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WO/2011/004186 |
In craft of the type in which a fan (2) is used to direct a radial jet of air over a curved canopy (1), the canopy is shaped so as to divert the flow of air from a radial to an axial direction to produce lift. The air flowing from the fa...
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WO/2011/004187 |
A Coanda vehicle comprises a canopy (1) having an upper convex surface (7), an impeller (2, 5), means (1, 3)defining a path for fluid which passes through the impeller and curves from a relatively axial direction to a relatively radial d...
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WO/2011/004186 |
In craft of the type in which a fan (2) is used to direct a radial jet of air over a curved canopy (1), the canopy is shaped so as to divert the flow of air from a radial to an axial direction to produce lift. The air flowing from the fa...
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WO/2011/002331 |
The invention relates to a small unmanned aircraft system for aerial surveillance and reconnaissance, which comprises a ground control station, on-board and ground radio-communication, navigation and flight control means, a launching dev...
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WO/2011/002309 |
A carapaced blended wing-body gliding, flying or airdrop aircraft having rearwardly stowed wings able to assume and/or be caused to assume a flight mode condition, and stowed stabilator components able to assume and/or be caused to assum...
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WO/2011/002517 |
A turbine, mini or micro turbine powered personal flight system configured as a jet pack includes a frame having an aerodynamic shell positioned thereon. At least two turbine, mini or micro turbine powered engines are positioned on oppos...
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WO/2010/143179 |
A sensor/emitter arrangement (M1-M3) is integrated into the fuselage (120) structure of a specially designed air vehicle (100), in which the air vehicle is configured for optimizing operation of the sensor/emitter arrangement (M1-M3) wit...
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WO/2010/137016 |
According to one aspect of the invention there is provided a system and method for providing propulsion and control to an air vehicle, and for operating the vehicle, in which at least three propulsion units provide vertical thrust for ve...
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WO/2010/135604 |
A tethered airborne electrical power generation system which may utilize a strutted frame structure with airfoils built into the frame to keep wind turbine driven generators which are within the structure airborne. The primary rotors uti...
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WO/2010/135727 |
An unmanned, towable aerovehicle is described and includes a container to hold cargo, an autogyro assembly connected to the container and to provide flight characteristics, and a controller to control operation the autogyro assembly for ...
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WO/2010/135727 |
An unmanned, towable aerovehicle is described and includes a container to hold cargo, an autogyro assembly connected to the container and to provide flight characteristics, and a controller to control operation the autogyro assembly for ...
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WO/2010/128489 |
An aerial robotic system comprises an aircraft (4) provided with four rotors (11a, 11b, 11c 11d). The aircraft (4) comprises control means (8) for controlling operating parameters of each of said rotors 11a, 11b, 11c, 11d) independently ...
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WO/2010/128489 |
An aerial robotic system comprises an aircraft (4) provided with four rotors (11a, 11b, 11c 11d). The aircraft (4) comprises control means (8) for controlling operating parameters of each of said rotors 11a, 11b, 11c, 11d) independently ...
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WO/2010/118860 |
The invention relates to a plastic composite component (10) which is formed by a thin hard plastic outer layer (12), at least one elastomer layer (14) adjoining the former on the inside, and at least one metal and/or plastic carrier laye...
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WO/2010/118860 |
The invention relates to a plastic composite component (10) which is formed by a thin hard plastic outer layer (12), at least one elastomer layer (14) adjoining the former on the inside, and at least one metal and/or plastic carrier laye...
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WO/2010/116018 |
Aircraft having a lambda-box wing configuration, comprising a fuselage (1 ), a propulsion system (5), a first pair of swept-back airfoils (2), connected to the top forward portion of the fuselage (1 ), a second pair of swept-forward airf...
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WO/2010/116362 |
A method, system and a floating unit. The floating unit includes a propeller, a frame, a propeller motor that is configured to rotate the propeller about a first axis; wherein the propeller motor is coupled to the frame, a movable steeri...
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WO/2010/116018 |
Aircraft having a lambda-box wing configuration, comprising a fuselage (1 ), a propulsion system (5), a first pair of swept-back airfoils (2), connected to the top forward portion of the fuselage (1 ), a second pair of swept-forward airf...
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WO/2010/106343 |
An electric and hybrid Vertical -Take Off and Landing ("VTOL") aircraft is disclosed comprising a plurality of small Electric Ducted Fans ("EDFs") (201-208, 232-235) of various sizes and orientations. The thrust of each fixed EDF (201-20...
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WO/2010/100436 |
A gust-insensitive unmanned air vehicle (UAV) for imaging the ground, the UAV comprising: an airframe which is substantially neutrally stable and comprises a fuselage and at least three wings which include control surfaces, wherein the w...
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WO/2010/100374 |
The invention relates to a method for airborne commuting secured by a teleporting aircraft. The method is characterised in that it involves selecting said teleporting aircraft (1) provided with a flexible airfoil (2) and adapted for take...
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WO/2010/099730 |
An amphibious large aircraft without airstairs is provided. The fuselage (7) of the amphibious large aircraft is flat，and the shape of its bottom is rectangular. The longitudinal cross-section of the fuselage has a shape of the cross-s...
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WO/2010/092253 |
The invention relates to an aerodyne (10) comprising a lift propeller (84), a fairing (14) surrounding the propeller, and an electric motor (26) for rotating the propeller relative to the fairing. The aerodyne also comprises a landing ge...
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WO/2010/070631 |
The present invention relates to an unmanned air vehicle (105), comprising a body having front (121) and rear (122) sections with at least one pair of end plates (110) connected to said body, wherein one end plate within said at least on...
