The invention relates to the technical field of aircraft launching, in particular to a guide rail type composite launching device for an aircraft. Comprising a roller guide rail sliding block, a first standard sliding block, a second standard sliding block and a sliding guide rail, the roller guide rail sliding block, the first standard sliding block and the second standard sliding block are sequentially and fixedly connected with an aircraft, and the roller guide rail sliding block is in linear contact with the guide rail and can share the total missile weight borne by the standard sliding block; the multiple faces of the standard sliding block make contact with the guide rail, so that the aircraft can only keep linear sliding acceleration along the guide rail, and it is guaranteed that the aircraft directionally and stably slides on the guide rail in a linear mode. The first standard sliding block and the second standard sliding block are located on the two sides of the gravity center of the aircraft. The roller guide rail sliding block is formed by combining a supporting frame and six rollers, the supporting frame is in an I shape, the middle axial face of the supporting frame serves as the symmetry plane, and the two rows of rollers are distributed at the two ends. According to the invention, the structure and the installation process are simplified, and the reliability and the safety are enhanced.

    本发明涉及飞行器发射技术领域,具体涉及一种飞行器导轨式复合型发射装置。包括滚柱导轨滑块、标准滑块一、标准滑块二及滑行导轨,所述滚柱导轨滑块、标准滑块一及标准滑块二与飞行器依次固定连接,滚柱导轨滑块与导轨实现线接触,能够分担标准滑块所承受的全弹重量,飞行器发射时,标准滑块的多个面与导轨相接触,足够实现飞行器仅能沿导轨保持直线滑行加速,保证飞行器在导轨上定向、稳定直线滑行。所述标准滑块一和标准滑块二位于飞行器重心两侧。所述滚柱导轨滑块由1个支持架和6个滚柱组合而成,支持架为工字型,以支持架中轴面为对称面,两排滚柱分布两端。本发明不仅简化了其结构和安装工艺,而且增强了其可靠性和安全性。


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    Title :

    Aircraft guide rail type composite launching device


    Additional title:

    一种飞行器导轨式复合型发射装置


    Contributors:
    LI YONGSHENG (author) / WANG XIAOLEI (author) / ZHANG PINGSHANG (author) / LIU XIAOPING (author) / SHI YANBO (author) / ZHANG SU (author) / WANG YU (author) / HU YUANXIN (author) / LI LIANG (author)

    Publication date :

    2024-10-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    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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