| 发明名称 |
ROTOR SEAL AND ROTOR THRUST BALANCE CONTROL |
| 摘要 |
Aspects of the disclosure are directed to an engine of an aircraft comprising: a first seal located forward of a disk of a turbine section of the engine, a second seal located forward of the disk of the turbine section and radially inward of the first seal relative to an axial centerline of the engine, where the first and second seals are floating, non-contact seals. |
| 申请公布号 |
US2017107839(A1) |
申请公布日期 |
2017.04.20 |
| 申请号 |
US201514887013 |
申请日期 |
2015.10.19 |
| 申请人 |
United Technologies Corporation |
发明人 |
Glahn Jorn A.;Schwarz Frederick M. |
| 分类号 |
F01D11/02;F04D29/32;F01D11/04;F04D29/08;F02C3/04;F01D5/02 |
主分类号 |
F01D11/02 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An engine of an aircraft comprising:
a first seal located forward of a disk of a turbine section of the engine; a second seal located forward of the disk of the turbine section and radially inward of the first seal relative to an axial centerline of the engine, wherein the first and second seals are floating, non-contact seals. |
| 地址 |
Hartford CT US |
