Vertical lift aircraft

Aeronautics and astronautics – Aircraft – heavier-than-air – Airplane and fluid sustained

Patent

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244 23C, B64C 3906

Patent

active

053441001

ABSTRACT:
A vertical lift aircraft includes a central cabin and a set of concentric, circular, counter-rotating power blade assemblies. Gas turbine engines located in the central cabin provide power for rotating the power blade assemblies to cause lift and motion of the aircraft. The turbine engine exhaust gases are directed through a rotatable exhaust nozzle for aiding in the thrust and momentum of the aircraft. The gas turbine engines drive electric power generators which provide the necessary power for operation of the aircraft.

REFERENCES:
patent: 2951660 (1960-09-01), Giliberty
patent: 3650583 (1972-03-01), Itin et al.
patent: 3774865 (1973-11-01), Pinto
patent: 3997131 (1976-12-01), Kling

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