Turbojet engine with sonic injection afterburner

Details Turbojet engine with sonic injection afterburner Turbojet engine with sonic injection afterburner

1987-10-22

1990-01-30

Stout, Donald E.

Power plants

Reaction motor

Liquid oxidizer

60264, F02K 310

Patent

active

048965014

ABSTRACT:
A propulsion system having an afterburning turbojet with turbine bypass ducts in which the afterburner fuel is added. The hot gas products and fuel mixture enters the afterburner at sonic velocity. The turbojet turbine bypass has a flow control connected to the exit of the combustor to control the amount of turbine bypass flow.

REFERENCES:
patent: 2673445 (1954-03-01), Bruckmann
patent: 2929201 (1960-03-01), Lindsey
patent: 3063239 (1962-11-01), Jensen et al.
patent: 3352112 (1967-11-01), Chase
patent: 3626698 (1971-12-01), Baum
patent: 3633361 (1972-01-01), Bauger et al.
patent: 3712062 (1973-01-01), Nash
patent: 4072008 (1978-02-01), Kenworthy et al.
patent: 4448019 (1984-05-01), Klees
patent: 4509324 (1985-04-01), Urbach et al.

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