| 发明名称 |
GEARED TURBOFAN WITH A GEARBOX UPSTREAM OF A FAN DRIVE TURBINE |
| 摘要 |
A gas turbine engine according to an example of the present disclosure includes a drive turbine configured to drive a fan section, a combustor section located axially upstream of the drive turbine, and a speed change mechanism located axially downstream of the combustor section and axially upstream of the drive turbine. An output of the speed change mechanism connects to the fan. |
| 申请公布号 |
US2015176497(A1) |
申请公布日期 |
2015.06.25 |
| 申请号 |
US201414573812 |
申请日期 |
2014.12.17 |
| 申请人 |
United Technologies Corporation |
发明人 |
Schwarz Frederick M.;Suciu Gabriel L. |
| 分类号 |
F02C7/36;F02C7/32 |
主分类号 |
F02C7/36 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A gas turbine engine comprising:
a drive turbine configured to drive a fan section; a combustor section located axially upstream of the drive turbine; and a speed change mechanism located axially downstream of the combustor section and axially upstream of the drive turbine, an output of the speed change mechanism connected to the fan. |
| 地址 |
Hartford CT US |
