An aircraft suspension device actuator cylinder test device comprises a metal housing used as a main body structure of the device to install and bear each function system; the circuit detection system is used for releasing a control signal for simulation output, accurately controlling the working time sequence of the actuator cylinder, detecting the action current and the action voltage of the actuator cylinder, carrying out a single test and an aging test on the actuator cylinder, and displaying the test frequency and fault information; the air path detection system is used for simulating an air source of the aircraft suspension device, providing a power source for the actuator cylinder pneumatic transmission device and monitoring input air pressure and output air pressure in real time so as to control inflation and deflation; the power supply system is used for providing power supplies with different parameters for the test equipment; the control system is used for electrically controlling the test equipment; and the actuating cylinder mounting seat is used for mounting and connecting the actuating cylinder.
一种飞行器悬挂装置作动筒测试设备,所述测试设备包括:金属壳体,所述金属壳体用于作为设备的主体结构以安装承载各个功能系统;电路检测系统,所述电路检测系统用于投放控制信号进行仿真输出并精确控制作动筒工作时序,检测作动筒的动作电流和动作电压,针对作动筒开展单次试验和老练试验,并显示试验次数和故障信息;气路检测系统,所述气路检测系统用于模拟飞行器悬挂装置的气源,为作动筒气压传动装置提供动力源并实时监控输入气压和输出气压以控制充放气;电源系统,所述电源系统用于为测试设备提供不同参数的电源;控制系统,所述控制系统用于电气控制测试设备;作动筒安装座,所述作动筒安装座用于进行作动筒的安装和连接。
Aircraft suspension device actuator cylinder test equipment
一种飞行器悬挂装置作动筒测试设备
2024-02-09
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 |
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