发明名称 GAS TURBINE ENGINE WITH AXIAL MOVABLE FAN VARIABLE AREA NOZZLE
摘要 <p>A nacelle assembly for a high-bypass gas turbine engine includes a fan variable area nozzle axially movable relative the fan nacelle to define an auxiliary port to vary a fan nozzle exit area and adjust a pressure ratio of the fan bypass airflow during engine operation.</p>
申请公布号 EP2788609(A1) 申请公布日期 2014.10.15
申请号 EP20120869088 申请日期 2012.12.07
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 KOHLENBERG, GREGORY A.;ZAMORA, SEAN P.
分类号 F02K3/075 主分类号 F02K3/075
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