The invention relates to the technical field of flight, in particular to a continuously-adjustable circular-truncated-cone-shaped composite material component structure. The continuously-adjustable circular-truncated-cone-shaped composite material component structurally comprises a top shaping and fixing area, a top transition area, a continuously-adjustable operation area, a middle transition area and a bottom shaping and fixing area. Compared with the existing design, the continuous curl deformation effect is achieved through continuous and adjustable operation of the component structure, the radial size change and the axial stroke change of the component structure are achieved, and an important breakthrough is completed in the research of the adjustable aircraft deformation structure.

    本发明涉及飞行技术领域,具体涉及一种连续可调的圆台型复合材料构件结构。所述连续可调的圆台型复合材料构件结构包括顶部定形固定区、顶部过渡区、连续可调运行区、中部过渡区、底部定形固定区。相较于现有设计,本发明通过构件结构连续可调运行以达到连续卷曲变形的效果,实现了构件结构径向尺寸变化及轴向行程变化,在可调节飞行器变形结构的研究上完成了重要突破。


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    Titel :

    Continuously-adjustable circular-truncated-cone-shaped composite material component structure


    Weitere Titelangaben:

    一种连续可调的圆台型复合材料构件结构


    Beteiligte:
    SUN ZHENG (Autor:in) / WANG WEIHAO (Autor:in) / WANG YAOYAO (Autor:in) / SHAN XUEHAO (Autor:in) / YUAN ZHICHAO (Autor:in) / LIU JIALE (Autor:in)

    Erscheinungsdatum :

    23.02.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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