The tilting mechanism comprises a first mounting seat, a driving module and a connecting rod mechanism, the driving module is arranged on the first mounting seat and comprises a tilting motor, the connecting rod mechanism is arranged on the first mounting seat and comprises a first connecting rod, a second connecting rod and a third connecting rod which are sequentially connected, and the tilting motor is arranged on the first connecting rod. The first connecting rod and the third connecting rod are further connected with the first mounting seat, the tilting motor is in driving connection with the first connecting rod, the length of the first connecting rod is a, the length of the second connecting rod is b, the length of the third connecting rod is c, the distance between the head end of the first connecting rod and the tail end of the third connecting rod is d, a is smaller than b and c, d and c are larger than b and d, and the sum of a and c is smaller than the sum of b and d. According to the technical scheme, when the driving module is out of control, the second mounting base cannot rotate infinitely relative to the first mounting base in one direction, the movement range of the second mounting base is limited, and collision interference between the connecting rod mechanism and other components is avoided.
本发明公开一种倾转机构和飞行器,其中,倾转机构包括第一安装座、驱动模块、及连杆机构,驱动模块设于第一安装座,驱动模块包括倾转电机,连杆机构设于第一安装座,连杆机构包括依次连接的第一连杆、第二连杆、及第三连杆,第一连杆和第三连杆还连接第一安装座,倾转电机与第一连杆驱动连接,第一连杆的长度为a,第二连杆的长度为b,第三连杆的长度为c,第一连杆的首端到第三连杆的末端的距离为d,a分别小于b、c、及d,c分别大于b和d,a和c的总和小于b和d的总和。本发明的技术方案旨在驱动模块失控时,第二安装座也不会沿一方向相对第一安装座无限旋转,限制第二安装座的活动范围,避免连杆机构与其他构件发生碰撞干涉。
Tilting mechanism and aircraft
倾转机构和飞行器
2024-01-23
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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