| 发明名称 | Thrust reversal device | ||
| 摘要 | The invention relates to a thrust reversal device comprising at least one cowl arranged in such a way that it can be moved between a closed position and an open position, said cowl being actuated by at least one actuator that can be driven by at least one electric engine. The invention is characterized in that at least one electric engine is connected to at least two separate power supplies (7a, 7b). | ||
| 申请公布号 | US9051898(B2) | 申请公布日期 | 2015.06.09 |
| 申请号 | US201013264951 | 申请日期 | 2010.03.18 |
| 申请人 | AIRCELLE | 发明人 | Maalioune Hakim |
| 分类号 | F02K1/70;F02K1/76;H02K11/00;H02K16/04 | 主分类号 | F02K1/70 |
| 代理机构 | Brinks Gilson & Lione | 代理人 | Brinks Gilson & Lione |
| 主权项 | 1. A thrust reversal device for an aircraft comprising at least one cowl mounted so as to be mobile between a closing position and an opening position, said cowl being actuated by at least one actuator able to be driven by at least one electric motor, wherein at least one electric motor is connected to at least two separate power supplies, and the electric motor is a dual-winding electric motor, each winding being connected to a separate power supply from the power supply of the other winding. | ||
| 地址 | Gonfreville L'Orcher FR | ||