发明名称 BLEED STRUCTURE FOR A BLEED PASSAGE IN A GAS TURBINE ENGINE
摘要 A bleed structure for a bleed passage in a gas turbine engine includes a first wall portion defining a first side of an opening for the passage, and a second wall portion defining a second side, opposite the first side of the opening. The first and second wall portions end at different positions in an extension direction of the opening.
申请公布号 US2010199633(A1) 申请公布日期 2010.08.12
申请号 US20100752284 申请日期 2010.04.01
申请人 VOLVO AERO CORPORATION 发明人 MARTENSSON HANS;NILSSON MARTIN
分类号 F02K3/075 主分类号 F02K3/075
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