| 发明名称 |
REMOVABLE AUXILIARY POWER DEVICE FOR AIRCRAFT AND AIRCRAFT ADAPTED TO USE AT LEAST ONE SUCH DEVICE |
| 摘要 |
An auxiliary power device may be exteriorly removably connected to an aircraft in order to allow the increase of the performance data of the aircraft, namely at take-off and landing. The auxiliary power device includes a propeller (or fan) connected to an electric engine fed by an electric power supply. |
| 申请公布号 |
US2016176533(A1) |
申请公布日期 |
2016.06.23 |
| 申请号 |
US201514974660 |
申请日期 |
2015.12.18 |
| 申请人 |
Airbus Operations SAS |
发明人 |
Cazals Olivier;Druot Thierry;Guillemaut Julien |
| 分类号 |
B64D27/24;B64D41/00;B64D29/02;B64C3/32;B64C11/00 |
主分类号 |
B64D27/24 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An auxiliary power device for aircraft, said auxiliary power device comprising:
at least one electric motor; an electrical power supply for said electric motor; and a propeller connected to said electric motor and able to generate at least one of the following forces: a propulsion force, a reverse force in the opposite direction to the direction of the speed of the aircraft, said auxiliary power device being externally connectable in removable fashion to said aircraft and being configured so that the auxiliary power device can be mounted and demounted on the ground. |
| 地址 |
Toulouse FR |
