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
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