发明名称 COMBUSTOR OF A GAS TURBINE
摘要 An exemplary combustor includes at least a portion having an inner liner and an outer cover plate, which together form an interposed cooling chamber. A plurality of hollow elements extend from the liner and protrude into the cooling chamber. Each hollow element defines a damping volume connected to an inner volume of the combustion chamber via a calibrated duct. During operation, the hollow elements damp pressure pulsations and, in addition, also transfer heat.
申请公布号 US2012260657(A1) 申请公布日期 2012.10.18
申请号 US201213424839 申请日期 2012.03.20
申请人 EROGLU ADNAN;FREITAG EWALD;RUEDEL UWE;BENZ URS;HUBER ANDREAS;ALSTOM TECHNOLOGY LTD 发明人 EROGLU ADNAN;FREITAG EWALD;RUEDEL UWE;BENZ URS;HUBER ANDREAS
分类号 F23R3/26 主分类号 F23R3/26
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