Method and apparatus for stabilizing an augmenter system

Power plants – Reaction motor – Method of operation

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60241, 60243, 60261, 60 3928R, 60262, F02K 306, F02K 308, F02C 908

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active

041289951

ABSTRACT:
A turbine is stabilized in high speed, high altitude flight conditions by reducing the maximum augmenter fuel/air ratio in response to certain pressure and temperature conditions. Temperatures and pressures indicative of those at the combustor are sensed and the augmenter fuel schedule is accordingly modified to a level which provides reduced fuel/air ratios and stable burning conditions.

REFERENCES:
patent: 3205655 (1965-09-01), Wright
patent: 3293847 (1966-12-01), Rogers
patent: 3513899 (1970-05-01), Paduch
patent: 3688504 (1972-09-01), Hutchinson
patent: 3830055 (1974-08-01), Erlund
patent: 3852958 (1974-12-01), Adams
patent: 3854287 (1974-12-01), Rembold
patent: 3867717 (1975-02-01), Moehring
patent: 3908363 (1975-09-01), Bauerfeind
IHI Engineering Review (Japan), vol. 3, No. 5, Sep. 1970, Basic Study of After-Burner, pp. 37-53.

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