| 发明名称 |
GAS TURBINE ENGINE WITH TWIN OFFSET GAS GENERATORS |
| 摘要 |
A gas turbine engine comprises a fan on an engine central axis. Plural gas generators are downstream of the fan, each along a respective central axis, mutually offset, and offset from the engine central axis. A fan drive turbine is on the engine central axis, downstream of the dual gas generators, and driven by output from the dual gas generators, to drive the fan. |
| 申请公布号 |
US2015211416(A1) |
申请公布日期 |
2015.07.30 |
| 申请号 |
US201514595284 |
申请日期 |
2015.01.13 |
| 申请人 |
United Technologies Corporation |
发明人 |
Chandler Jesse M.;Suciu Gabriel L. |
| 分类号 |
F02C3/14;F02C3/06;F02C3/10;F02C7/20;F02C6/02 |
主分类号 |
F02C3/14 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A gas turbine engine comprising:
a fan on an engine central axis; plural gas generators downstream of the fan, each along a respective central axis that are mutually offset and offset from the engine central axis; and a fan drive turbine on the engine central axis, downstream of the dual gas generators, and driven by output from the dual gas generators, for driving the fan. |
| 地址 |
Hartford CT US |
