| 发明名称 |
COOLING PASSAGES FOR GAS TURBINE ENGINE COMPONENT |
| 摘要 |
A gas turbine engine component includes a wall having an inner surface and an outer surface. At least one non-rectangular slot extends through the outer wall surface and is in communication with a passage. The passages extend through the wall and include an inlet portion located at the inner surface and an outlet portion located at the outer surface. An intermediate portion fluidly connects the inlet portion and the outlet portion. |
| 申请公布号 |
US2016169004(A1) |
申请公布日期 |
2016.06.16 |
| 申请号 |
US201514949047 |
申请日期 |
2015.11.23 |
| 申请人 |
United Technologies Corporation |
发明人 |
Quach San;King Christopher;Propheter-Hinckley Tracy A. |
| 分类号 |
F01D5/18;F01D11/08;F04D29/32;F02C7/18;F23R3/00;F01D9/04;F01D25/12 |
主分类号 |
F01D5/18 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A gas turbine engine component comprising:
a wall having an inner surface and an outer surface; and at least one non-rectangular slot extending through the outer wall surface and in communication with a passage, the passages extending through the wall comprising:
an inlet portion located at the inner surface;an outlet portion located at the outer surface; andan intermediate portion fluidly connecting the inlet portion and the outlet portion. |
| 地址 |
Farmington CT US |
