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7624732 |
Method and apparatus for extending flight crew's time of useful consciousness after decompression
Systems and methods are provided for regulating the pressure within an aircraft flight crew area during and/or after a decompression event. For example, an aircraft may include a flight crew area,...
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7445180 |
Actuation system for tail section of aircraft
The invention is directed to an actuation system in an aircraft comprising a fuselage and a hinged tail section with at least one interlock component that engages a tail support, wherein the...
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7367530 |
Aerospace vehicle yaw generating systems and associated methods
Aerospace vehicle yaw generating systems and associated methods are disclosed herein. One aspect of the invention is directed toward a yaw generating system that can include an aerospace vehicle...
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7278609 |
Movable nose cap and control strut assembly for supersonic aircraft
A nose cap and control strut assembly for supersonic aircraft is disclosed. In one embodiment, the nose cap extends forward from the nose of the aircraft to deflect shock waves and decrease draft...
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7185859 |
***WITHDRAWN PATENT AS PER THE LATEST USPTO WITHDRAWN LIST***
Aerospace vehicle yaw generating systems and associated methods
Aerospace vehicle yaw generating systems and associated methods are disclosed herein. One aspect of the invention is directed toward a yaw generating system that can include an aerospace vehicle...
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7070144 |
Aircraft and missile afterbody flow control device and method of controlling flow
The present invention relates to an afterbody flow control system and more particularly to aircraft or missile flow control system for enhanced maneuverability and stabilization. The present...
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7048234 |
Adaptive flap and slat drive system for aircraft
A drive station includes two drives connected via drive transmissions to one or more flaps or slats of a flap/slat group. The drives may be mechanically coupled to a rotational shaft, with a shaft...
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6283407 |
Fuselage nose for controlling aerodynamic vehicles and method of utilizing same
A control system for aerodynamic vehicles has a fuselage nose segment and at least one strake. The fuselage nose segment is rotationally adjustable with respect to the aircraft fuselage. The at...
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5927645 |
Shovel nose pneumatic vortex control
A system for facilitating the enhanced aerodynamic control of an aircraft having a fuselage including a forebody defining a frontal portion adapted to create a primary vortex under certain flight...
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5901929 |
Control and augmentation of passive porosity through transpiration control
A device for controlling pressure loading of a member caused by a fluid moving past the member or the member moving through a fluid. The device consists of a porous skin mounted over the solid...
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5794887 |
Stagnation point vortex controller
Means are described for controlling the asymmetry of the leeside vortices developing over a pointed object placed at an angle of attack in a flowing fluid. Unlike prior art, the stagnation point...
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5564652 |
Body spoiler for yaw control of a supersonic airplane
A body spoiler rotatably mounted within a recess formed within opposite sides of the forebody of a supersonic air vehicle and configured to conform with the fuselage of the vehicle. A sensor...
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5326050 |
Aerodynamic surface distension system for high angle of attack forebody vortex control
A deployable system for assisting flight control under certain flight conditions, such as at high angles of attack, whereby two inflatable membranes are located on the forebody portion of an...
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5209430 |
Helicopter low-speed yaw control
A system for improving yaw control at low speeds consists of one strake placed on the upper portion of the fuselage facing the retreating rotor blade and another strake placed on the lower portion...
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5201829 |
Flight control device to provide directional control
An airplane has a control device for providing a directional moment to control yaw during high angles of attack. The control device includes a chine support member carried at the forward end of the...
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5186117 |
Submarine steering apparatus and method
A submarine is steered by means of a special bow assembly. The submarine has a body formed with a contoured surface and a forward portion forming a bow. The assembly comprises an annular member...
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5050819 |
Rotatable non-circular forebody flow controller
The invention is a rotatable, non-circular forebody flow controller. The apparatus comprises a small geometric device located at a nose of a forebody of an aircraft or missile. The geometric device...
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4917333 |
Actuated forebody strakes
Actuated forebody strakes provide yaw control at high angles of attack. In one embodiment, the strakes are axially slidable in the forebody to be deployed out of slots provided for the strakes in...
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4869443 |
Method of extending the performance of a specific jet aircraft
A method of extending the maneuver, performance and flight safety of a specific fighter aircraft, namely, the F-16, is disclosed. In accordance with the method, a portion of the forebody strakes on...
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4786009 |
Yaw and pitch control of air vehicles at high angles of attack
Method and apparatus for controlling the yaw and pitch of air vehicles at high angles of attack by controlling the vortex pattern around the forebodies of the air vehicles by means of deflecting...
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4501397 |
Method of stabilizing flight of a flying body and flight-stabilized flying body
A method of stabilizing flight of a flying body having a circular cross-section by the use of a plurality of tripping wires, when the flying body flies in an air current at a high angle of attack...
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3069112 |
Radome
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