The invention discloses a rotating folding wing which comprises at least one pair of wings and a driving device, the wings can be horizontally and rotatably mounted on a fuselage, the driving device is mounted on the fuselage and used for driving the wings to rotate, and the driving device comprises a linear driver and a transmission device connected between the output end of the linear driver and each wing. The driving direction of the linear driver is consistent with the length direction of the fuselage, and the linear driver can drive each pair of wings to synchronously rotate through a transmission device to form a folded state or an unfolded state; the folding wing is simple in structure, the rotating angle of the wing can be accurately controlled, the control structure of the wing is simplified, the rotating precision of the wing is improved, the wing can automatically form a locking state when unfolded, the stability of the wing during flying is improved, in addition, the wing of the structure is horizontally stored to the two sides of a fuselage during folding, and the wing can be folded conveniently. The wings can synchronously rotate and be stored without mutual interference, and the landing occupied area of the whole aircraft can be reduced.
本发明公开了一种旋转式折叠机翼,包括可水平转动安装于机身上的至少一对机翼以及安装于机身上用于驱动机翼转动的驱动装置,所述驱动装置包括直线驱动器以及连接于直线驱动器输出端与每个机翼之间的传动装置,所述直线驱动器的驱动方向与机身长度方向一致,所述直线驱动器可通过传动装置驱动每对机翼同步转动形成折叠状态或展开状态;本发明折叠机翼其结构简单,可精确的控制机翼的转动角度,简化了机翼的控制结构,其提高机翼的转动精度,而且可在机翼展开时自动形成锁死状态,提高机翼飞行时的稳定性,另外该结构的机翼折叠时水平收纳至机身两侧,可满足各个机翼同步转动收纳而不相互干涉,而且可减小整个飞行器的降落占地面积。
rotating folding wing
旋转式折叠机翼
2021-07-23
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |