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System for adjusting the spanwise load distribution of a wing
System for adjusting the spanwise load distribution of a wing
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机译:用于调节机翼翼展方向载荷分布的系统
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摘要
The wing (2) comprises a base flap system (4) consisting of inboard landing flap (5), an outboard landing flap (6) and an aileron (7). The inboard landing flap and outboard landing flap are not mechanically connected with each other and are independently displaceable in relative to the wing span direction.
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