Antenna elements for a missile
    1.
    发明授权
    Antenna elements for a missile 失效
    天线元素为导弹

    公开(公告)号:US07030820B2

    公开(公告)日:2006-04-18

    申请号:US10475488

    申请日:2002-04-25

    申请人: Axel Stiller

    发明人: Axel Stiller

    IPC分类号: H01Q1/28

    CPC分类号: H01Q13/085 F41G7/306

    摘要: The invention relates to antenna elements for the UHF and VHF range for antennas of an airborne vehicle with empennage parts. These antenna elements are integrated into the empennage parts (L) which are made of a dielectric material and are configured in such a way that they radiate directionally broadband in flight direction. The empennage parts are made, for example, of ceramic, and the antenna elements are embedded therein or are applied to their surface.The antenna elements (A) are preferably expanding Vivaldi-type slot radiators that are halved along their axis of symmetry and use the airborne vehicle (F) as an electrical mirror.Arranging the antenna elements in the area of the rudder maximizes both the aperture and the distance between the phase centers of the individual elements, but no additional volume is required for the antennas.

    摘要翻译: 本发明涉及用于具有尾翼部件的机载车辆的天线的UHF和VHF范围的天线元件。 这些天线元件集成到由电介质材料制成的尾翼部件(L)中,并且被配置成使得它们在飞行方向上辐射定向宽带。 尾翼部件例如由陶瓷制成,并且天线元件嵌入其中或施加到其表面。 天线元件(A)优选是扩展的Vivaldi型槽式散热器,其沿其对称轴线减半,并使用机载车辆(F)作为电反射镜。 在方向舵区域内布置天线元件使孔径和各个元件的相位中心之间的距离最大化,但是天线不需要额外的体积。