发明名称 |
Blade arrangement, particularly guide vane arrangement, for rotating turbo-engine, particularly turbine, has blade root, which has upstream blade root front edge and downstream blade root rear edge |
摘要 |
<p>The blade arrangement has a blade root, which has an upstream blade root front edge and a downstream blade root rear edge, where at the edges an attachment hook is provided, which is inserted into an receptacle groove of a component of a turbo-engine and which has two blade root sides laterally connecting the front edge and rear edge of the blade root with each other. A structure (9) that is wrapped around the blade root side laterally in peripheral direction is provided along one of the blade root sides and on the other blade root side a support surface is provided.</p> |
申请公布号 |
DE102011117755(A1) |
申请公布日期 |
2012.05.31 |
申请号 |
DE201110117755 |
申请日期 |
2011.11.05 |
申请人 |
ALSTOM TECHNOLOGY LTD. |
发明人 |
LAMMINGER, MARCO;TSYPKAIKIN, IGOR |
分类号 |
F01D5/14 |
主分类号 |
F01D5/14 |
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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