发明名称 Jet engine compressor
摘要 <p>The compressor has a shroud (36) with upper and lower surface ramps (38, 40) joined upstream of a leading edge (28) of a blade to form a projection (42). A profile of the projection is twisted about a longitudinal axis of the shroud to force gas stream flowing in flow passages to flow around a blade root (16). The ramp (40) has a profile between the edge and a trailing edge (30) of the blade, and inclined relative to an outer surface of the shroud to deflect the gas stream flowing in the corresponding passage from an upper surface side of the blade to a lower surface side of an adjacent blade.</p>
申请公布号 EP2085620(A1) 申请公布日期 2009.08.05
申请号 EP20090151195 申请日期 2009.01.23
申请人 SNECMA 发明人 AUBIN, STEPHAN;BELMONTE, OLIVIER
分类号 F04D29/32;F01D5/14;F02K3/06 主分类号 F04D29/32
代理机构 代理人
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