The embodiment of the invention relates to an aircraft wing device. The aircraft wing device comprises a shell, a wing body pneumatic center adjusting assembly, a wing body assembly, a linear potentiometer and a cover body, the shell comprises a shell body and a sliding rail located on the inner side wall of the shell body. The wing body pneumatic center adjusting assembly comprises a wing body unfolding pushing component and a wing body unfolding angle adjusting component. The wing body unfolding pushing component and the wing body unfolding angle adjusting component are symmetrically arranged at the two ends of the shell body. The wing body assembly comprises a wing body mounting seat and a wing body; the wing body mounting base comprises a wing body mounting base body and a sliding groove formed in the side face of the wing body mounting base body. The sliding grooves are matched and connected with the sliding rails. The group of wing bodies are arranged at the top of the wing body mounting seat body; sliding columns are arranged at the front edges of the wing bodies; the linear potentiometer is arranged on the side face of the wing body mounting base body, located below the sliding groove and used for monitoring the axial position of the wing body; the cover body is arranged at the top of the wing body, and a slideway is arranged on the bottom face of the cover body and connected with the sliding column in a matched mode.

    本发明实施例涉及一种飞行器翼装置,包括:壳体、翼体气动中心调节组件、翼体组件、线性电位计和盖体;壳体包括壳体本体,以及位于壳体本体的内侧壁的滑轨;翼体气动中心调节组件包括翼体展开推动部件和翼体展开角度调节部件;翼体展开推动部件和翼体展开角度调节部件对称设置在壳体本体的两端;翼体组件包括翼体安装座和翼体;翼体安装座包括翼体安装座本体和设置在翼体安装座本体的侧面的滑槽;滑槽与滑轨配合连接;一组翼体设置在翼体安装座本体的顶部;翼体的前缘具有滑柱;线性电位计设置在翼体安装座本体的侧面且位于滑槽的下方,用于监测翼体的轴向位置;盖体设置在翼体的顶部,盖体的底面具有滑道,滑道和滑柱配合连接。


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Aircraft wing device, unmanned aerial vehicle and patrolling bomb


    Weitere Titelangaben:

    一种飞行器翼装置、无人机和巡飞弹


    Beteiligte:
    LI PENG (Autor:in) / ZHANG PENGCHENG (Autor:in) / LIU CHANG (Autor:in) / LIU HUAIZHE (Autor:in) / WANG YUNZHAO (Autor:in) / WANG JIANGANG (Autor:in)

    Erscheinungsdatum :

    2023-07-04


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / F42B EXPLOSIVE CHARGES, e.g. FOR BLASTING , Explosive Ladungen, z.B. für Sprengungen



    Fixed-wing unmanned aerial vehicle for patrolling flight

    BAI YALEI / YANG BONING / LI CHAOJIE et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    Composite guidance self-destruction patrolling fixed-wing unmanned aerial vehicle

    LIU ZHENGXU / XIONG YIFA / LI RUIJING et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    Unmanned aerial vehicle guided bomb device

    LI ZHE / WU DAN | Europäisches Patentamt | 2022

    Freier Zugriff

    Cylinder-type launched rotor-wing patrolling bomb and working method thereof

    XU KAI / WANG LIN / XU LEILEI et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    Unmanned aerial vehicle rainfall bomb hanging device

    LIAO XIAOXIA / MA CHUNGUANG / HUANG XIA | Europäisches Patentamt | 2024

    Freier Zugriff