发明名称 Diffusor for an annular combustor, as well as combustor and turboprop with such a diffusor
摘要 The diffuser has a separator (36) formed of a thin sheet for distributing an air flow (38) coming from a compressor into two annular internal and external jets (40, 42). The separator is connected to internal and external orbit walls (32, 34) by structural arms (44) which extend radially between the separator and the walls. The jets delimited by the separator have diffuser angles ranging from 12 to 13 degrees.
申请公布号 EP1688588(A1) 申请公布日期 2006.08.09
申请号 EP20050292746 申请日期 2005.12.20
申请人 SNECMA 发明人 CAYRE, ALAIN;DAGUENET, LUC;GAUTIER, CLAUDE;PIEUSSERGUES, CHRISTOPHE;TOUCHAUD, STEPHANE
分类号 F01D9/04;F23R3/04 主分类号 F01D9/04
代理机构 代理人
主权项
地址