Method and System for Mitigating Bowed Rotor Operation of Gas Turbine Engine
Embodiments of systems and methods for operating a gas turbine engine defining a bowed rotor condition are generally provided. The systems and methods include rotating a rotor assembly defining a bowed rotor condition from approximately zero revolutions per minute (RPM) to within a bowed rotor mitig...
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Format: | Patent |
Sprache: | chi ; eng |
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