| 发明名称 |
PROPULSION UNIT FOR AN AIRCRAFT |
| 摘要 |
Propulsion unit for an aircraft, comprising a turbine, at least one propeller offset with respect to the turbine, and a power transmission disposed between the turbine and the propeller, the transmission comprising in series two constant velocity joints with a slide connection. |
| 申请公布号 |
US2017096231(A1) |
申请公布日期 |
2017.04.06 |
| 申请号 |
US201615285117 |
申请日期 |
2016.10.04 |
| 申请人 |
SAFRAN AIRCRAFT ENGINES |
发明人 |
Curlier Augustin Marc Michel |
| 分类号 |
B64D35/04;F02C7/36;B64D27/10;F02C3/00;B64D35/02;B64C11/46 |
主分类号 |
B64D35/04 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. Propulsion unit for an aircraft, comprising a turbine, at least one propeller of which the axis is offset with respect to the axis of the turbine, and a transmission for transmitting power between the turbine and the propeller, wherein the transmission comprises in series two constant velocity joints with a slide connection. |
| 地址 |
Paris FR |
