The invention discloses a flaperon structure, a wing and an aircraft. The flaperon structure comprises a main wing, a flaperon, a fixed bracket and a connecting rod, wherein the flaperon is arranged on the rear edge of the main wing, the first end of the fixing support is fixedly arranged on a rear beam of the main wing, the second end of the fixing support inclines towards the rear inclined lower portion of the main wing and is hinged to the first end of the connecting rod through a hinge shaft, and the second end of the connecting rod is fixedly connected with the flaperon. The hinge shaft is arranged on the main wing, so that the flaperon can be driven to deflect upwards or downwards around the axis of the hinge shaft, and when the flaperon does not deflect, the front edge of the flaperon is attached to the rear edge of the main wing. According to the invention, the problems of inaccurate transmission distance and angle, low transmission efficiency and unsuitability for small aircrafts caused by the adoption of a complex connecting rod system and an actuating mechanism in the flaperon in the prior art are solved.
本申请公开了一种襟副翼结构、机翼及飞行器,包括:主翼、襟副翼、固定支架和连杆;其中,所述襟副翼设于所述主翼的后缘,所述固定支架的第一端固设于所述主翼的后梁上,所述固定支架的第二端朝向所述主翼的后斜下方倾斜并与所述连杆的第一端通过铰链轴铰接,所述连杆的第二端与所述襟副翼固定连接,以使所述襟副翼可受驱动地绕铰链轴的轴线向上偏转或向下偏转,当所述襟副翼未偏转时,所述襟副翼的前缘与所述主翼的后缘相贴合。本申请解决了相关技术中襟副翼采用了复杂的连杆系和作动机构,导致传动的距离与角度不准确,传动效率不高,不适用于小型飞机的问题。
Flaperon structure, wing and aircraft
襟副翼结构、机翼及飞行器
2023-04-04
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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