The invention discloses a wing high-lift device in an over-stall state, and relates to the field of wings, and the wing high-lift device comprises a high-lift winglet device, a wing supplementary surface device, a motor and a connecting rod device; the high lift winglet device is directly connected with the motor and the connecting rod device, so that the high lift winglet device is driven by the motor and the connecting rod device to rotate; the wing supplementary surface device is a relatively independent device and is used for supplementing a gap left on the wing surface of the main wing after the high lift winglet device is opened; the high lift winglet device, the wing supplementary surface device, the motor and the connecting rod device are fixed together with the wing through the auxiliary fixing rib plate, so that the whole high lift device is fixed on the wing. The wing high-lift device disclosed by the invention is simple in structure and light in weight, the opening angle, closing and the like of the high-lift device are mainly controlled through one steering engine, the control reliability is high, and the number of occupied flight control channels is small.
本发明公开了一种过失速状态下的机翼增升装置,涉及机翼领域,其包括增升小翼装置、机翼补充面装置、电机和连杆装置;增升小翼装置直接和电机和连杆装置连接在一起,以实现增升小翼装置在电机和连杆装置带动下的转动;机翼补充面装置为一个相对独立的装置,用以补充翼面在增升小翼装置打开后在主翼翼面上留下的缺口;增升小翼装置、机翼补充面装置、电机和连杆装置通过辅助固定肋板和机翼固定在一起,以实现整个增升装置在机翼上的固定。本发明公开的机翼增升装置,结构简单、重量较轻,主要通过一个舵机来控制增升装置的打开角度及关闭等,控制可靠性高,且占用飞控的通道数少。
Wing high lift device in over-stall state
一种过失速状态下的机翼增升装置
2022-06-21
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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