A device for reducing a bowing angle of a shipboard aircraft traction system is characterized in that a frame left vertical rod is connected with a left connecting lug through a bolt, a frame right vertical rod is connected with a right connecting lug through a bolt, a frame front cross rod is connected with a front guide rail mechanism through a screw, and a frame rear cross rod is connected with a rear guide rail mechanism through a screw. The lower portion of a front transverse rod of the sliding platform is connected with a front guide rail left sliding block and a front guide rail right sliding block through screws, the lower portion of a middle transverse rod of the sliding platform is connected with a left L-shaped connecting lug and a right L-shaped connecting lug through bolts, and the lower portion of a rear transverse rod of the sliding platform is connected with a rear guide rail left sliding block and a rear guide rail right sliding block through screws. A left end cover of the two-way hydraulic cylinder is connected with the left L-shaped connecting lug through a bolt, a right end cover of the two-way hydraulic cylinder is connected with the right L-shaped connecting lug through a bolt, the left end of the hydraulic rod is connected with the left connecting lug through a connecting pin, the right end of the hydraulic rod is connected with the right connecting lug through a connecting pin, and the clamping and lifting reserved platform is installed on the upper side of the sliding platform. The device is simple in structure and high in safety, when the bowing angle of a traction system is too large, the bowing angle can be reduced, and the device has good practical value.

    一种用于减小舰载机牵引系统折腰角的装置,由车架左竖杆与左连接耳通过螺栓连接,车架右竖杆与右连接耳通过螺栓连接,车架前横杆与前导轨机构通过螺钉连接,车架后横杆与后导轨机构通过螺钉连接,滑动平台前横杆下方与前导轨左滑块和前导轨右滑块通过螺钉连接,滑动平台中横杆下方与左L型连接耳和右L型连接耳通过螺栓连接,滑动平台后横杆下方与后导轨左滑块和后导轨右滑块通过螺钉连接,双向液压缸左端盖与左L型连接耳通过螺栓连接,双向液压缸右端盖与右L型连接耳通过螺栓连接,液压杆左端与左连接耳通过连接销连接,液压杆右端与右连接耳通过连接销连接,滑动平台的上侧安装夹持举升预留平台。本发明结构简单,安全性高,在牵引系统折腰角度过大时,可以实现减小折腰角度,具有很好的实用价值。


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    Titel :

    Device for reducing bowing angle of shipboard aircraft traction system


    Weitere Titelangaben:

    一种用于减小舰载机牵引系统折腰角的装置


    Beteiligte:
    LIU HONGBO (Autor:in) / LIN YUZE (Autor:in) / WU JUNCHENG (Autor:in) / YANG XIAODONG (Autor:in) / ZENG ZHAOBIAO (Autor:in) / LI SHUXIN (Autor:in)

    Erscheinungsdatum :

    11.03.2025


    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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