| 发明名称 |
Compressor blade has in radially outer blade end one or more indentations in one or more rows |
| 摘要 |
<p>The compressor blade for an air jet drive mechanism has a radially outer blade end (6) with at least one indentation (9). If more than one indentation is provided these can be arranged in a single or several rows. The depth of the indentations is greater than the width of a gap between the outer blade end and the compressor housing.</p> |
| 申请公布号 |
DE10305351(A1) |
申请公布日期 |
2004.08.19 |
| 申请号 |
DE2003105351 |
申请日期 |
2003.02.10 |
| 申请人 |
ROLLS-ROYCE DEUTSCHLAND LTD & CO KG |
发明人 |
OPPER, HANS OTTO |
| 分类号 |
F01D5/20;F04D29/16;F04D29/32;(IPC1-7):F04D29/38;F01D5/14;F02K3/06 |
主分类号 |
F01D5/20 |
| 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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