| 发明名称 |
UNIVERSAL SEAL |
| 摘要 |
A seal for a gas turbine engine includes a top, a bottom, a left side, a right side, a back and a front. The back is parallel to the front and the left side is parallel to the right side such that a non-square shape is formed by the intersection of the back, the left side, the front and the right side. The top includes a first vane mating surface and the bottom includes a second vane mating surface. |
| 申请公布号 |
US2015315924(A1) |
申请公布日期 |
2015.11.05 |
| 申请号 |
US201514735530 |
申请日期 |
2015.06.10 |
| 申请人 |
United Technologies Corporation |
发明人 |
Duelm Bradley T.;Brown Randall J.;Shirk Nathan A.;Holby Lewis M. |
| 分类号 |
F01D11/00;F16J15/16 |
主分类号 |
F01D11/00 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A seal for a gas turbine engine comprising:
a top; a bottom; a left side; a right side; a back; and a front, wherein said back is parallel to said front and said left side is parallel to said right side such that a non-square shape is formed by the intersection of the back, the left side, the front and the right side, and said top includes a first vane mating surface and said bottom includes a second vane mating surface. |
| 地址 |
Hartford CT US |
