METHOD AND SYSTEM FOR REDUCING HOT SOAKBACK

A method for cooling a gas turbine engine includes supplying power to a motor to generate mechanical motion and translating the mechanical motion of the motor to a shaft of the gas turbine engine to rotate a compressor stage and a turbine stage after the engine has been shutdown to circulate air wit...

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Bibliographische Detailangaben
1. Verfasser: FRANCISCO JAY M
Format: Patent
Sprache:eng
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