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    • 1. 发明授权
    • Array antenna including a monolithic antenna feed assembly and related methods
    • 阵列天线包括单片天线馈电组件及相关方法
    • US07038625B1
    • 2006-05-02
    • US11035533
    • 2005-01-14
    • Robert C. TaylorWilliam F. CroswellRonald J. Hash
    • Robert C. TaylorWilliam F. CroswellRonald J. Hash
    • H01Q1/38
    • H01Q21/0006H01L2223/6677H01Q21/0093H01Q21/062
    • An antenna includes antenna elements, an antenna feed assembly and at least one integrated circuit adjacent the antenna feed assembly on a side thereof opposite the antenna elements. The at least one integrated circuit is connected to the antenna elements via the antenna feed assembly. The antenna feed assembly includes a conductive base plate spaced from the antenna elements, and has feed openings therein. Spaced apart conductive posts are integrally formed with the conductive base plate as a monolithic unit, and extend outwardly therefrom toward the antenna elements. Each conductive post has at least one passageway therethrough aligned with at least one respective feed opening to define at least one antenna feed passageway. A respective elongated feed conductor extends through each antenna feed passageway.
    • 天线包括天线元件,天线馈送组件和与天线元件相对的一侧与天线馈送组件相邻的至少一个集成电路。 所述至少一个集成电路经由所述天线馈送组件连接到所述天线元件。 天线馈送组件包括与天线元件间隔开的导电基板,并且其中具有馈电开口。 间隔开的导电柱与导电基板一体地形成为单片单元,并从其向外延伸到天线元件。 每个导电柱具有与至少一个相应进料口对准的至少一个通道,以限定至少一个天线进料通道。 相应的细长进给导体延伸穿过每个天线馈送通道。
    • 3. 发明授权
    • Enhanced bandwidth single layer current sheet antenna
    • 增强带宽单层电流片天线
    • US06552687B1
    • 2003-04-22
    • US10052288
    • 2002-01-17
    • James J. RawnickTimothy E. DurhamWilliam F. Croswell
    • James J. RawnickTimothy E. DurhamWilliam F. Croswell
    • H01Q138
    • H01Q9/285H01Q1/38H01Q5/42H01Q21/062H01Q21/22
    • The invention concerns an array of radiating elements. A first plurality of antenna elements in a first plane in an array configuration is configured for operating on a first band of frequencies. A second plurality of planar antenna elements in an array configuration is configured for operating on a second frequency band, the second plurality of antenna elements is also positioned in the first plane. A first effective ground plane is provided for the first plurality of antenna elements and a second effective ground plane is provided for the second plurality of antenna elements. A first spacing between the first plurality of elements and the first effective ground plane is different from a second spacing between the second plurality of elements and the second effective ground plane. According to one embodiment, the second plurality of elements are adjacent to one another in a unitary cluster that is disposed within the first plurality of elements.
    • 本发明涉及辐射元件阵列。 阵列配置的第一平面中的第一多个天线元件被配置为在第一频带上进行操作。 阵列配置中的第二多个平面天线元件被配置为在第二频带上操作,第二多个天线元件也位于第一平面中。 为第一多个天线元件提供第一有效接地平面,并且为第二多个天线元件提供第二有效接地平面。 第一多个元件与第一有效接地平面之间的第一间隔与第二多个元件与第二有效接地平面之间的第二间隔不同。 根据一个实施例,第二多个元件在布置在第一多个元件内的单一群集中彼此相邻。
    • 4. 发明授权
    • Waveguide fed composite horn antenna
    • 波导馈电复合喇叭天线
    • US4700195A
    • 1987-10-13
    • US782550
    • 1985-10-01
    • Bobby J. BoanWilliam F. Croswell
    • Bobby J. BoanWilliam F. Croswell
    • H01Q1/00H01Q13/02H01Q13/00
    • H01Q13/0208H01Q1/002H01Q13/0233Y10S343/02
    • A waveguide-fed horn structure includes a constraining mechanism having an extremely high degree of dimensional stability over a wide thermal range. The constraining mechanism comprises a composite graphite honeycomb structure that forms a support backing for the waveguide feed and for the conductive surface sections of the horn radiator. The conductive surface of the horn radiator is supported on a first section of graphite epoxy laminate while a second section of graphite epoxy laminate supports the honeycomb backing and is bonded to the first section of laminate, thereby effectively surrounding the feed-horn structure with a thermally tolerant, physical distortion constraining support. The graphite epoxy support provides sufficient mass and mechanical stiffness to prevent performance degrading distortion of both the waveguide feed and the horn radiator surface in spite of the severe transient thermal conditions encountered in a spaceborne environment, thereby maintaining structural integrity of the components of the structure during extreme thermal cycling conditions (full sun to no sun).
    • 波导馈电喇叭结构包括在宽的热范围内具有非常高的尺寸稳定性的约束机构。 约束机构包括复合石墨蜂窝结构,其形成用于波导进料和喇叭辐射体的导电表面部分的支撑背衬。 喇叭辐射体的导电表面被支撑在石墨环氧树脂层压体的第一部分上,而第二部分石墨环氧层压板支撑蜂窝背衬并结合到层压板的第一部分,由此有效地围绕馈电喇叭结构 容忍,物理失真约束支持。 石墨环氧树脂支撑体提供足够的质量和机械刚度,以防止波导进料和喇叭辐射体表面的性能降低,尽管在空间环境中遇到严重的瞬态热条件,从而保持结构的部件的结构完整性 极端的热循环条件(全太阳到无太阳)。