发明名称 Gas turbine engine having slim-line nacelle
摘要 A nacelle assembly for a gas turbine engine includes a nacelle, a variable area fan nozzle, a sensor that detects a windmilling condition and a controller that communicates with the sensor. The variable area fan nozzle is moveable between a first position having a first discharge airflow area and a second position having a second discharge airflow area greater than the first discharge airflow area in response to detecting the windmilling condition.
申请公布号 US2008092548(A1) 申请公布日期 2008.04.24
申请号 US20060584030 申请日期 2006.10.20
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 MORFORD STEPHEN A.;LARKIN MICHAEL J.
分类号 F02K1/00 主分类号 F02K1/00
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