The invention relates to a gas-turbine system (2) of a power plant, said system comprising: a compressor (4); an annular combustion chamber (10) having a burner (14); and a turbine (6) coupled to the compressor (4). The gas turbine system (2) has a bypass line (16) for compressed air, said line bypassing the burner (14) and having a flow connection parallel thereto.
申请公布号
WO2015150088(A1)
申请公布日期
2015.10.08
申请号
WO2015EP55765
申请日期
2015.03.19
申请人
SIEMENS AKTIENGESELLSCHAFT
发明人
BÖTTCHER, ANDREAS;JUHNKE, SHAHRZAD;KLUGE, ANDRE;KOCK, BORIS FERDINAND;KRIEGER, TOBIAS
