Aircraft with gyroscopic stabilization system

Details Aircraft with gyroscopic stabilization system Aircraft with gyroscopic stabilization system

1992-03-03

1993-11-09

Oberleitner, Robert J.

Aeronautics and astronautics

Aircraft, heavier-than-air

Airplane and fluid sustained

244236, 244165, 74573F, B64C 1500

Patent

active

052595714

ABSTRACT:
An aircraft of the heavier-than-air type driven by reactors includes a fuselage of a lenticular configuration, a central shaft, and two rotary discs rotating in opposite directions and provided with large masses of inertia displaced or diplaceable toward the periphery thereof. The discs rotate about the central shaft driven by the reactors and turbines associated thereto, determining a gyroscopic effect which renders the aircraft stable. The base of the fuselage has a middle longitudinal hollow where the reactors are located. Two vertical rudders are positioned in front of and behind the fuselage and a horizontal depth aileron extends from the rear extension of the fuselage body.

REFERENCES:
patent: 2856142 (1958-10-01), Haviland
patent: 2980363 (1961-04-01), Schonstedt
patent: 3051414 (1962-08-01), Frost
patent: 3537669 (1970-11-01), Modesti
patent: 3862732 (1975-01-01), Wyatt et al.
patent: 4014483 (1977-03-01), MacNeill
patent: 4109549 (1978-08-01), Vincent
patent: 4214720 (1980-07-01), DeSautel
patent: 5026008 (1991-06-01), Lurie et al.

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