| 发明名称 |
SISTEMA DE AUMENTO DE CONTROLABILIDAD PARA UNA AERONAVE. |
| 摘要 |
<p>The system includes deflection transmission means (16) to provide a deflection position of the high-lift device (8) for each setting angle position of an adjustable HTP (2). Preferably, the deflection transmission means (18,20,23) comprise essentially of a mechanical linkage connected between the high-lift device (8) and the aircraft (1).</p> |
| 申请公布号 |
ES2350544(B1) |
申请公布日期 |
2012.05.16 |
| 申请号 |
ES20090000687 |
申请日期 |
2009.03.12 |
| 申请人 |
AIRBUS OPERATIONS, S.L.;AIRBUS ESPANA, S.L. |
发明人 |
VELA ORGE, PILAR;NAMER, ARNAUD;PASCUAL FUERTES, ANGEL;SIMON CALERO, FCO. JAVIER |
| 分类号 |
B64C9/10;B64C5/10;B64C13/28 |
主分类号 |
B64C9/10 |
| 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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