发明名称 Gas turbine set
摘要 A gas turbine set, with a cooling air system through which at least one cooling air mass flow flows from a compressor to thermally highly loaded components of the gas turbine set. Pressure increasing ejectors are arranged in a cooling air duct of the cooling air system for increasing the pressure of flowing cooling air. The ejectors are operable with a working fluid. The working fluid mass flow is less than twenty percent of a driven cooling air mass flow.
申请公布号 US7143573(B2) 申请公布日期 2006.12.05
申请号 US20030635668 申请日期 2003.08.07
申请人 ALSTOM SWITZERLAND LTD 发明人 HOFFMANN JUERGEN;ROFKA STEFAN;WAELCHLI RENE;DITTMANN ROLF
分类号 F02C6/00;F01K23/10;F02C7/18 主分类号 F02C6/00
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