The invention belongs to the field of aviation engineering tests, and relates to a cabin control loading device and system. The cabin control mechanism loading device comprises a control mechanism loading tool; the mounting point of the operating mechanism loading tool sleeve is positioned between the left and right rocker arms; when the operating mechanism loading tool moves according to an operating instruction, the output rocker arm is driven to rotate, the rocker arm pushes the spring shaft core to compress the left spring or the right spring, and therefore the loading force borne by the operating mechanism is simulated. The operating mechanism loading tool comprises a loading rod, a left insertion lug, a right insertion lug, a mounting support, a sleeve assembly, a left spring, a right spring and a laser sensor assembly.
本发明属于航空工程试验领域,涉及一种座舱操纵加载装置及系统。座舱操纵机构加载装置包括操纵机构加载工装;操纵机构加载工装套筒安装点位于左右摇臂中间;操纵机构加载工装根据操纵指令运动时,带动输出摇臂转动,摇臂推动弹簧轴芯压缩左或右弹簧,从而模拟操纵机构受到的载荷力;操纵机构加载工装包括:加载杆、左插耳、右插耳、安装支座、套筒组件、左弹簧、右弹簧、激光传感器组件。
Cabin control loading device and system
一种座舱操纵加载装置及系统
2024-04-09
Patent
Electronic Resource
Chinese
IPC: | G01M TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES , Prüfen der statischen oder dynamischen Massenverteilung rotierender Teile von Maschinen oder Konstruktionen / 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 |
Collision protection platform structure for large loading cabin and large loading cabin
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