发明名称 |
Gas turbine with tip clearance control for blades |
摘要 |
<p>The gas turbine has several cover band segments forming a seal around the blades (3) of the turbine wheel (5). The cover band segments are fixed at front and rear points to the radially outer region of the blade segments (7) mounted on a control ring (9). The blade segments are radially an adjustable on the control ring.</p> |
申请公布号 |
EP1512842(A2) |
申请公布日期 |
2005.03.09 |
申请号 |
EP20040018924 |
申请日期 |
2004.08.10 |
申请人 |
ROLLS-ROYCE DEUTSCHLAND LTD & CO KG |
发明人 |
SCHIEBOLD, HARALD;MISTARECK, OLAF;WUNDERLICH, THOMAS |
分类号 |
F01D11/18;(IPC1-7):F01D11/18 |
主分类号 |
F01D11/18 |
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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