发明名称 COMBINED STABILITY AND CUSTOMER BLEED WITH DIRT, WATER AND ICE REJECTION
摘要 A compressor section of a gas turbine engine includes a bleed port having a flow splitter therein so as to define a downstream bleed channel having a downstream inlet and an upstream bleed channel having an upstream inlet that is positioned radially outward from the downstream inlet.
申请公布号 US2016326957(A1) 申请公布日期 2016.11.10
申请号 US201514706748 申请日期 2015.05.07
申请人 United Technologies Corporation 发明人 Feulner Matthew R.;Merry Brian D.;Chandler Jesse M.;Suciu Gabriel L.;Staubach Joseph B.
分类号 F02C6/08;F02K3/06;F02C3/10 主分类号 F02C6/08
代理机构 代理人
主权项 1. A compressor section of a gas turbine engine comprising: a bleed port having a flow splitter therein so as to define a downstream bleed channel having a downstream inlet and an upstream bleed channel having an upstream inlet that is positioned radially outward from the downstream inlet.
地址 Hartford CT US
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