The invention provides a wingtip mounting layout of a geophysical prospecting unmanned aerial vehicle, which is used for arranging two magnetic probes on a single side of the unmanned aerial vehicle with a vertical fin on the outer side of a main wing. The wingtip mounting layout comprises a first magnetic probe outer cover which is installed at the tail end of a vertical fin on the outer side ofthe main wing, a transition section winglet which is installed on the outer edge of the main wing, a second magnetic probe outer cover which is installed on the outer side of the main wing and connected with the main wing through the transition section winglet, and the transition section winglet is structurally connected with the main wing through a fixing rod inserted into the outer section of the main wing. Wherein the first magnetic probe outer cover and the second magnetic probe outer cover are symmetrical wing-shaped bodies which are used as a spiral body of a bus, and the axis of the spiral body of the first magnetic probe outer cover and the axis of the spiral body of the second magnetic probe outer cover are parallel to the axis of the machine body. The wingtip mounting layout of the geophysical prospecting unmanned aerial vehicle can meet simultaneous measurement of the geomagnetic field horizontal gradient and the geomagnetic field vertical gradient, the geomagnetic measurement result precision is effectively improved, and the wingtip mounting layout of the geophysical prospecting unmanned aerial vehicle has obvious advantages compared with a single probe.

    本发明提供了一种物探无人机翼梢挂载布局,用以实现在具有主翼外侧垂尾的无人机上单侧布置两个磁探头,包括:安装于主翼外侧垂尾末端的第一磁探头外罩、主翼外缘的过渡段小翼、以及安装于主翼外侧通过过渡段小翼与主翼连接的第二磁探头外罩,所述过渡段小翼通过插入主翼外段的固定杆与主翼结构连接;其中,所述第一磁探头外罩和第二磁探头外罩为对称翼型作为母线的旋成体,所述第一磁探头外罩和第二磁探头外罩的旋成体轴线与机身轴线平行。本发明中物探无人机翼梢挂载布局,能够满足地磁场水平梯度和地磁场垂直梯度的同时测量,还使得地磁测量结果精度得到有效提高,对比单探头具有明显优势。


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    Titel :

    Wingtip mounting layout of geophysical prospecting unmanned aerial vehicle


    Weitere Titelangaben:

    一种物探无人机翼梢挂载布局


    Beteiligte:
    CUI YUELI (Autor:in) / WANG CHAO (Autor:in) / LYU CHAO (Autor:in) / LIU KAIFEI (Autor:in) / LI JUNWEI (Autor:in) / GAO QIHANG (Autor:in) / GE CHUNLEI (Autor:in)

    Erscheinungsdatum :

    2021-01-12


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



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