VTOL aircraft (1, 10) having a displaceable mass (9) attached to or fitted in the fuselage (7), and at least two pivotable rotors (3). The rotors (3) are arrangeable in a substantially horizontal position and a...  
WO/2017/021414A1
A display management system 10 is provided for displaying a graphical representation of flight envelope information of an aircraft. Included in the display management system is a control module 20 being coupled to the display management ...  
WO/2017/022178A1
Provided is an unmanned flying body, a flight control method, and a flight control program whereby it is possible to prevent the unmanned flying body from traveling to a place invisible to an operator and to cause the unmanned flying bod...  
WO/2017/022473A1
When a long shaped member is to be held, in order to hold the long shaped member in the original shape of the long shaped member at a precise position without using a jig for immobilization, a long member assembling device (1) is provide...  
WO/2017/021485A1
The invention relates to a vehicle seat, preferably multiple-seater, which is deformable at the centre thereof and makes it possible to respond to deformation stresses in the event of an accident, impact or crash. In the case of a three-...  
WO/2017/023383A1
In one aspect and one example, a liquid fueled pulsed plasma thruster includes an ionic liquid propellant and electrodes disposed to at least partially cause electrolytic decomposition of the ionic liquid propellant. The ionic liquid pro...  

Matches 1 - 50 out of 55,262