NACELLE SCOOP INLET

申请号 PCT/US2013055935 申请日 2013-08-21 公开(公告)号 WO2014077922A3 公开(公告)日 2014-07-31
申请人 UNITED TECHNOLOGIES CORP; 发明人 ZYSMAN STEVEN H;
摘要 A scoop inlet for use in a gas turbine engine nacelle has a scoop inlet, and a tab extending forwardly of the scoop inlet. The scoop communicates with a downstream flowpath. The tab has at least one opening at a location upstream of the scoop inlet. A nacelle and a gas turbine engine are also disclosed.
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