| 发明名称 |
ADHESIVE PATTERN FOR FAN CASE CONFORMABLE LINER |
| 摘要 |
A section of a gas turbine engine includes a case structure and a liner. The liner is attached to the case structure by a compliant adhesive. The adhesive covers at least a portion of the liner surface area, and can have interruptions used to tune the compliance of the adhesive layer. |
| 申请公布号 |
US2014186165(A1) |
申请公布日期 |
2014.07.03 |
| 申请号 |
US201213728200 |
申请日期 |
2012.12.27 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
Robertson, JR. Thomas J.;Lussier Darin S.;Stackhouse Kirk D.;Santana Johan |
| 分类号 |
F04D29/52 |
主分类号 |
F04D29/52 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A fan section of a gas turbine engine comprising:
a case structure; a continuous ring-shaped conformable liner with a surface area; and an adhesive layer attaching the liner to the case structure, wherein the adhesive layer includes interruptions. |
| 地址 |
US |
