发明名称 High by-pass ratio turbofan
摘要 <p>The turbofan has a fan mounted on upstream of a compressor and driven in rotation by a turbine A rigid cylindrical envelop (10) has upstream and downstream ends (19, 26) fixed on intermediate and exhaust cases, respectively. The envelope assures transmission of force between the intermediate and exhaust cases. The end (26) has foil flaps (27) which hinder air flow towards the downstream and break the thrust provided by the fan.</p>
申请公布号 EP1568868(A2) 申请公布日期 2005.08.31
申请号 EP20050290121 申请日期 2005.01.20
申请人 SNECMA 发明人 BEUTIN, BRUNO;DOS SANTOS, NELSON;FERT, JEREMY;LACORRE, FABIENNE;PICARD, JEAN-LOUIS
分类号 F01D25/24;F02K1/68;F01D5/22;F02C7/00;F02C7/20;F02K1/70;F02K3/06;(IPC1-7):F02C7/20 主分类号 F01D25/24
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