Method and apparatus for controlling the throat area, expansion

Power plants – Reaction motor – Method of operation

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Details

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.

REFERENCES:
patent: 2952123 (1960-09-01), Rich
patent: 3020714 (1962-02-01), Eggers et al.
patent: 3659422 (1972-05-01), Hope
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.

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