Method and apparatus for stabilizing an augmenter system

Details Method and apparatus for stabilizing an augmenter system Method and apparatus for stabilizing an augmenter system

F - Mech Eng,Light,Heat,Weapons

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F02C 7/22 (2006.01) F02K 99/00 (2009.01) F02C 9/16 (2006.01) F02C 9/28 (2006.01) F02K 3/06 (2006.01) F02K 3/08 (2006.01) F02K 3/10 (2006.01)

Patent

CA 1083836

METHOD AND APPARATUS FOR STABILIZING AN AUGMENTER SYSTEM Abstract A turbine engine is stabilized in high speed, high altitude flight conditions by reducing the maximum augmenter fuel/air ratio in response to certain pressure and temperature conditions. Temperatures and pressures indicative of those at the combustor are sensed and the augmenter fuel schedule is accordingly modified to a level which provides reduced fuel/air ratios and stable burning conditions.

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