Thrust control system for a gas turbine engine

Power plants – Reaction motor – With destruction sensing and preventing means

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Details

60243, F02K 300, F02C 904

Patent

active

041365178

ABSTRACT:
A thrust control system is provided for varying the thrust output of a gas turbine engine. The system is adapted to control the thrust output of the engine in a first mode in accordance with at least a pair of thrust-indicating parameters. The system is further adapted to control thrust output of the engine in a second mode in accordance with one of the thrust-indicating parameters.

REFERENCES:
patent: 3772880 (1973-11-01), Kubota
patent: 3790765 (1974-02-01), Morrison
patent: 3813063 (1974-05-01), Martin
patent: 3854287 (1974-12-01), Rembold
patent: 3867717 (1975-02-01), Moehring

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