| 发明名称 |
Turbine engine compressor vane and spacer |
| 摘要 |
<p>A gas turbine engine rotor stack (44) includes one or more longitudinally outwardly concave spacers (62). Outboard surfaces of the spacers (62) may be in close facing proximity to inboard tips of vane airfoils (50). The airfoils have a dihedral and sweep profile.</p> |
| 申请公布号 |
EP1905952(A2) |
申请公布日期 |
2008.04.02 |
| 申请号 |
EP20070253629 |
申请日期 |
2007.09.12 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
BAUMANN, P. WILLIAM;LEJAMBRE, CHARLIE R.;SHARMA, OM PARKASH;HINGORANI, SANJAY S. |
| 分类号 |
F01D5/14;F01D5/06;F01D5/20;F01D11/00 |
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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