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WO/2010/064548 |
The unmanned aircraft is equipped with a camera, a laser ranging system, and a drive unit. The laser ranging system measures the distance to an object in the camera field of view. The drive unit rotates the field of view. Information on ...
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WO/2010/064326 |
Disclosed is an automobile capable of traveling and flying. A conventional automobile having a flying function is hard to take off and land on a road, because the width and the height thereof are large. The width and the height of an aut...
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WO/2010/064886 |
The present invention relates to an improved encased square aerodynamic wing, the structure of which incorporates the vertical stabilizers and aerodynamic brake, offering the special feature of reducing wing resistance and providing bett...
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WO/2010/061071 |
The invention relates to a nacelle (23) for a turbojet engine (21), comprising an air intake structure (25) capable of directing an air flow towards a fan (27) of a turbojet engine (21), a middle structure (29) for surrounding said fan (...
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WO/2010/061071 |
The invention relates to a nacelle (23) for a turbojet engine (21), comprising an air intake structure (25) capable of directing an air flow towards a fan (27) of a turbojet engine (21), a middle structure (29) for surrounding said fan (...
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WO/2010/061070 |
The invention relates to a flying wing (3) that comprises two side wings (5, 7), a central body (9), and at least one propulsion assembly (20) including a turbojet engine (21) surrounded by a nacelle (23), characterised in that the propu...
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WO/2010/050839 |
The invention relates to aviation, in particular to aircraft, and can be used for transporting cargo and passengers, spraying gardens and fields, conserving forests and nature reserves and as an ambulance in difficult-to-reach regions. T...
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WO/2010/049647 |
The invention relates to an automatic takeoff method for an aircraft with a flexible airfoil, comprising a carriage suspended by rigging lines from an airfoil. According to said method: - said carriage is provided with an autopilot contr...
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WO/2010/027801 |
A morphing aircraft that is achieves multi- modality location and camouflage for payload emplacement The morphing aircraft includes a substantially cylindrical fuselage including a shape configured as a packaging container with a first e...
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WO/2010/027801 |
A morphing aircraft that is achieves multi- modality location and camouflage for payload emplacement The morphing aircraft includes a substantially cylindrical fuselage including a shape configured as a packaging container with a first e...
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WO/2010/024525 |
The present invention discloses one or more flying objects of which a reference path is set up, based on one or more reference locations, which fly according to the reference path around the reference location by detecting the distance b...
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WO/2010/024726 |
The group of inventions relates to the field of apparatuses for travel in an air and water medium. The apparatus for travel in a fluid medium comprises a blade with an aerodynamic section with an upper convex surface, and a source of hig...
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WO/2010/024525 |
The present invention discloses one or more flying objects of which a reference path is set up, based on one or more reference locations, which fly according to the reference path around the reference location by detecting the distance b...
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WO/2010/016796 |
It is an object of the present invention to provide a termination system allowing an unmanned vehicle to be remotely terminated in a safe and cost efficient manner. The object is achieved by a termination system (1; 1A; 1 B) based on the...
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WO/2010/009434 |
A power generation system (20) including an airborne electricity generator (30), a tether assembly (40) configured to carry electricity from the generator to land, the tether assembly having a first end portion (42) coupled to the genera...
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WO/2010/001147 |
The thrust vectoring apparatus comprises: a housing defining a primary outlet for emitting the primary jet; Coanda surfaces extending from opposing regions of said housing, and radially spaced from the primary outlet such that a step is ...
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WO/2009/157781 |
A personal flight device including : a housing securable to the pilot; at least one pair of ducted fans, one fan of each pair mounted to each side of the housing; wherein each fan rotates about an axis of rotation to draw air through the...
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WO/2009/157780 |
A personal flight device which includes: a housing which is securable to a pilot; at least one pair of ducted fans, one fan of the pair mounted to one side of the housing, the other fan of the pair mounted to the other side of the housin...
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WO/2009/153588 |
A UAV having an airframe supporting a tri-rotor triangular array, each tri-rotor comprising a pair of rotors (21,23) on the same axis, withan individual motor (20,22) for each rotor, the pairs of rotors being arrangedto contra-rotate.
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WO/2009/150364 |
The invention relates to a device comprising a base (1) for receiving a load, connected to two side supporting elements (2) supported by the medium and formed by two hinged assemblies (3) including a swivel lever (31) with two arms (31a,...
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WO/2009/150478 |
The new method used with the new aircraft for forest fire extinguishing is a concept which consists of a new means by which the new method of fire extinction, especially forested areas, will be applied and consists of an aircraft that wi...
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WO/2009/150478 |
The new method used with the new aircraft for forest fire extinguishing is a concept which consists of a new means by which the new method of fire extinction, especially forested areas, will be applied and consists of an aircraft that wi...
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WO/2009/146084 |
A sliding-arm whirling wheel thruster includes first and second whirling wheels and a housing. The first whirling wheel is disposed about a first rotational axis, and the second whirling wheel about a second rotational axis parallel to t...
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WO/2009/146084 |
A sliding-arm whirling wheel thruster includes first and second whirling wheels and a housing. The first whirling wheel is disposed about a first rotational axis, and the second whirling wheel about a second rotational axis parallel to t...
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WO/2009/135468 |
The invention relates to a propeller device comprising a flow profile body that is associated with a propeller and a multiple eccentric cam arrangement that is functionally coupled to the flow profile body, said arrangement having two ec...
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WO/2009/135260 |
A fluid dynamic device (100) for directing fluid flow to generate thrust comprising a thrust control shroud (130) disposed about a central axis (210) of said fluid dynamic device (100) for directing a fluid flow between an upstream fluid...
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