Advanced integrated propulsion system with total optimized cycle

Details Advanced integrated propulsion system with total optimized cycle Advanced integrated propulsion system with total optimized cycle

1986-04-24

1989-08-22

Stout, Donald E.

Power plants

Combustion products used as motive fluid

Multiple fluid-operated motors

60 3929, 60 39511, F02C 106

Patent

active

048584282

ABSTRACT:
A gas turbine system with integrated high and low pressure circuits having a power transmission for extracting work from one of the circuits, the volume of air and fuel to the respective circuits being varied according to the power demand monitored by a microprocessor, wherein the turbine system has a low pressure compressor and a staged high pressure compressor with a combustion chamber and high pressure turbine associated with the high pressure compressor, and, a combustion chamber and a low pressure turbine associated with the low pressure compressor, the low pressure turbine being staged with the high pressure turbine to additionally receive gases expended from the high pressure turbine and a microprocessor to regulate air and gas flows between the compressor and turbine components in the turbine system.

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