The invention discloses an unmanned aerial vehicle launching fixing device which comprises an unmanned aerial vehicle fixing frame, a supporting plate, a locking seat, a rotating shaft A, a pin shaft B, a pin shaft and a supporting plate elastic reset part, a pin shaft limiting clamping groove is formed in the locking seat, the unmanned aerial vehicle fixing frame comprises a left baffle, a right baffle and a bottom plate, and a supporting plate groove is formed in the bottom plate; the lower end of the left baffle and the lower end of the right baffle are fixedly connected with the bottom plate, rotating shaft limiting sliding grooves are formed in the middle of the left baffle and the middle of the right baffle, the rotating shaft limiting sliding grooves are V-shaped grooves composed of recycling positioning grooves and extending positioning clamping grooves, the front end of the supporting plate is rotationally connected with the rotating shaft A, the middle of the supporting plate is fixedly connected with the pin shaft B, and the rear end of the supporting plate is fixedly connected with the pin shaft. The rotating shaft A is connected with the left baffle and the right baffle, the pin shaft B extends out of the rotating shaft limiting sliding groove, the pin shaft B is in clamping fit with the extending positioning clamping groove, and the pin shaft is in clamping fit with the pin shaft limiting clamping groove. The unmanned aerial vehicle launching device has the advantages of being good in unmanned aerial vehicle supporting effect, high in launching safety, capable of avoiding overlarge resistance and the like.

    本发明公开了一种无人机发射固定装置,包括无人机固定架、支撑板、锁紧座、转轴A、销轴B、销轴和支撑板弹性复位部,锁紧座上开设有销轴限位卡槽,无人机固定架包括左挡板、右挡板和底板,底板上开设有支撑板凹槽,左挡板下端、右挡板下端与底板固定连接,左挡板、右挡板的中部开设有转轴限位滑槽,转轴限位滑槽为由回收定位槽和伸出定位卡槽组成的V形槽,支撑板的前端与转轴A转动连接,中部与销轴B固定连接,后端与销轴固定连接,转轴A与左挡板、右挡板相连接,销轴B伸出转轴限位滑槽,销轴B与伸出定位卡槽卡紧配合,销轴与销轴限位卡槽卡紧配合,本发明具有无人机支撑效果好、发射安全性高、可避免产生过大阻力等优点。


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    Titel :

    Unmanned aerial vehicle launching fixing device


    Weitere Titelangaben:

    无人机发射固定装置


    Beteiligte:
    SI SHENGWEI (Autor:in) / LI ANGRAN (Autor:in) / WANG TIANYI (Autor:in) / LI DONG (Autor:in) / LU LIANG (Autor:in) / LIU JINGSHANG (Autor:in)

    Erscheinungsdatum :

    2023-02-03


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    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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