The invention provides a nacelle appearance structure for throwing drop sonde. The structure comprises a front section part, a middle section part and a rear section part. The middle section part is acylinder, and the front section part and the rear section part are cone-like bodies; and by arranging the middle section part, an internal storage space of the drop sonde is increased, and meanwhilepneumatic drag reduction is performed through smooth transition of simple cambered surfaces of the front section part and the rear section part.

    本发明提出了一种用于投放下投探空仪的吊舱外形结构,包括前段部、中段部和后段部,其中中段部为圆柱体,前段部、后段部为类圆锥体;本发明通过设置中段部增大了下投探空仪的内部存储空间,同时通过前段部和后段部简单弧面平滑过渡进行气动减阻。


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    Title :

    Nacelle appearance structure for throwing drop sonde


    Additional title:

    一种用于投放下投探空仪的吊舱外形结构


    Contributors:
    CAO SHIKUN (author) / YAN LINMING (author) / XIAO LIANGHUA (author) / XIA SHENGLIN (author) / FENG WENLIANG (author) / YAO JIEKE (author) / ZHOU WEI (author) / XU LIANG (author)

    Publication date :

    2020-10-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G01W METEOROLOGY , Meteorologie



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