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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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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/2009/134513 |
An aircraft (10) has a flight termination system (12) that allows flight of an unmanned aircraft to be quickly and efficiently terminated. The flight termination system separates one of the control surfaces (20) of the aircraft, such as ...
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WO/2009/134513 |
An aircraft (10) has a flight termination system (12) that allows flight of an unmanned aircraft to be quickly and efficiently terminated. The flight termination system separates one of the control surfaces (20) of the aircraft, such as ...
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WO/2009/126469 |
A flying vehicle in accordance to an embodiment of the present invention includes a propeller control mechanism for flying the vehicle. The propeller control mechanism includes a propeller having a center shaft for connecting to the driv...
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WO/2009/113914 |
The invention relates to aircraft building, rocket building, shipbuilding, and power machine building, in particular to methods and devices using a wing which is placed in a flow and moves therein (a propeller blade, a screw propeller bl...
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WO/2009/109918 |
A cycloidal rotor system having airfoil blades travelling along a generally non-circular, elongated and, in most embodiments, dynamically variable orbit. Such non-circular orbit provides a greater period in each revolution and an optimiz...
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WO/2009/109918 |
A cycloidal rotor system having airfoil blades travelling along a generally non-circular, elongated and, in most embodiments, dynamically variable orbit. Such non-circular orbit provides a greater period in each revolution and an optimiz...
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WO/2009/109918 |
A cycloidal rotor system having airfoil blades travelling along a generally non-circular, elongated and, in most embodiments, dynamically variable orbit. Such non-circular orbit provides a greater period in each revolution and an optimiz...
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WO/2009/105160 |
Systems, method, devices and apparatus are provided for reducing drag and increasing the flight efficiency characteristics of aircraft and airships including hybrid aircraft utilizing distributed boundary layer control and propulsion mea...
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WO/2009/097846 |
Thrust or carrying force generates a tubular fluid jet, which is created in that a fluid after radial acceleration in a disk-shaped driven rotor (11) mixes with another fluid (28, 32) in the peripherally disposed annular chamber (20) bef...
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WO/2009/095696 |
A VTOL flying-wing aircraft has a pair of thrust-vectoring propulsion units (2, 3; 4, 5) mounted fore and aft of the aircraft pitch axis (PA) on strakes (6, 7) at opposite extremities of the wing-structure (1), with the fore unit (2; 4) ...
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WO/2009/095696 |
A VTOL flying-wing aircraft has a pair of thrust-vectoring propulsion units (2, 3; 4, 5) mounted fore and aft of the aircraft pitch axis (PA) on strakes (6, 7) at opposite extremities of the wing-structure (1), with the fore unit (2; 4) ...
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WO/2009/085021 |
The Spring flying device (1) preferably of circular, oval or polygon shape, capable of vertical take-off and landing, comprises the source (5) of flowing medium (6), which flows through chamber (2) consisting of curved bottom face genera...
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WO/2009/085021 |
The Spring flying device (1) preferably of circular, oval or polygon shape, capable of vertical take-off and landing, comprises the source (5) of flowing medium (6), which flows through chamber (2) consisting of curved bottom face genera...
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WO/2009/077504 |
The invention relates to a device (1) for permanently maintaining the altitude of a payload having an altitude-maintenance energy source that is practically permanent and extracted from the surrounding medium. The device is cheap to buil...
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WO/2009/071755 |
The present invention relates to a modular drone (1) consisting of a flying structure (2) and image acquisition means, characterized in that said image acquisition means as well as the motorization are supported by a rigid platen (6) con...
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WO/2009/068835 |
A static wing (1) comprises a ring portion (2) having an aerofoil shaped cross section. Positioned above the centre aperture of the ring portion (2) is a diffuser plate (3), the diffuser plate is optionally arranged to be moveable vertic...
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WO/2009/066073 |
An unmanned aerial vehicle (UAV) (1) in the form of a "tail sitter" flying wing (1) adapted for vertical take off and landing and transitions between flight as a helicopter and wing-borne flight. The vehicle is electrically powered from ...
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WO/2009/061540 |
According to one embodiment of the disclosure, an unmanned vehicle message conversion system generally includes a message interpreter that is coupled between a first unmanned vehicle control interface and a second unmanned vehicle contro...
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WO/2009/058475 |
According to one embodiment, code embodied in a computer readable storage medium is configured to generate a checklist for a vehicle by receiving a measured value obtained from at least one sensor configured on the vehicle, setting a par...
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WO/2009/054015 |
Herewith is presented and described the adaptation of existing manned helicopters used for firefighting or other purposes for use as remote-controlled helicopters commanded by wire or radio and equipped with water hydrant with sufficient...
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WO/2009/048666 |
The invention is a method for launching and recovering a child aircraft, manned or unmanned, as well as providing a method for continuous flight to and from a parent aircraft, manned or unmanned, from a pylon that is mounted externally o...
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WO/2009/046503 |
Method to decrease the turnaround time of aircraft, whereby if an airplane (7) is to carry passengers (10) or a combination of passengers (10) and cargo, the airplane (7) contains at least one passenger module (1) provided with seats (2)...
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WO/2009/041922 |
The invention subject is an plane wing in the shape of a ring, that can be inflated. The plane wing in the shape of a ring after invention, which shape and setup is shown in picture 1, can be set up as a carrying wing 2 and attached to f...
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WO/2009/041922 |
The invention subject is an plane wing in the shape of a ring, that can be inflated. The plane wing in the shape of a ring after invention, which shape and setup is shown in picture 1, can be set up as a carrying wing 2 and attached to f...
