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| Number | Title | Issue Date |
| 8104707 | X-vane configuration in a ducted-fan aerial vehicle Disclosed herein is a propulsion system, which may be implemented in an air-vehicle, such as a ducted-fan organic air-vehicle. The propulsion system comprises (a) a power source, (b) a fan located within a duct and powered by the power source, (c) a plurality of van... | 01/31/2012 |
| 7971823 | Saucer shaped gyroscopically stabilized vertical take-off and landing aircraft An aircraft that is housed within a gyroscope providing for improved flight stability that includes an inner hull which remains stationary within a rotating outer hull. A rotating sine-wave ring is used to activate and move a plurality of pistons which will intake a... | 07/05/2011 |
| 7857256 | Thrust generating apparatus There have been past proposals for air vehicles employing the Coanda effect. In these proposals, a jet of fluid, usually air, is made to flow radially outwardly over 5 a dome-shaped canopy to create lift. A cross-section through the canopy is curved to follow a segm... | 12/28/2010 |
| 7712701 | Unmanned aerial vehicle with electrically powered, counterrotating ducted rotors An unmanned aerial vehicle having counterrotating ducted rotors that are driven by electric motors. The vehicle has a low weight and a small profile. The unmanned aerial vehicle is suitable for a number of different tasks, including control, surveillance and reconna... | 05/11/2010 |
| 7410123 | Aircraft and hybrid with magnetic airfoil suspension and drive An aircraft is disclosed that comprises a fuselage with first and second wings non-rotatably secured to and extending from sides of the fuselage. Inner and outer tracks are secured to and encircle the fuselage, and airfoils are operably secured between the inner and... | 08/12/2008 |
| 7407132 | Method of steering aircraft by moving the stagnation point and aircraft using the method An aircraft which includes elements providing air circulation and directing the circulation along a housing. Different operational stages of the aircraft such as take off and level flight are achieved by using the same functionally inter-connected elements. The circ... | 08/05/2008 |
| 7364114 | Aircraft The present invention concerns an aircraft having a plurality of lifting and thrust rotors, with an electric motor and an inverter for each motor. In order to provide an aircraft having a greater payload, connecting bars are provided between the motors. In that resp... | 04/29/2008 |
| 7294036 | Flying disc A circular planform wing includes a contiguous thin central plate having top and bottom surfaces. An outer annular rim encompasses the central plate. The rim has a lower edge defining a lower plane of the wing, and the central plate has an upper zone defining an upp... | 11/13/2007 |
| 7273195 | Vertical lift craft A vertical lift craft includes a vertical lift craft, a powered rotor system including two counter-rotating lift rotors rotatably mounted to the body and a cage fixed to the body and extending about the powered rotor system, the cage including flexible rods extendin... | 09/25/2007 |
| 7267299 | Aircraft An aircraft includes a fuselage with a circular airfoil body supported thereabove on a vertical drive shaft mechanism. The airfoil body includes an upper disk forming an upper surface of the body and a lower disk forming a lower surface of the body in which the uppe... | 09/11/2007 |
| 7267300 | Aircraft capable of vertical and short take-off and landing Aircraft comprising an airframe having a forward end, an aft end opposite the forward end, a top extending between the forward end and the aft end, and a bottom opposite the top side. The aircraft further includes a power plant mounted on the airframe. In addition, ... | 09/11/2007 |
| 7255623 | Self-stabilizing rotating toy A rotating toy may then include a hub having a central axis and a lower portion; a plurality of counter rotating blades extending outwardly from the lower portion of the hub, the plurality of counter rotating blades having a tip connected to an outer ring; a single ... | 08/14/2007 |
| 7252265 | Microaircraft and cellular phone equipped with microaircraft An aircraft which is attachable to, for example, a cellular phone. The aircraft is provided with at least four rotors actuated with compressed fluid or by ring-shaped electric motors. ... | 08/07/2007 |
| 7249732 | Aerodynamically stable, VTOL aircraft A hover aircraft employs an air impeller engine having an air channel duct and a rotor with outer ends of its blades fixed to an annular impeller disk that is driven by magnetic induction elements arrayed in the air channel duct. The air-impeller engine is arranged ... | 07/31/2007 |
| 7201346 | Circular fixed wing VTOL aircraft A VTOL aircraft includes a wing, a propulsion system, and an air dam. The propulsion system is located in a central void formed in the wing to cause air flow from an outer perimeter of the wing over the wing and down through the void to generate lift. The air dam is... | 04/10/2007 |
| 7195208 | Multi-device controller for model aircraft Control system for radio-controlled aircraft. The control system includes a control master for simultaneously controlling a group of flight control means, for example, a group of ailerons. A control bar is slidably mounted in the control master and connected to a se... | 03/27/2007 |
| 7185848 | Mass transfer system for stabilizing an airship and other vehicles subject to pitch and roll moments The invention relates to a mechanism to control the pitch and/or roll and/or center of gravity of a vehicle. The first embodiment is a track-based mass transfer system in which pathways are positioned along or radially terminate at a central horizontal plane of the ... | 03/06/2007 |
| 7147640 | External fixator Bone fixators for securing and/or repairing fractures and/or other defects of a distal radius and wrist. The bone fixators may include, among others, (1) a distal mounting element configured to be mounted in a metacarpal bone, or other hand bone, (2) a proximal moun... | 12/12/2006 |
| 7147183 | Lift system for an aerial crane and propulsion system for a vehicle The present invention provides an improved lift system for an aerial crane incorporating a wing, coanda and curved surface. The arrangement of the wing, coanda and curved surface use and induce airflow to create additional lift through an increase in airflow mass, d... | 12/12/2006 |
| 7108228 | Hydrogen-fueled spacecraft A spacecraft having facilities for carrying astronauts and payloads into the earth satellite orbit and space having a composite fiber body with a Kevlar exterior skin. Said craft having a substantially round shape with a portion covered with solar cells. Said solar ... | 09/19/2006 |
| 7077358 | Helicopter with torque-correcting thruster device A helicopter having a torque-correcting thruster device. The helicopter has an aerodynamic body which has opposite side portions, a top portion and a bottom portion. The aerodynamic body has a cockpit and a pilot seat in the cockpit. The helicopter includes landing ... | 07/18/2006 |
| 7044422 | Gyrostabilized self propelled aircraft An unmanned air vehicle comprises a fuselage that defines aerodynamic flight surfaces, an engine mounted to the fuselage having an engine shaft arranged to rotate about a longitudinal axis with respect to the fuselage, and a propeller mounted to the engine shaft so ... | 05/16/2006 |
| 7032859 | Counter rotating ducted fan having a permanent magnet drive A counter rotating ducted fan having a permanent magnet drive. comprising a ducted housing having an iron core stator and a pair of counter rotating propeller blades rotationally mounted on a propeller shaft positioned axially within the housing Each of the propelle... | 04/25/2006 |
| 7032861 | Quiet vertical takeoff and landing aircraft using ducted, magnetic induction air-impeller rotors A hover aircraft employs an air impeller engine having an air channel duct and a rotor with outer ends of its blades fixed to an annular impeller disk that is driven by magnetic induction elements arrayed in the air channel duct. The air-impeller engine is arranged ... | 04/25/2006 |
| 6969027 | Vertical takeoff and landing apparatus A vertical takeoff and landing apparatus is excellent in the maneuverability and postural stability of its airframe, serves to protect a pilot from an impact when landing, and can make extremely stable flight when hovering near a building. An airframe has a propulsi... | 11/29/2005 |
| 6932296 | Cycloidal VTOL UAV A system and method for moving an aerial vehicle along a flight path includes rotatable hubs mounted on opposite sides of the vehicle. Elongated airfoils are mounted on the hubs parallel to a common hub axis for rotation about the hub axis on a blade path. Each airf... | 08/23/2005 |
| 6899586 | Self-stabilizing rotating toy A rotating toy may then include a hub having a central axis and a lower portion; a plurality of counter rotating blades extending outwardly from the lower portion of the hub, the plurality of counter rotating blades having a tip connected to an outer ring; a single ... | 05/31/2005 |
| 6843699 | Flying toy A rotating toy may then include a hub having a central axis and a lower portion; a plurality of counter rotating blades extending outwardly from the lower portion of the hub, the plurality of counter rotating blades having a tip connected to an outer ring; a single ... | 01/18/2005 |
| 6708920 | Air vehicle Disclosed is an air vehicle (Z) comprising a vehicle body (1); hollow fan ducts (3A-3D) supported to and elongating through the vehicle body at least at its foreside and rear-side locations, respectively. Each fan duct communicates with air at t... | 03/23/2004 |
| 6698685 | Circular vertical take off and landing aircraft A circular VTOL aircraft with a central vertically mounted jet or rocket engine 7, (or engines) having below vertical thrust vents 14 at cardinal points, together with a jet/rocket engine 20 (or engines) horizontally mounted on turntable pod 16 which is s... | 03/02/2004 |
| 6672539 | Power generation system A power generation system comprises an internal housing. The housing has a top portion, a bottom portion and a peripheral sidewall. An external housing is provided. The housing is coupled to and receives the internal housing. The housing has an upper lip,... | 01/06/2004 |
| 6666404 | Tripodal modular unmanned rotorcraft Conventional rotorcraft are required to provide a significant amount of anti-torque movement to offset the torque created by the rotor and the right-angle gearbox coupling the rotor to the engine. By vertically integrating the engine in the unmanned rotor... | 12/23/2003 |
| 6666403 | Force-producing apparatus A force-generating device employing a flared body and a surrounding shroud to define a duct of axially diminishing flow area defining a nozzle for accelerating and directing the discharge of a fluid at a cambered vane, a pressure dam depends from the bott... | 12/23/2003 |
| 6588701 | Unmanned mobile device A remotely-controlled unmanned mobile device (UMD) adapted to function as a robot scout to enter and reconnoiter the site of a disaster and to communicate to a rescue mission information regarding conditions prevailing at the site, making it possible for ... | 07/08/2003 |
| 6581872 | Circular vertical take off & landing aircraft A circular VTOL aircraft with a central vertically mounted turboprop engine (14), driving contra-rotating co-axial propellers (24), above a central jet engine, or engines (12), horizontally mounted on a turntable pod (11) which is steerable through 360 de... | 06/24/2003 |
| 6575401 | Vertical-lift and horizontal flight aircraft A vertical-lift and horizontal flight aircraft, which can be operated in a horizontal flight mode, as soon as ground clearance is made. And, because of its unique design is very stable in flight, is very light, has a low drag resistance factor and is vers... | 06/10/2003 |
| 6575402 | Cooling system for a hybrid aircraft A cooling system for a hybrid aircraft includes an inlet which extends through the body to communicate airflow to a powerplant subsystem and out through an exhaust within a rotor duct. In a hover mode, there is a significant low-pressure area created insi... | 06/10/2003 |
| 6572053 | Flying vehicle of inverse sustentation (FVIS) The Flying Vehicle of Inverse Sustentation (FVIS) is an air transport unit for passengers and cargo. The vehicle comprises a main flow generating unit to burn a mixture of fuel and air and produce a gas flow with an appropriate speed to achieve the force ... | 06/03/2003 |
| 6565038 | Supersonic propellers for aircrafts The present invention provides one pair or two pairs of horizontal propellers incorporated on the two opposite sides of an aircraft, which propellers by their rotating external blades create through their frontal shell opening a very strong frontal depres... | 05/20/2003 |
| 6561456 | Vertical/short take-off and landing aircraft An aircraft is provided having a fuselage and a pair of main wings. Each main wing includes a lift fan segment, a generally circular duct defined within the lift fan segment and a fan mounted within the duct. A tip extender is coupled with the tip of at l... | 05/13/2003 |