The invention provides an aircraft test comprehensive climate environment simulation system and a simulation method, and belongs to the technical field of an aircraft test. The simulation system comprises a testing machine, a laboratory structure system and an environment simulation system. The simulation method comprises the following steps: S1, low-temperature environment simulation; S2, high-temperature environment simulation; S3, temperature daily circulation environment simulation; S4, humidity environment simulation; S5, solar radiation environment simulation; S6, rain/wind-blown rain environment simulation; S7, snowfall/snow blowing environment simulation; S8, fog environment simulation; and S9, icing/freezing rain environment simulation. The system solves the problems that an existing experiment facility is generally small in size and relatively single in function, and has the advantages that the functions are complete, all modules work in a matched mode, and the number of devices is reduced.

    本发明提供了一种飞机试验综合气候环境模拟系统及模拟方法,属于飞机测试技术领域。模拟系统包括:试验机、实验室结构系统、环境模拟系统,模拟方法包括以下步骤:S1、低温环境模拟;S2、高温环境模拟;S3、温度日循环环境模拟;S4、湿度环境模拟;S5、太阳辐射环境模拟;S6、淋雨/风吹雨环境模拟;S7、降雪/风吹雪环境模拟;S8、雾环境模拟;S9、积冰/冻雨环境模拟。本发明解决了现有实验设施体积普遍较小、功能相对单一的问题,具有功能齐全且各个模块互相配合工作,节约设备数量的优点。


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    Title :

    Aircraft test comprehensive climate environment simulation system and simulation method


    Additional title:

    一种飞机试验综合气候环境模拟系统及模拟方法


    Contributors:
    WANG BINWEN (author) / WU JINGTAO (author) / CHENG ZHU (author) / REN ZHANPENG (author) / MA JIANJUN (author)

    Publication date :

    2022-02-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    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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