发明名称 Gas turbine has slits in radially outer ends of vanes of rotor to contain radially movable sealing element sealing gap between vane and housing
摘要 The gas turbine has a rotor with vanes (10) adjoining the housing by radially outer ends (11). To minimize or seal the gap between these ends and the housing at least one slit (12) is inserted in the radially outer ends to contain at least one radially movable sealing element (17). The or each slit in each vane extends between a flow inlet edge (13) and a flow outlet edge (14) over the entire profile length of the relevant vane.
申请公布号 DE102004050739(A1) 申请公布日期 2006.04.20
申请号 DE20041050739 申请日期 2004.10.19
申请人 MTU AERO ENGINES GMBH 发明人 BICHLMAIER, CHRISTOPH
分类号 F01D5/20;F01D11/08;F04D29/16 主分类号 F01D5/20
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