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WO/2016/066848A1 |
The invention relates to a driving module for a motor vehicle. Said driving module comprises two driving devices with a total of at least three impellers that have rotor blades; at least two of the impellers are coupled to a swiveling me...
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WO/2016/062223A1 |
The present invention relates to a vertical take-off and landing aircraft, comprising a fuselage (1), a main wing, a main thrust apparatus (2) that can tilt between the horizontal position and the vertical position, a tilt apparatus that...
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WO/2016/062921A1 |
An electrically powered vertical takeoff and vertical landing (VTOL) aircraft, which comprises at least two main propellers (101a, 101b), wherein the main propellers are adapted to generate at least 70% of the aircraft propulsion. The ai...
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WO/2016/059555A1 |
An unmanned aerial vehicle (UAV) system provides for UAV deployment and remote, unattended operation with reduced logistics requirements. The system includes a launcher that can include one or more containers, or hangars, configured to h...
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WO/2016/060720A1 |
The Curtis Protocol, a standardized aircraft control interface, e.g. for aircraft with multiple flight regimes and flight modes, is provided. The Curtis Protocol standardizes the division and selection of aircraft flight regimes and flig...
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WO/2016/058502A1 |
Disclosed is a tail-sitter aircraft, comprising an aircraft body (1), an aircraft wing (2), an attitude control device and a main thrust device (3) using a heat engine as a power device, wherein the aircraft wing (2) comprises a left hal...
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WO/2016/059040A1 |
A flying apparatus is provided that comprises a airfoil (1) with a streamlined profile for generating an aerodynamic lift force vector (L) acting on the flying apparatus when being exposed to an apparent air flow. The flying apparatus al...
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WO/2016/047343A1 |
This vertical take-off and landing aircraft (1) is provided with: a fuselage (2); a plurality of engines (3) that are installed on the fuselage and generate jet streams to produce thrust; an abnormality signal-acquiring unit for acquirin...
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WO/2016/037543A1 |
A suction-cup-type aircraft comprises a propulsion device (1) and a venting device (9); the venting device (9) actively drives the air above the upper surface of the propulsion device (1) to flow quickly to produce a negative pressure, o...
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WO/2016/028358A2 |
The present disclosure relates to a high performance Vertical Takeoff and Landing (VTOL) aircraft for executing hovering flight, forward flight, and transitioning between the two in a stable and efficient manner. The VTOL aircraft provid...
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WO/2016/022040A1 |
The proposed technical solution relates to the field of ultralight aviation and allows for increasing the quality of aircraft control during flight. An air-mobile includes a glider, a propulsion system with propellers for vertical tak...
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WO/2016/022011A1 |
The invention relates to aviation equipment An object of this invention is to develop a new aerodynamic device which can extend the range of aerodynamic devices for aviation, increase the efficiency of the air flow power use, increase th...
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WO/2016/016889A1 |
A propulsion system is provided, including a first propulsion unit, a second propulsion unit, a rotor, a first coupling and a second coupling. The first propulsion unit is configured for being fixedly mounted to an airframe. The rotor is...
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WO/2016/018486A2 |
A vertical takeoff and landing aircraft includes a pair of ducted lift/thrust fans that are rotatably movable between a first vertical lift position and a second horizontal thrust position. The lift/thrust fans are disposed within curvil...
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WO/2016/004852A1 |
A vertical take-off and landing aircraft comprises an aircraft body (6), a main thrust device (7) that provides a main thrust for the aircraft, and a posture control device. The posture control device comprises multiple posture alignment...
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WO/2016/007049A1 |
The invention relates to aviation technology, specifically to vertical take-off and landing aircraft. The vertical take-off and landing aircraft comprises two turbines, the lower of which is of plate-like shape, and the upper is of flat ...
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WO/2016/003530A2 |
One example embodiment includes a vertical takeoff and landing (VTOL) unmanned aerial vehicle (UAV). The VTOL UAV includes a flight control system configured to provide avionic control of the VTOL UAV in a hover mode and in a level-fligh...
