发明名称 |
Fixing device for a blade mounting of a compressor or turbine stage of a gas turbine system comprises a blade having a counter-contour corresponding to a connecting element of a wedge element to produce a form-locking connection |
摘要 |
Fixing device for a blade mounting of a compressor or turbine stage of a gas turbine system comprises a wedge element (43) having at least one connecting element (45) for the side of a blade (31, 32). At least one of the two blades adjacent to the wedge element has a counter-contour (46) corresponding to the connecting element so that the wedge element and the blade engage with each other with a form-locking connection. Preferred Features: The connecting element and the corresponding counter-contour are designed as a dovetail joint. |
申请公布号 |
DE10134611(A1) |
申请公布日期 |
2002.06.27 |
申请号 |
DE2001134611 |
申请日期 |
2001.07.17 |
申请人 |
ALSTOM (SWITZERLAND) LTD., BADEN |
发明人 |
KAPPIS, WOLFGANG;WALTKE, ULRICH;WETTSTEIN, HANS E.;THUERINGER, FERDINAND;RIHAK, PAVEL;BACHOFNER, RENE |
分类号 |
F01D5/30;F01D5/32;(IPC1-7):F01D5/32 |
主分类号 |
F01D5/30 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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