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Browse by: INVENTOR PATENT HOLDER PATENT NUMBER DATE
 
 
Inventor:
Gerhardt; Heinz A.
Address:
Redondo Beach, CA
No. of patents:
12
Patents:












Patent Number Title Of Patent Date Issued
D356990 Aircraft April 4, 1995
5992341 Linear motion wind driven power plant November 30, 1999
A linear motion wind driven power plant utilizes a closed-loop track having a plurality of carriages configured to move thereabout. At least one sail is formed to each of the carriages so as to be rotatable 360 degrees of azimuth. At least one electrical power generator generates electri
5984231 Aircraft with variable forward-sweep wing November 16, 1999
An aircraft with a variable forward-sweep wing and the method of configuring the wing in an optimal position for a desired flight regime. The variable forward-sweep wing is positionable from an essentially unswept position to a full-forward sweep position. In the unswept position the
5758911 Linear motion wind driven power plant June 2, 1998
A linear motion wind driven power plant utilizes a closed-loop track having a plurality of carriages configured to move thereabout. At least one sail is formed to each of the carriages so as to be rotatable 360 degrees of azimuth. At least one electrical power generator generates electri
5669308 Linear turbine propulsion system September 23, 1997
Propulsion apparatus for a transportation system vehicle. At least one gas producer is mounted on the vehicle for discharging a propulsive fluid stream. The propulsive fluid stream is directed against at least one longitudinally extending linear turbine assembly to propel the vehicle. A
5542357 Linear turbine propulsion system August 6, 1996
Propulsion apparatus for a transportation system vehicle. At least one gas producer is mounted on the vehicle for discharging a propulsive fluid stream. The propulsive fluid stream is directed against at least one longitudinally extending linear turbine assembly to propel the vehicle. A
5538201 Supersonic natural laminar flow wing July 23, 1996
A reverse delta aerodynamic wing has a basic reverse delta wing portion bounded by a leading edge and by a pair of trailing edges extending from respective ends of said leading edge toward a trailing apex point and respective span-wise wing extensions in a natural laminar boundary layer
5398888 Skewed hinge control surface March 21, 1995
Aerodynamic control apparatus for an aircraft is provided which includes a pair of control surfaces, one for each side of the aircraft, each control surface extending between a root end at the fuselage and a distant tip end. The root end of each control surface is pivotally mounted on th
5265827 Paddle wheel rotorcraft November 30, 1993
An aircraft having vertical takeoff and landing capability having at least first and second laterally extending paddle wheels rotatable on a central axis generally perpendicular to the longitudinal axis of the aircraft and between its nose and tail. Each of the paddle wheels has a plural
5156358 Aircraft outboard control October 20, 1992
An outboard control surface for an aircraft. The control surface is operably connected to wing side edges of the aircraft and includes a forward flap and a rearward flap with at least one of the flaps being movable into and out of alignment with the plane of the wing.
4648571 Transverse thrust lift augmentation system March 10, 1987
Disclosed is a propulsive lift mechanism which improves the short takeoff and landing capabilities of an aircraft by generating transverse thrust lift augmentation by exhausting gasses ported from the main exhaust through a nozzle, close behind and parallel with the trailing edges of the
4181277 Variable span wing January 1, 1980
A variable span wing in which a movable wing segment is externally mounted to slide along the trailing edge of the stationary main wing. The movable wing segment is extended beyond the span of the main wing at subsonic flight and retracted to the same span at supersonic flight. Extension










 
 
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