A device for fixing and detecting an aircraft control surface gap comprises a pressure loading mechanism and an automatic test system loaded with a test program, a control surface clamp in the pressure loading mechanism is of a U-shaped structure, a clamping disc is arranged on the inner side surface of the U-shaped structure, and a rotary handle is arranged on the control surface clamp; the control surface clamp is fixed to the top of a height adjusting rod, and the bottom of the height adjusting rod is installed on a supporting body. The height adjusting rod is provided with a force sensor fixing clamp used for installing a force sensor, a motor fixing clamp used for installing a servo motor, a laser distance measuring sensor installing support used for installing a laser distance measuring sensor and an adjusting disc used for controlling the height adjusting rod to move up and down. The force sensor, the servo motor and the laser distance measuring sensor are respectively connected with an automatic test system; and the measurement operation is simple and convenient, the applied force can be freely controlled, the continuous change is realized, and the flexible test requirement can be met.
一种用于固定检测飞机舵面间隙的装置,包括压力加载机构与装载有测试程序的自动测试系统,其中,压力加载机构中舵面夹具为U型结构,并在U型结构内侧表面设置有夹紧圆盘,所述舵面夹具上设置有旋柄;所述舵面夹具固定在高度调节杆顶部,所述高度调节杆底部安装在支撑体上,所述高度调节杆上设置有用于安装力传感器的力传感器固定夹、用于安装伺服电机的电机固定夹、用于安装激光测距传感器的激光测距传感器安装支架及用于控制高度调节杆上下位移的调整盘,且所述力传感器、伺服电机及激光测距传感器分别与自动测试系统连接;测量操作简便,且能自由控制所施加的力,具备持续性变化,能够满足灵活性测试要求。
Device for fixedly detecting aircraft control surface gap
一种用于固定检测飞机舵面间隙的装置
2021-09-28
Patent
Electronic Resource
Chinese
IPC: | B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / G01B MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS , Messen der Länge, der Dicke oder ähnlicher linearer Abmessungen |
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