| 发明名称 |
Double Propulsor Imbedded In Aircraft Tail With Single Core Engine |
| 摘要 |
A drive arrangement for an aircraft comprises a pair of propulsor units each having a fan and a fan shaft for driving the fan. A core engine has a turbine driving a core engine shaft. A mechanical connection connects the core engine shaft to drive the fan shafts for each of the propulsor units An aircraft is also disclosed. |
| 申请公布号 |
US2017096232(A1) |
申请公布日期 |
2017.04.06 |
| 申请号 |
US201514874560 |
申请日期 |
2015.10.05 |
| 申请人 |
United Technologies Corporation |
发明人 |
Suciu Gabriel L.;Chandler Jesse M.;Lord Wesley K.;Epstein Alan H.;O'Flarity Steven M. |
| 分类号 |
B64D35/06;B64D29/04;B64D33/02;B64D27/20 |
主分类号 |
B64D35/06 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A drive arrangement for an aircraft comprising:
a pair of propulsor units each having a fan and a fan shaft for driving the fan; a core engine, the core engine having a turbine driving a core engine shaft; and a mechanical connection to connect said core engine shaft to drive the fan shafts for each of said propulsor units. |
| 地址 |
Hartford CT US |
