Saucer shaped gyroscopically stabilized vertical take-off...

Details Saucer shaped gyroscopically stabilized vertical take-off... Saucer shaped gyroscopically stabilized vertical take-off...

2011-07-05

2011-07-05

Eldred, J. W (Department: 3641)

Aeronautics and astronautics

Aircraft, heavier-than-air

Fluid sustained

C244S008000, C244S012200, C244S039000

Reexamination Certificate

active

07971823

ABSTRACT:
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 air from above the upper surface of the inner hull configuration and create a negative pressure on the aircraft. The craft contains compression chambers which receive the air and which feed the various impeller thrusters which are rotational within three-fourths of a hemisphere.

REFERENCES:
patent: 4807830 (1989-02-01), Horton
patent: 5259571 (1993-11-01), Blazquez
patent: 6050520 (2000-04-01), Kirla
patent: 6837457 (2005-01-01), Kirjavainen
patent: 7407132 (2008-08-01), Kirjavainen
patent: 2010/0051754 (2010-03-01), Davidson
patent: 2010/0270420 (2010-10-01), Hansen

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