Adaptive gas turbine acceleration control

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Details

364150, 364151, 340965, 340966, 60 39281, G05B 1300, F04D 2702

Patent

active

044907915

ABSTRACT:
An acceleration schedule, from which data is derived for use in calculating fuel flow during acceleration of a gas turbine engine, is modified each time the engine surges so as to avoid future surges.

REFERENCES:
patent: 2974483 (1961-03-01), Sanders
patent: 3482396 (1969-12-01), Nelson et al.
patent: 4117668 (1978-10-01), Elsaesser et al.
patent: 4249238 (1981-02-01), Spang et al.
patent: 4407013 (1983-09-01), Arcara et al.

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