Formation of auxiliary drive gas for turbine

Details Formation of auxiliary drive gas for turbine Formation of auxiliary drive gas for turbine

1977-03-14

1979-04-03

Croyle, Carlton R.

Power plants

Combustion products used as motive fluid

60 3914, 60 3946R, F02C 726, F02C 732

Patent

active

041470257

ABSTRACT:
An auxiliary gas turbine in an aircraft is driven by adding dimethyl-hydrazine to Kerosine and producing propellant gas by adding HNO.sub.3 or N.sub.2 O.sub.4 as oxidizer. Additional Kerosine is injected into the resulting gas for matching the gas constant of that gas to the gas constant of regular combustion gas which normally drives the turbine.

REFERENCES:
patent: 2900788 (1959-08-01), Felberg et al.
patent: 2906091 (1959-09-01), Kretschmer
patent: 3093968 (1963-06-01), Osofsky
patent: 3149460 (1964-09-01), La Rocca
patent: 3707074 (1972-12-01), Meyer et al.
patent: 3828551 (1974-08-01), Schmidt

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