Acceleration control for a gas turbine engine

Power plants – Combustion products used as motive fluid – Multiple fluid-operated motors

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60 39181, F02C 928

Patent

active

049844253

ABSTRACT:
A control to control the acceleration mode for a gas turbine engine so as to allow the engine to accelerate rapidly with adequate stall margin by simulating a compressor stall limit. The stall limit is attained by generating a limiting ratio of burner pressure and another engine pressure as a function of corrected compressor rotor speed assuming that the stall margin is independent of compressor bleed, power extraction and degradation of engine efficiency.

REFERENCES:
patent: 3882672 (1975-05-01), Bauerfeind
patent: 4117668 (1978-10-01), Elsaesser et al.
patent: 4228650 (1980-10-01), Camp

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