HIGH-TEMPERATURE GAS-TURBINE ENGINE AND ITS OPERATING PROCEDURE Russian patent published in 1994 - IPC

Abstract RU 2006631 C1

FIELD: engine building. SUBSTANCE: some portion of compressed air is taken from compressor main air circuit, cooled down by means of heat exchange and heating of fuel (cryogenic fuel is used) burnt in auxiliary combustion chamber. Excess power obtained in auxiliary circuit is transferred to main circuit by compressing air in compressor auxiliary circuit. EFFECT: facilitated procedure. 2 cl, 1 dwg

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RU 2 006 631 C1

Authors

Grishin A.N.

Dates

1994-01-30Published

1988-03-25Filed