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实用新型
CN204775997U 一种轻型飞机动翼面操纵系统固定结构 有权

一种轻型飞机动翼面操纵系统固定结构
摘要：
一种动翼面操纵系统固定结构，涉及飞机结构设计技术领域，用于固定轻型飞机动翼面的操纵系统，固定翼通过操纵系统控制动翼面，动翼面操纵系统固定结构为楔形钣金件，上顶面、下顶面、斜立面为一体成型结构且边缘设置有翻边，翻边通过铆钉固定连接在翼肋的腹板与翼梁的腹板上，斜立面上开设有长圆孔。本实用新型提供的动翼面操纵系统固定结构减少了固定装置的零件、降低了固定装置的重量，钣金件与翼肋腹板、翼梁腹板围成的楔形件结构稳定。
摘要（英）：

The utility model provides a move airfoil control system fixed structure, relates to aircraft structural design technical field for fixed light aerocraft moves the control system of airfoil, and the stationary vane moves the airfoil through control system control, and it be the wedge sheet metal component to move airfoil control system fixed structure, go up the top surface, down the top surface, to one side the facade be provided with the turn -ups for integrated into one piece structure and edge, the turn -ups passes through fix with rivet to be connected on the web of the web of rib and spar, has seted up the slotted hole on the oblique facade. The utility model provides a move the part that airfoil control system fixed structure has reduced fixing device, the weight that has reduced fixing device, wedge piece stable in structure that sheet metal component and rib web, spar web enclose.

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