The invention relates to a servo mechanism load simulation test method, belongs to the technical field of spacecrafts, and solves the problem that an existing high-power servo mechanism load simulation device cannot be placed in a conventional incubator and cannot be coupled with a mechanical environment and a thermal environment at the same time for a composite loading test. The method comprises the following steps: S1, assembling a load simulation device; s2, installing a servo mechanism to be tested; s3, the load simulation device provided with the servo mechanism to be tested is installed in a conventional temperature box; s4, debugging the load of the load simulation device; and S5, testing the servo mechanism to be tested. According to the invention, the high-power servo mechanism load simulation device is placed in a conventional incubator and is coupled with a mechanical environment and a thermal environment to carry out a composite loading test on the high-power servo mechanism, and the load test of the high-power servo mechanism of an aircraft in a real operation environment can be simulated.

    本发明涉一种伺服机构负载模拟测试方法,属于航天器技术领域,解决了现有大功率伺服机构负载模拟装置无法放在常规温箱中同时耦合力学环境、热学环境进行复合加载试验的问题。本发明包括以下步骤:步骤S1:组装负载模拟装置;步骤S2:安装待测伺服机构;步骤S3:将安装了待测伺服机构的负载模拟装置安装到常规温箱内;步骤S4:调试负载模拟装置的负载;步骤S5:测试待测伺服机构。本发明实现了大功率伺服机构负载模拟装置放置在常规温箱中同时耦合力学环境、热学环境对大功率伺服机构进行复合加载试验,能够模拟飞行器的大功率伺服机构真实运行环境下的负载测试。


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    Title :

    Servo mechanism load simulation test method


    Additional title:

    一种伺服机构负载模拟测试方法


    Contributors:
    LI ZHAOKAI (author) / MA JUN (author) / YU LINGJUN (author) / CHEN KAILUN (author) / QIN WENYUAN (author) / TANG XUDONG (author) / WEI HOUZHEN (author) / DI YU (author)

    Publication date :

    2024-10-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    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 / 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



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