发明名称 Diffusor für Ringbrennkammer, sowie Brennkammer und Turboprop mit einem solchen 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 DE602005003916(D1) 申请公布日期 2008.01.31
申请号 DE20056003916T 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
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