The gas turbine (51) has a combustion chamber (55) and a burner (1) opening into the combustion chamber at a burner opening enclosed by a Helmholtz resonator in annular manner. The resonator has a resonator volume and opens into the burner at a resonator opening that is continued into the resonator volume by a small pipe.
申请公布号
EP1342953(A1)
申请公布日期
2003.09.10
申请号
EP20020005137
申请日期
2002.03.07
申请人
SIEMENS AKTIENGESELLSCHAFT
发明人
FLOHR, PATRICK;KREBS, WERNER, DR.;PRADE, BERND, DR.
