| 发明名称 |
INTEGRALLY BLADED ROTOR |
| 摘要 |
An integrally bladed rotor for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a radially inner hoop extending circumferentially about an axis, a plurality of circumferentially spaced, axially extending slots, separated by respective blade supports, and a seal system that includes seal fingers extending axially through the slots. |
| 申请公布号 |
US2016069203(A1) |
申请公布日期 |
2016.03.10 |
| 申请号 |
US201314783925 |
申请日期 |
2013.04.12 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
Aiello Nicholas |
| 分类号 |
F01D11/00;F01D5/02;F04D29/32;F01D5/30 |
主分类号 |
F01D11/00 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An integrally bladed rotor for a gas turbine engine, comprising:
a radially inner hoop extending circumferentially about an axis; a plurality of circumferentially spaced, axially extending slots, separated by respective blade supports; and a seal system that includes seal fingers extending axially through the slots. |
| 地址 |
Hartford CT US |
