| 发明名称 |
NOZZLE RING ADHESIVE BONDED BLADING FOR AIRCRAFT ENGINE COMPRESSOR |
| 摘要 |
A compressor nozzle ring for an aircraft includes an inner shroud, an outer shroud and a multiplicity of blades extending from the inner shroud to the outer shroud. Each blade passes through the inner shroud and is attached to it with sealing cement containing an organic polymer adhesive. The adhesive is polyimide based.
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| 申请公布号 |
US2009148283(A1) |
申请公布日期 |
2009.06.11 |
| 申请号 |
US20060523522 |
申请日期 |
2006.09.20 |
| 申请人 |
SNECMA MOTEURS |
发明人 |
MONS CLAUDE MARCEL;ANDRIEU SANDRA;GIRARD MANUEL;RIBASSIN FRANCOIS PIERRE |
| 分类号 |
F01D5/14;F01D9/04;F04D29/02;F04D29/54 |
主分类号 |
F01D5/14 |
| 代理机构 |
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代理人 |
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