The invention discloses a wing trailing edge deflection driving mechanism, a wing and an aircraft. Relates to the field of aircrafts. The mechanism comprises two supporting devices, and the two supporting devices are hinged and used for being connected with the front edge and the rear edge of a wing correspondingly; the connecting devices are symmetrically arranged above and below a hinge point of the two supporting devices and are connected with the two supporting devices; the connecting device can deform along the length direction of the wing; the driving devices are symmetrically arranged above and below the hinge point of the two supporting devices, the two ends of the driving device located above the hinge point are connected with the parts, located above the hinge point, of the two supporting devices correspondingly, and the two ends of the driving device located below the hinge point are connected with the parts, located below the hinge point, of the two supporting devices correspondingly. The driving device can deform in the length direction of the wings. The weight can be reduced, and the energy consumption can be reduced.
本发明公开了一种机翼后缘偏转驱动机构、机翼及飞行器;涉及飞行器领域;该机构包括支撑装置,两个支撑装置铰接,分别用于连接机翼前缘和连接机翼后缘;连接装置对称设于两个支撑装置的铰接点上方和下方,并连接两个支撑装置;连接装置能够沿机翼长度方向形变;驱动装置对称设于两个支撑装置的铰接点上方和下方,且位于铰接点上方的驱动装置两端分别与两个支撑装置位于铰接点上方的部分连接,位于铰接点下方的驱动装置两端分别与两个支撑装置位于铰接点下方的部分连接;驱动装置能够沿机翼长度方向形变。本发明能够减轻重量、并降低能量消耗。
Wing trailing edge deflection driving mechanism, wing and aircraft
一种机翼后缘偏转驱动机构、机翼及飞行器
30.05.2025
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |