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US20070194171 |
ROCKET-POWERED VEHICLE RACING INFORMATION SYSTEM
A rocket-powered race for entertaining spectators wherein computer-generated images are optionally provided to at-least partially define a race-course. |
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US20050017125 |
Kite and assembly connector
The present invention provides for a connector used in a kite, including two or more legs with a first end and a second end, and a junction portion coupled adjacent the first end of the two or... |
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US20080187785 |
Fuel system for an aircraft including a fuel tank inerting system
A fuel system for an aircraft is disclosed. The fuel system comprises a fuel tank and a fuel reformer for receiving fuel from the fuel tank. The system includes a hydrogen fuel cell array for... |
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US20050023410 |
Multipurpose airfoil assembly
The present disclosure describes a multipurpose airfoil assembly including a body, at least one pair of wings, and a control system. The body provides a structural connection for the wings. At... |
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US20070200029 |
Hydraulic cycloidal control system
A cycloidal propulsion unit for controlling a thrust vector includes a hub that rotates about a hub axis. Further, the unit includes an airfoil blade pivotally mounted on the hub along a blade... |
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US20050116087 |
Aircraft converts drag to lift
An aircraft that has a fuselage that has a majority of its frontal surface areas that strike air angled to deflect air down and cause an upward lift on said fuselage and a propulsion means... |
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US20050045764 |
Canard position and dihedral for boom reduction and pitch/directional control
A supersonic aircraft comprises the fuselage extending forward and aft along a longitudinal axis, a wing coupled to the fuselage, and a canard. The canard is coupled onto the fuselage forward of... |
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US20160023760 |
SYSTEMS AND METHODS COUNTERING AN UNMANNED AIR VEHICLE
Systems and methods for countering an unmanned air vehicle are disclosed. Representative methods include directing an interceptor UAV toward a target UAV, and directing the interceptor UAV back to... |