Method and apparatus for preventing overspeed in a gas turbine

Power plants – Combustion products used as motive fluid

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Details

60 3923, 60 3925, 60 3929, F02C 914

Patent

active

039980472

ABSTRACT:
A method and apparatus for preventing overspeed in a gas turbine in response to the rapid loss of applied load is disclosed. The method involves diverting gas from the inlet of the turbine, bypassing the same around the turbine and thereafter injecting the diverted gas at the turbine exit in a direction toward or opposing the flow of gas through the turbine. The injected gas is mixed with the gas exiting the turbine to thereby minimize the thermal shock upon equipment downstream of the turbine exit.

REFERENCES:
patent: 2759327 (1956-08-01), Huber
patent: 3037348 (1962-06-01), Gassmann
patent: 3070131 (1962-12-01), Wheatley
patent: 3203177 (1965-08-01), Johnson
patent: 3255586 (1966-06-01), Hennig
patent: 3418806 (1968-12-01), Wagner
patent: 3584459 (1971-06-01), Amann

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