| 发明名称 |
SEAL HAVING A LARGE COMPRESSION RANGE |
| 摘要 |
The invention relates to a seal designed to be inserted between a cowl of a rear section of a nacelle and a turbojet of an aircraft propulsion unit. The seal includes a cylindrical portion and at least one lip extending radially from a generatrix of the cylindrical part. |
| 申请公布号 |
CA2696837(C) |
申请公布日期 |
2016.02.16 |
| 申请号 |
CA20082696837 |
申请日期 |
2008.08.08 |
| 申请人 |
AIRCELLE |
发明人 |
BUNEL, SERGE |
| 分类号 |
F16J15/02;B64D29/00;F02C7/28;F16J15/10 |
主分类号 |
F16J15/02 |
| 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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