The invention relates to an aerostat icing characteristic test system. The system comprises an aerostat, a water drop ejector, an environment data acquisition module, an aerostat differential pressuredata acquisition module, a tension test module, a data storage and processing module, a test state recording module and a low-temperature environment laboratory; the water drop ejector is arranged above the aerostat, the environment data acquisition module, the aerostat differential pressure data acquisition module and the tension test module are connected with the data storage and processing module, and the tension test module is connected with the mooring rope of the aerostat. Through the test system, the icing condition of the surface of the high-altitude aerostat can be truly reflected, so that an aerostat icing characteristic calculation model is verified and perfected.

    本发明涉及一种浮空器结冰特性试验系统,包括:浮空器,水滴喷射器,环境数据采集模块,浮空器压差数据采集模块,拉力测试模块,数据存储和处理模块,试验状态记录模块,低温环境实验室,其中,所述水滴喷射器设置在所述浮空器的上方,所述环境数据采集模块、浮空器压差数据采集模块、拉力测试模块与所述数据存储和处理模块相连,所述拉力测试模块与所述浮空器的系留绳相连。通过该试验系统可以真实反应高空中浮空器表面的结冰情况,从而验证和完善浮空器结冰特性计算模型。


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    Title :

    Aerostat icing characteristic test system


    Additional title:

    一种浮空器结冰特性试验系统


    Contributors:
    LIU QIANG (author) / WANG QIAN (author) / YANG YANCHU (author) / ZHU RONGCHEN (author) / CAI JINGJING (author) / CUI YANXIANG (author) / ZHAO KAIBIN (author)

    Publication date :

    2020-04-14


    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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