| 发明名称 |
СИСТЕМА ЩИТКОВ НА КРЫЛЕ САМОЛЕТА С ЖЕСТКИМ КРЫЛОМ |
| 摘要 |
The flap system is centrally monitored by a flight control device connected to a flap control unit. Front and rear flaps (3) are mechanically coupled to drives integrated in the wings. The drives are connected to the flap control unit and can be individually controlled by it. |
| 申请公布号 |
RU2004109127(A) |
申请公布日期 |
2005.09.20 |
| 申请号 |
RU20040109127 |
申请日期 |
2004.03.26 |
| 申请人 |
ЭЙРБАС ДОЙЧЛАНД ГМБХ (DE) |
发明人 |
РЕКЗИК Мартин (DE);РЕХТЕР Харальд (DE);БЕЗИНГ Вольфганг (DE) |
| 分类号 |
B64C13/00;B64C3/00;B64C13/50;B64D45/00 |
主分类号 |
B64C13/00 |
| 代理机构 |
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代理人 |
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| 主权项 |
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| 地址 |
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