Control means for an augmentor for a gas turbine engine

F - Mech Eng,Light,Heat,Weapons – 02 – C

Patent

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60/129, 341/38.1

F02C 9/28 (2006.01) F02K 3/10 (2006.01)

Patent

CA 1121876

Abstract of the Disclosure This invention serves to improve augmentor effectiveness of a turbine fan engine that has a bypass airstream and a core stream by synthesizing signals indicative of both the airflow of the bypass stream and core stream and directly scheduling fuel/air ratio for both streams and ascertaining the desired fuel flow to be used to meter fuel to each of the streams. -1-

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