发明名称 TURBOMACHINE COMPRESSOR
摘要 Turbomachine compressor comprising variable-pitch vanes comprising an aerofoil section connected by a mounting plate (17) of circular outline to a pivot (18) guided in rotation in an orifice in a casing (14), the mounting plate of the vane comprising at least one notch (60) for bleeding air from the compressor stream, this notch being intended to communicate with a hole (62) in the casing in order to remove the air bled off when the vanes are in a first position, and to be closed off by this casing when the vanes are in a second position, so that the flow rate of bled air depends on the pitch angle of the vanes.
申请公布号 US2011110773(A1) 申请公布日期 2011.05.12
申请号 US200913000929 申请日期 2009.06.15
申请人 SNECMA 发明人 DOMERCQ OLIVIER STEPHANE;PERROT VINCENT PAUL GABRIEL
分类号 F01D9/02 主分类号 F01D9/02
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