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WO/2009/034805 |
Provided is a positive-pressure floating type airplane (10) comprising an airfoil portion (12), left-right fuselages (30A and 30B), a central fuselage (40), an elevator (50) and a rudder (52) disposed at the back of the airfoil portion (...
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WO/2009/032027 |
A harness with mounted engine frame comprises a harness to be worn by a user. An engine support arm is mounted on the harness and a pair of lateral arms extend from the engine support arm. At least one engine is associated with each late...
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WO/2009/027742 |
In a vertical-take-off air vehicle, a rotary impeller (3) causes air to flow over convex outer surfaces (1) to create lift. In accordance with the invention air is also caused to flow under one or more outer surfaces (5) at a selected ci...
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WO/2009/024101 |
Aircraft, using wall jet to generate a lift, contains a rotor (3) located on the fuselage (2) of the aircraft (1) and circumferential or discontinued ring (4) surrounding the rotor (3), whereas there is an outlet gap (5) between the lowe...
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WO/2009/025632 |
The inventive vertical-takeoff-and-landing aircraft is used for transporting passengers and cargo and makes it possible to increase the powerplant performance and to improve aerodynamic and operational characteristics thereof. Said verti...
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WO/2009/024101 |
Aircraft, using wall jet to generate a lift, contains a rotor (3) located on the fuselage (2) of the aircraft (1) and circumferential or discontinued ring (4) surrounding the rotor (3), whereas there is an outlet gap (5) between the lowe...
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WO/2009/022889 |
The present invention concerns a new airship wherein are installed infrared cameras and radars for monitoring urban zones and conduits for gas or petroleum derivatives, for detection of leaks, and also for checking of the same; also for ...
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WO/2009/005875 |
This disclosure involves aerial robots (1) that dispense conductive filament (110) or systems, methods, and software for supporting such aerial robots (1). One remotely powered aerial robot system includes an aerial robot (1) and a power...
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WO/2009/005875 |
This disclosure involves aerial robots (1) that dispense conductive filament (110) or systems, methods, and software for supporting such aerial robots (1). One remotely powered aerial robot system includes an aerial robot (1) and a power...
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WO/2009/002279 |
A sequential wing construction for airplanes or wind turbines rotors. The wing comprises independent blades (5) rotably located on girders (1) of circular cross-section, which create, along with sideward positioned aerodynamic traverses ...
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WO/2009/002279 |
A sequential wing construction for airplanes or wind turbines rotors. The wing comprises independent blades (5) rotably located on girders (1) of circular cross-section, which create, along with sideward positioned aerodynamic traverses ...
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WO/2008/140502 |
A method is provided for producing an arthropod comprising introducing a microsystem such as a MEMS device into an immature arthropod under conditions that result in producing an adult arthropod with a functional microsystem permanently ...
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WO/2008/138972 |
The invention relates to a helicopter (10, 48, 76) comprising at least one rotor (12, 68, 70), a drive that can be driven by the rotor, and a cabin (22, 50) that receives a load, for example a person. The at least one rotor is cardanical...
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WO/2008/129244 |
An airborne vehicle (1) having a wing-body (2) which defines a wing-body axis (3) and appears substantially annular when viewed along the wing-body axis, the interior of the annulus defining a duct (5) which is open at both ends. A propu...
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WO/2008/129244 |
An airborne vehicle (1) having a wing-body (2) which defines a wing-body axis (3) and appears substantially annular when viewed along the wing-body axis, the interior of the annulus defining a duct (5) which is open at both ends. A propu...
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WO/2008/127792 |
An unmanned aerial vehicle (UAV) is designed for low-speed, low altitude, long endurance missions typical to UAVs of this size and class. The UAV structure is configured to be substantially impervious to small arms fire and to have a ver...
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WO/2008/127792 |
An unmanned aerial vehicle (UAV) is designed for low-speed, low altitude, long endurance missions typical to UAVs of this size and class. The UAV structure is configured to be substantially impervious to small arms fire and to have a ver...
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WO/2008/121774 |
A solar thermal powered aircraft (100) powered by heat energy from the sun. A Rankine-Bray ton hybrid cycle heat engine (140) is carried by the aircraft body for producing power for a propulsion mechanism, such as a propeller (109) or ot...
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WO/2008/119246 |
A flying saucer is provided with a fuselage (22), a controlling system, an electrical system, interior instruments, a fuel system, a startup system and an ignition system. On the fuselage (22) is mounted with a moving direction adjusting...
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WO/2008/121774 |
A solar thermal powered aircraft (100) powered by heat energy from the sun. A Rankine-Bray ton hybrid cycle heat engine (140) is carried by the aircraft body for producing power for a propulsion mechanism, such as a propeller (109) or ot...
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WO/2008/105899 |
A trajectory control system includes a first control mechanism having a pair of outputs operably associated with a first pair of control surfaces, the first control mechanism operable to articulate the first pair of control surfaces in u...
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WO/2008/099192 |
An aerial vehicle comprising an aerofoil (2), a generally forward facing propeller (10), a drive motor (6) arranged to drive the propeller about a drive axis to generate thrust, and mounting means (32) on which the propeller is pivotably...
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WO/2008/094075 |
The invention relates to astronautics and can be used for flying in the atmosphere of the Earth, in space and in other media. The inventive method consists in generating lift by rotating a disk with the aid of jet engines at a speed of r...
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WO/2008/083636 |
The invention relates a flying device with at least one propulsion unit in an oval body shape, which that the propulsion unit consists of a closed chamber (1), with gas in this space with lower pressure than the air pressure, containing ...
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