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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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