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WO/2016/000668A1 |
An aircraft with vertical take-off and landing contains a central fan to produce lift by expelling air from the bottom part of the aircraft (1). The fan comprises a rotor (2) driven by the motor (4). In the bottom part of the aircraft (1...
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WO/2015/198200A1 |
A vertical takeoff and landing aircraft includes rotors that provide vertical and horizontal thrust. During forward motion, the vertical lift system is inactive. A lift fan mechanism positions the fan blades of the aircraft in a collapse...
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WO/2015/189684A1 |
The invention relates to a convertible tilt-wing aircraft, including: a fuselage (F), a wing, at least one portion of which can tilt (AB) relative to the fuselage (F) about an axis (A) of rotation substantially perpendicular to the longi...
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WO/2015/191747A1 |
An aerial vehicle capable of convertible flight from hover to linear flight includes a body having a longitudinal body axis, a plurality of forward wings, a plurality of aft wings, at least one motor, and at least three aerodynamic propu...
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WO/2015/187836A1 |
An aerial vehicle includes a body having a center and a number of spatially separated thrusters. The spatially separated thrusters are statically coupled to the body at locations around the center of the body and are configured to emit t...
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WO/2015/159196A1 |
VTOL aircraft with a thrust-to-weight ratio smaller than 0.1, during vertical take-off/landing, obtains another vertical lift, besides traditional vertical lift generated by low-temp bypass duct directing, under the closing of the propel...
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WO/2015/157114A1 |
Modular nacelles to provide vertical takeoff and landing (VTOL) capabilities to fixed-wing aerial vehicles, and associated systems and methods are disclosed. A representative system includes a nacelle, a power source carried by the nacel...
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WO/2015/143684A1 |
Systems，methods，and devices are provided for assisted takeoff of an aerial vehicle．The aerial vehicle may takeoff using a first control scheme and switch to a second control scheme for normal flight when a takeoff threshold is metï...
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WO/2015/145101A1 |
A rotor-lift aircraft has at least two rotors 1, 2 mounted on spaced parallel axes A1, A2. The rotors rotate in use in planes in which the blade envelope subscribed by the tips of the blade(s) of each of the rotors overlaps with the blad...
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WO/2015/143093A2 |
An aerial vehicle adapted for vertical takeoff and landing using a set of wing mounted thrust producing elements and a set of tail mounted rotors for takeoff and landing. An aerial vehicle which is adapted to vertical takeoff with the ro...
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WO/2015/143098A2 |
An aerial vehicle adapted for vertical takeoff and landing using a set of wing mounted thrust producing elements and a set of tail mounted rotors for takeoff and landing. An aerial vehicle which is adapted to vertical takeoff with the ro...
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WO/2015/124556A1 |
The invention relates to an aircraft comprising a fuselage (1), a plurality of propeller units (3) that can pivot in relation to the fuselage (1), and wings (5) that can pivot at least partially in relation to the fuselage (1) and indepe...
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WO/2015/123035A1 |
A camera system and method capture image data with a camera, a data storage device electrically connected to the camera and configured to store the video data and/or a communication device electrically connected to the camera and configu...
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WO/2015/116015A1 |
An inflatable vertical takeoff and landing aircraft intended for individual use, in which lift is generated by a rotor, wherein deflectors which deflect the airflow from said rotor compensate for the reaction torque arising from the rota...
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WO/2015/108578A2 |
A VTOL aircraft includes at least one puller rotor and at least one pusher rotor. The VTOL aircraft, for example, may include three puller rotors and one pusher rotor. The combination of static puller and pusher rotors allows the rotors ...
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WO/2015/105396A1 |
The disclosed flight device according to the present invention comprises a flying flight unit and a control unit for controlling the flight of the flight unit, the flight unit comprising: a frame part in which the control unit is install...
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WO/2015/099603A1 |
An unmanned aerial vehicle (UAV) capable of vertical and horizontal flight modes, a method of assembling a UAV, and a kit of parts for assembling a UAV. The UAV comprises an elongated wing structure having an elongated axis along the lon...
