The invention provides a system for measuring the handle force of an aviation airborne accelerator console. The system comprises a controller (1), a loading table (2), a mechanical arm (3), a measuring device (4), a clamping device (5) and an aviation airborne accelerator console handle (11). In the measuring process, a test guide block (17) firstly moves to the position over a clamping block I (8), then the test guide block (17) moves downwards, then a shaft of the test guide block (17) slowly enters a clamping groove of the clamping block I (8), and after the shaft moves to a limited position, connection between a clamping device (5) and a measuring device (4) is achieved. After the clamping device (5) stably clamps the aviation airborne accelerator console handle (11), the measuring device (4) measures the handle force of the aviation airborne accelerator console handle (11). According to the invention, the technical problems of large force value error, tedious operation, high labor cost and the like in the aviation airborne accelerator console handle force testing process are solved.
本发明提出了一种航空机载油门操纵台手柄力的测量系统,该系统包括:控制器(1)、加载台(2)、机械臂(3)、测量装置(4)、夹持装置(5)和航空机载油门操纵台手柄(11)。在测量过程中,测试引导块(17)先移动到夹持块Ⅰ(8)的正上方,然后测试引导块(17)下移,然后测试引导块(17)的轴缓慢进入夹持块Ⅰ(8)卡槽,待移动到限定位置后,实现夹持装置(5)与测量装置(4)的连接;夹持装置(5)在稳定夹持航空机载油门操纵台手柄(11)之后,测量装置(4)测量航空机载油门操纵台手柄(11)的手柄力。本发明解决了航空机载油门操纵台手柄力测试过程中力值误差大、操作繁琐,人工成本高等技术难题。
Aviation airborne accelerator console handle force measuring system
一种航空机载油门操纵台手柄力的测量系统
2023-12-12
Patent
Electronic Resource
Chinese
IPC: | G01L Messen von Kraft, mechanischer Spannung, Drehmoment, Arbeit, mechanischer Leistung, mechanischem Wirkungsgrad oder des Drucks von Fluiden , MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE / 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 |
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