Multiple propulsion with quatro vectorial direction system

Details Multiple propulsion with quatro vectorial direction system Multiple propulsion with quatro vectorial direction system

1988-11-02

1990-04-17

Stout, Donald E.

Power plants

Reaction motor

Motive fluid from diverse generators alternatively ejected...

60 3933, F02K 1100

Patent

active

049168967

ABSTRACT:
A compact, multimode propulsion system for aerial vehicles having multiple thermal cycles for selective independent or integrated operation in multiple modes to enable the propelled vehicle to operate in a full range of velocities under a variety of atmospheric conditions and efficiencies, the system including a turbo-jet unit with an air compressor, a gas turbine and an intermediate fuel injected combustor in association with an auxiliary combustor unit that includes a supplemental fuel and selective oxidizer supply, and a conversion system for selectively converting the auxiliary combustion unit into a secondary burner mode for the turbo-jet unit, an independent rocket mode operable with or without the turbo-jet unit or in independent ram-jet mode operable with or without the turbo-jet unit, the turbo-jet unit and auxiliary combustor system having separate exhaust systems for directional mobility of the vehicle to which the propulsion system is applied.

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patent: 3834161 (1974-09-01), Quigley, Jr. et al.
patent: 4010608 (1977-03-01), Simmons
patent: 4054030 (1977-10-01), Pedersen
patent: 4175384 (1979-11-01), Wagenknecht et al.

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