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WO/2015/099375A1 |
The present invention provides a multi-rotor flying object comprising: a body; a plurality of rotor units, each of which comprises a propeller and a power unit for driving the propeller; and a steering unit comprising a connection member...
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WO/2015/094003A1 |
The invention relates to air transport and can be used in aircraft of various designs. The aircraft wing comprises a lifting surface and a turbojet engine (1). The lifting surface is the combination of a conventional aerodynamic wing (3)...
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WO/2015/089679A1 |
A VTOL aircraft comprises a fuselage (10), two main wings (41, 42) which are arranged on both sides of a rear region of the fuselage (10), two propellers (53, 54), wherein in each case one propeller (53, 54) is arranged on each main wing...
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WO/2015/056124A1 |
The present invention relates to a propulsion system for aircraft, comprising: • - a primary propulsion system (PI) for generating horizontal thrust needed for cruise; • - a secondary propulsion system (RAPS) for generating vertical ...
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WO/2015/049798A1 |
A lightweight small flight vehicle (1) that flies by rotation of a rotor (2) is characterized by being equipped with: a rotation prevention blade (5) that generates a torque about a main shaft (100) in a fuselage (10) by receiving by a b...
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WO/2015/043568A1 |
The present invention relates to a drive apparatus which has an engine and a thrust nozzle for generating thrust in a first direction. Furthermore, the engine and the thrust nozzle are connected to one another by a thrust nozzle pipe. Th...
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WO/2015/030630A1 |
Described is a flying apparatus which makes use of the Coanda effect. The apparatus is made in the form of a disk having, provided thereon, a plurality of blades in the shape of wings, said blades being equipped with diffusers which a...
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WO/2015/028627A1 |
The invention relates to an aircraft (1) which can both take off and land vertically and can hover and also fly horizontally at a high cruising speed. The aircraft (1) has a support structure (27), a wing structure (15), at least three a...
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WO/2015/026302A1 |
Vertical Take Off and Landing Unmanned Aerial Vehicle (VTOL UAV) with Twin Yaw Control System (TYCS). TYCS consists of auxiliary rotors (6) which are connected to the main rotor head frame. They acquire rotational forces from a gearbox (...
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WO/2015/022711A1 |
The proposed convertiplane has the ability to take off like a helicopter and then fly horizontally like a conventional aircraft. The aircraft comprises : - a variable incidence front wing of variable span located below the fuselage and m...
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WO/2015/019255A1 |
Boxwing aeroplane (1) comprising a fuselage (20) defining for said boxwing aeroplane (1) a preferred axis of development (1a), a prow (1b) and an ending (1c); a boxwing wing structure (30) comprising front wings (31) suitable to be coupl...
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WO/2015/012935A2 |
A flight control apparatus for fixed-wing aircraft includes a first port wing (115) and first starboard wing (120), a first port swash plate (145) coupled between a first port rotor 155) and first port electric motor (135), the first por...
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WO/2015/005776A1 |
A rotary device comprises a frame with a guide for flowing medium, a rotor with a number of blades, whereby a relation is obtained between the flowing medium and the rotation of the rotor, and energy converting means, the one part of whi...
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WO/2015/004370A1 |
The invention relates to a device which includes two longitudinal deflecting surfaces or two pluralities of longitudinal deflecting surfaces (1), which are symmetrical on either side of the plane formed by the roll and yaw axes of the de...
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WO/2015/000028A1 |
An aerodynamic lifting device comprises a chassis (200); a rotor (120) having a rotational axis (R) and a plurality of rotor blades (123) disposed in an annular ring about the rotational axis (R) supported by the chassis (200); and a tor...
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WO/2014/205419A1 |
The present invention provides lightweight fluid-jet thrust pack which provides three rotational axes and reduced restriction of fluid flow to the output nozzles. A first rotational axis is provided by a first rotatable coupling that is ...
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