Augmentor outer segment lockout and fan upmatch

Power plants – Reaction motor – Method of operation

Patent

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Details

60236, 60241, 60226R, F02K 310

Patent

active

040954200

ABSTRACT:
A thrust augmented twin spool turbofan engine system to control instability at high altitude, low Mach number conditions wherein an engine electronic control monitors engine inlet temperature, engine burner pressure and Mach number, and inhibits fuel flow to the outermost augmentor segment when the engine inlet temp drops below 25.degree. F, when engine burner pressure drops below 120 psia or when the Mach number drops below 0.4. When fuel flow to the outermost augmentor is inhibited, upmatch logic modifies the variable nozzle AJ trim signal closed 8% and the power level angle trim signal up 4.degree..

REFERENCES:
patent: 3331204 (1967-07-01), Love
patent: 3360940 (1968-01-01), Rimmer
patent: 3472027 (1969-10-01), Snow
patent: 3854287 (1974-12-01), Rembold

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