Method of operating a turbine

Details Method of operating a turbine Method of operating a turbine

1974-05-28

1978-06-06

Croyle, Carlton R.

Power plants

Combustion products used as motive fluid

60 3914, 60 3946M, F02C 700, F02C 732

Patent

active

040928241

ABSTRACT:
A gas turbine for starting an aircraft engine and for driving auxiliary equipment, being normally run by combustion, receives decomposition gases of hydrazine, selectively on a standby basis, whereby aircraft engine fuel is added to these gases, and the mixture is then fed to the turbine to drive the turbine without combustion.

REFERENCES:
patent: 2648317 (1953-08-01), Mikulasek
patent: 2775866 (1957-01-01), Randall
patent: 2930184 (1960-03-01), Plescia et al.
patent: 2959919 (1960-11-01), Chiera et al.
patent: 2972911 (1961-02-01), Volk et al.
patent: 3087304 (1963-04-01), Walter
patent: 3451215 (1969-06-01), Barr
patent: 3525217 (1970-08-01), DeMattia
patent: 3660977 (1972-05-01), Reynolds

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