Structurally integrated antenna aperture and fabrication method
    4.
    发明申请
    Structurally integrated antenna aperture and fabrication method 有权
    结构集成天线孔径和制造方法

    公开(公告)号:US20060097945A1

    公开(公告)日:2006-05-11

    申请号:US10970710

    申请日:2004-10-21

    IPC分类号: H01Q9/28

    摘要: A phased array antenna aperture able to form a structural, load bearing portion of another structure, for example, a portion of a mobile platform. The antenna aperture is formed with a plurality of radiating elements sandwiched between prepreg fabric plies to form independent wall sections having a plurality of electromagnetic radiating elements embedded therein. The wall sections are secured in a honeycomb arrangement to form an array of cells of radiating elements. The manufacturing methods described herein enable arrays of widely varying sizes and shapes to be created and used as structural, load bearing portions of a wing, fuselage, door panel or other area of a mobile platform. The antenna aperture is lightweight because it does not include the weight of parasitic support components typically required in the construction of phased array antenna apertures.

    摘要翻译: 相控阵天线孔,其能够形成另一结构的结构承载部分,例如移动平台的一部分。 天线孔径形成有夹在预浸织物层之间的多个辐射元件,以形成具有嵌入其中的多个电磁辐射元件的独立的壁部分。 壁部分固定在蜂窝结构中以形成辐射元件的阵列阵列。 本文描述的制造方法使得可以创建广泛变化的尺寸和形状的阵列,并且用作机翼,机身,门板或移动平台的其它区域的结构,承载部分。 天线孔径是轻量的,因为它不包括在相控阵天线孔径的构造中通常需要的寄生支撑部件的重量。