Power plants – Reaction motor – Method of operation
Patent
1995-03-28
1997-12-09
Koczo, Michael
Power plants
Reaction motor
Method of operation
60230, 60231, 23926517, 23926519, 23926523, F02K 112, F02K 130
Patent
active
056947666
ABSTRACT:
A method and apparatus for controlling the throat area, expansion ratio and thrust vector of an aircraft turbine engine exhaust nozzle, includes means, such as deflectors and/or injected air, for producing and controlling regions of locally separated flow. The exhaust nozzle also allows control of the thrust vector angle defined by the gas exiting the nozzle to provide increased directional control of the aircraft.
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patent: 4088270 (1978-05-01), Maiden
patent: 4449678 (1984-05-01), Hapke
patent: 4451015 (1984-05-01), Hapke
patent: 5165227 (1992-11-01), Grieb
patent: 5267435 (1993-12-01), Frenkel et al.
Smereczniak Philip
Spetnagel David R.
Koczo Michael
McDonnell Douglas Corporation
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