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US08726632B2 Gas turbine engine having slim-line nacelle 有权
具有细线机舱的燃气轮机

Gas turbine engine having slim-line nacelle
Abstract:
A method of providing a slim-line nacelle for a gas turbine engine includes the steps of detecting a windmilling condition and increasing a discharge airflow area of a variable area fan nozzle in response to the detection of the windmilling condition.
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