| 发明名称 |
REDUCED VIBRATORY RESPONSE ROTOR FOR A GAS POWERED TURBINE |
| 摘要 |
A rotor for a turbomachine includes a rim defining a base of a rotor, an airfoil shaped blade extending from said rim and defining a chord line and a bore extending from said rim opposite said airfoil shaped blade. The rim further includes at least one rail extending away from said airfoil shaped blade. |
| 申请公布号 |
US2015369045(A1) |
申请公布日期 |
2015.12.24 |
| 申请号 |
US201514740316 |
申请日期 |
2015.06.16 |
| 申请人 |
United Technologies Corporation |
发明人 |
Aiello Nicholas;Bamford Bob S. |
| 分类号 |
F01D5/02;F02C3/04;F01D5/14 |
主分类号 |
F01D5/02 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A rotor for a turbomachine comprising:
a rim defining a base of a rotor; an airfoil shaped blade extending from said rim and defining a chord line; a bore extending from said rim opposite said airfoil shaped blade; and the rim further including at least one rail extending away from said airfoil shaped blade. |
| 地址 |
Hartford CT US |
