Power plants – Reaction motor – Liquid oxidizer
Patent
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.
LandOfFree
Turbojet engine with sonic injection afterburner does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Turbojet engine with sonic injection afterburner, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Turbojet engine with sonic injection afterburner will most certainly appreciate the feedback.
Profile ID: LFUS-PAI-O-1917622