The invention discloses a design method of an omni-directional missile carrier of a reconnaissance and attack aircraft and the omni-directional missile carrier. A support capable of rotating by a certain range relative to an aircraft body is designed to serve as a bearing structure of the omni-directional missile carrier; a bullet loading mechanism of the omni-directional bullet rack is designed on a turntable mechanism, and the bullet loading mechanism is designed to rotate together with the turntable mechanism; meanwhile, the rotating disc mechanism is designed to be connected to the support through the rotating mechanism, the servo motor drives the rotating disc mechanism to rotate relative to the support, and the launching angle adjustment of the bullet loading mechanism in the plane direction and the three-dimensional direction is achieved. The invention provides a newly developed space omni-directional reconnaissance and attack, effectively solves the universal design of interior decoration and exterior decoration, effectively solves the air defense integrated design, comprehensively solves the technology of reconnaissance and attack and space omni-directional launching, and supports the application of increasing the loading capacity of equipment and weapons in interior decoration or loading large weapons. Therefore, the capability of the omnidirectional reconnaissance and attack integrated airplane is perfected and improved.

    本发明公开了一种察打飞机全向弹架的设计方法及全向弹架,通过设计可以相对于机身转动一定范围的支架作为全向弹架的承载结构;将全向弹架的装弹机构设计在一种转盘机构上,并将装弹机构设计为与转盘机构一起转动;同时,将转盘机构设计为通过转动机构连接在支架上,并且由伺服电机带动转盘机构相对于支架旋转,实现装弹机构在平面和立体方向的发射角度调整。本发明提出新发展的空间全向察打,有效解决内装与外装的通用设计,有效解决防空一体设计,综合解决即察即打且空间全向发射的技术,支持内装增加设备和武器装载量,或者装载大型武器的应用,从而完善和提高全向察打一体飞机的能力。


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    Titel :

    Design method of omni-directional missile carrier of reconnaissance and attack aircraft and omni-directional missile carrier


    Weitere Titelangaben:

    一种察打飞机全向弹架的设计方法及全向弹架


    Beteiligte:
    YANG XI (Autor:in) / TAO WENYING (Autor:in)

    Erscheinungsdatum :

    2022-12-13


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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