发明名称 Compressor for a gas turbine
摘要 An axial compressor providing a thermal adjustment of a housing of a compressor of a stationary gas turbine to the rotor is provided. A partial flow is decoupled from the compressor air flow for cooling gas turbine components. The contact of the partial flow decoupled from the compressor with the interior side of the housing is substantially limited, or even avoided, by a separating element in a collection chamber annularly encompassing the flow path in order to prevent the premature thermal heating of the gas turbine or of the housing during cold starting.
申请公布号 US2010275613(A1) 申请公布日期 2010.11.04
申请号 US20080812061 申请日期 2008.11.18
申请人 ALASTI MADJID;MAGHON HANS 发明人 ALASTI MADJID;MAGHON HANS
分类号 F02C6/04 主分类号 F02C6/04
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