| 发明名称 |
REPAIR OR REMANUFACTURE OF LINER PANELS FOR A GAS TURBINE ENGINE |
| 摘要 |
A method of remanufacturing a liner panel for a gas turbine engine includes removing a bushing from a damaged component; and molding the bushing with a material charge. A liner panel for a gas turbine engine includes a forward fan exit case liner panel with a donor bushing from a damaged forward fan exit case liner panel. A liner panel for a gas turbine engine includes a forward fan exit case liner panel molded from a material charge that includes a multiple of layers. At least one of the multiple of layer includes a discontinuity. |
| 申请公布号 |
US2015240661(A1) |
申请公布日期 |
2015.08.27 |
| 申请号 |
US201514628263 |
申请日期 |
2015.02.22 |
| 申请人 |
United Technologies Corporation |
发明人 |
Holland Brian K.;Morden Michael A.;Gates Brandon A.;Bogue William |
| 分类号 |
F01D25/24;F01D25/00;B23P6/00 |
主分类号 |
F01D25/24 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A method of remanufacturing a liner panel for a gas turbine engine, comprising:
removing a bushing from a damaged component; and molding the bushing with a material charge. |
| 地址 |
Hartford CT US |
