| 发明名称 |
GAS TURBINE ENGINE WITH THERMOPLASTIC FOR SMOOTHING AERODYNAMIC SURFACES |
| 摘要 |
A gas turbine engine has a surface configured for a gas flow path. The surface has at least one structural member defining a gap. A thermoplastic is deposited into the gap to smooth the surface, whereby the surface is aerodynamically and mechanically smoothly continuous over the gap area. A method is also disclosed. |
| 申请公布号 |
WO2014123838(A1) |
申请公布日期 |
2014.08.14 |
| 申请号 |
WO2014US14541 |
申请日期 |
2014.02.04 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
HYATT, THOMAS, B. |
| 分类号 |
F01D9/02;F01D11/00;F02C7/00 |
主分类号 |
F01D9/02 |
| 代理机构 |
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代理人 |
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| 主权项 |
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