Gas turbine circuit system

Details Gas turbine circuit system Gas turbine circuit system

1975-04-11

1976-12-14

Croyle, Carlton R.

Power plants

Combustion products used as motive fluid

Multiple fluid-operated motors

60 3952, F02C 702

Patent

active

039967387

ABSTRACT:
A gas turbine circuit system in which the individual heat exchanging components are never subjected to maximum temperature and maximum pressure simultaneously so to reduce maximum stress for the component material, a feed back circuit from the outlet of the first turbine stage back to the heat source gas inlet comprising a mixing path in which the operational hot gas is mixed with injected cold gas under high pressure and substantial pressure-gain for the hot gas.

REFERENCES:
patent: 3125855 (1964-03-01), Kofink et al.
patent: 3621654 (1971-11-01), Hull
patent: 3630022 (1971-12-01), Jubb

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