Gas turbine engine cooling system

Power plants – Combustion products used as motive fluid – Multiple fluid-operated motors

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Details

60 3966, F02C 702, F02C 712

Patent

active

039823903

ABSTRACT:
A device to produce engine braking on a two-shaft gas turbine engine including an air brake compressor on the power turbine shaft for absorbing energy from the power turbine shaft thereby to control power transfer to a power output shaft. The system includes a variable control assembly to throttle inlet air flow to the air brake compressor so as to regulate the amount of power absorption from the power turbine shaft.

REFERENCES:
patent: 3551068 (1970-12-01), Scalzo
patent: 3678285 (1972-07-01), Griffith
patent: 3742705 (1973-07-01), Sifford

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