发明名称 GAS TURBINE COMPRESSOR
摘要 A gas turbine compressor is disclosed. The compressor includes a compressor housing, guide vanes, rotor blades, and valve-controlled blow-in openings for stabilizing the compressor flow by air that is blown in. The air flow is detected by pressure sensors and the valves are controlled as a function thereof.
申请公布号 US2011103931(A1) 申请公布日期 2011.05.05
申请号 US20090935850 申请日期 2009.04.02
申请人 MTU AERO ENGINES GMBH 发明人 HILLER SVEN-J.
分类号 F01D17/08 主分类号 F01D17/08
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