发明名称 |
Device and method to attenuate thermo-acoustic resonance in combustion chambers |
摘要 |
The device has a combustion chamber (2) and a partial hollow cylindrical coaxial element (3) connected to the combustion chamber. Nozzle bores (10, 10a, 10b, 10c) are provided which are separated from each other and which a fluid flows and dissipates during the combustion of arising oscillation energy and an open jet (12) with a radial component into the combustion chamber (2). An independent claim is included for a method. |
申请公布号 |
EP1801500(A2) |
申请公布日期 |
2007.06.27 |
申请号 |
EP20060077112 |
申请日期 |
2006.11.27 |
申请人 |
DLR DEUTSCHES ZENTRUM FUER LUFT- UND RAUMFAHRT E.V. |
发明人 |
FORSTER, STEFAN;MICHEL, ULF;ROHLE, INGO |
分类号 |
F23M99/00;F23R3/06;F23J15/06 |
主分类号 |
F23M99/00 |
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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