| 发明名称 |
GAS TURBINE ENGINE ARCHITECTURE WITH INTERCOOLED TWIN CENTRIFUGAL COMPRESSOR |
| 摘要 |
A gas turbine engine includes an intercooled twin centrifugal compressor. A pipe diffuser extends from the intercooled twin centrifugal compressor into an airflow path. |
| 申请公布号 |
US2014271121(A1) |
申请公布日期 |
2014.09.18 |
| 申请号 |
US201414209326 |
申请日期 |
2014.03.13 |
| 申请人 |
United Technologies Corporation |
发明人 |
Kupratis Daniel B. |
| 分类号 |
F04D17/12 |
主分类号 |
F04D17/12 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A gas turbine engine comprising:
an intercooled twin centrifugal compressor; and a pipe diffuser that extends from said intercooled twin centrifugal compressor into an airflow path. |
| 地址 |
Hartford CT US |
