| 发明名称 |
METHOD OF ASSEMBLING GAS TURBINE ENGINE SECTION |
| 摘要 |
A method for assembling a section of a gas turbine engine is disclosed. The method involves aligning a vane ring with a first rotor hub such that a row of vanes on the vane ring is adjacent a first row of blades of the first rotor hub, and aligning a second rotor hub with the vane ring such that a second row of blades of the second rotor hub is adjacent the row of vanes and the row of vanes is axially between the first row of blades and the second row of blades. The first hub and the second hub are then non-mechanically bonded together. |
| 申请公布号 |
US2016215653(A1) |
申请公布日期 |
2016.07.28 |
| 申请号 |
US201615059805 |
申请日期 |
2016.03.03 |
| 申请人 |
United Technologies Corporation |
发明人 |
DaCunha Nelson;Christophel Jesse R. |
| 分类号 |
F01D25/24;B23K31/02;F01D5/06;F01D9/04;F01D17/14 |
主分类号 |
F01D25/24 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A method for assembling a section of a gas turbine engine, the method comprising:
aligning a vane ring with a first rotor hub such that a row of vanes on the vane ring is adjacent a first row of blades of the first rotor hub; aligning a second rotor hub with the vane ring such that a second row of blades of the second rotor hub is adjacent the row of vanes and the row of vanes is axially between the first row of blades and the second row of blades; and non-mechanically bonding the first hub and the second hub together. |
| 地址 |
Hartford CT US |
