Thrust control system for a gas turbine engine

Details Thrust control system for a gas turbine engine Thrust control system for a gas turbine engine

1979-07-27

1982-01-26

Krass, Errol A.

Boots, shoes, and leggings

60223, 60243, F02K 300

Patent

active

043131670

ABSTRACT:
An improved thrust control system is provided for controlling thrust output of a gas turbine engine in a manner which automatically compensates for engine deterioration and corresponding changes in engine performance. The system is further adapted to control the thrust output with at least a pair of thrust-indicating parameters, such as engine speed and temperature.

REFERENCES:
patent: 3813063 (1974-05-01), Martin
patent: 3846760 (1974-11-01), Ironside
patent: 3854287 (1974-12-01), Rembold
patent: 3987620 (1976-10-01), Giordano et al.
patent: 4032757 (1977-06-01), Eccles
patent: 4104876 (1978-08-01), Larsen et al.
patent: 4136517 (1979-01-01), Brown
patent: 4158884 (1979-06-01), McKinley et al.
patent: 4159625 (1979-07-01), Kerr

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