Gas turbine engine fuel control

Details Gas turbine engine fuel control Gas turbine engine fuel control

1982-04-19

1984-09-04

Gruber, Felix D.

Boots, shoes, and leggings

60 39281, F02C 902, F02C 914

Patent

active

044701187

ABSTRACT:
The ability of a gas turbine engine to recover from surge is enhanced by implementing a closed loop control mode wherein fuel flow is varied as a function of the ratio of the rate of change of engine gas generator speed to compressor discharge pressure.

REFERENCES:
patent: 2974483 (1961-03-01), Sanders
patent: 3307352 (1967-03-01), Stearns et al.
patent: 3482396 (1969-12-01), Nelson et al.
patent: 3939649 (1976-02-01), McCabe
patent: 4117668 (1978-10-01), Elsaesser et al.

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