发明名称 Gas turbine engine with noise attenuating variable area fan nozzle
摘要 A rotary-wing aircraft includes a retractable port movable between a closed position and an open position to selectively control flow of combustion gases into a bypass passage to change a power distribution between a rotor system and a secondary propulsion system.
申请公布号 US8615980(B2) 申请公布日期 2013.12.31
申请号 US201113271181 申请日期 2011.10.11
申请人 AGRAWAL RAJENDRA K.;SIRICA STEVEN J.;SCHNEIDER WILLIAM F.;UNITED TECHNOLOGIES CORPORATION 发明人 AGRAWAL RAJENDRA K.;SIRICA STEVEN J.;SCHNEIDER WILLIAM F.
分类号 F02C6/00;F02G1/00;F02G3/00 主分类号 F02C6/00
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