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    • 2. 发明授权
    • Structural wideband multifunctional aperture manufacturing
    • 结构宽带多功能孔径制造
    • US09190727B1
    • 2015-11-17
    • US14043563
    • 2013-10-01
    • The Boeing Company
    • Manny S. UrciaCharles W. Manry, Jr.Joseph A. Marshall, IVTai A. LamOtis F. Layton
    • H01Q1/28H01Q5/00
    • H01Q21/062H01Q1/286H01Q9/28
    • A structural wideband aperture assembly and methods are presented. A non-conductive structural backsheet comprises electrical vias. A structural egg-crate core comprises a grid of core strips coupled to the non-conductive structural backsheet and is configured substantially perpendicular to the non-conductive structural backsheet around open boxes. A non-structural grid of antenna feed cards is configured substantially perpendicular to the non-conductive structural backsheet and crosses the core strips. A non-structural grid of antenna feed cards comprises intersections configured within the open boxes, and electronic feed-lines aligned with the electrical vias. Antenna array unit cells comprising antenna cards coupled to the non-structural grid of antenna feed cards and configured to fit within the open boxes.
    • 提出了一种结构化的宽带孔径组件和方法。 非导电结构底片包括电气通孔。 结构蛋壳芯包括耦合到非导电结构底片的芯条的网格,并且被构造成基本上垂直于围绕打开框的非导电结构底片。 天线馈电卡的非结构网格被配置为基本上垂直于非导电结构底片并且穿过芯条。 天线馈电卡的非结构网格包括配置在开放框内的交叉点,以及与电气通孔对准的电子馈线。 天线阵列单元,其包括耦合到天线馈线卡的非结构网格并且被配置为装配在开放框内的天线卡。
    • 5. 发明授权
    • Ultra wide band antenna element
    • 超宽带天线元件
    • US09099777B1
    • 2015-08-04
    • US13658485
    • 2012-10-23
    • The Boeing Company
    • Charles W. Manry, Jr.
    • H01Q1/24H01Q1/28
    • H01Q1/288H01Q1/286H01Q1/38H01Q5/25H01Q5/385H01Q9/28H01Q21/062H01Q21/26H01Q21/30H01Q25/001
    • Antenna unit cells suitable for use in antenna arrays are disclosed, as are antenna arrays and mounting platform such as an aircraft comprising antenna unit cells. In one embodiment, an antenna unit cell comprises a dielectric substrate having a length extending along a first axis and a width extending along a second axis, a first plurality of radiating elements disposed on a first side of the dielectric substrate, a second plurality of radiating elements disposed on a second side of the dielectric substrate, opposite the first side, a feed pin coupled to at least one of the first plurality of radiating elements, and a shorting pin coupled to each of the first plurality of radiating elements and to a ground plane. Other embodiments may be described.
    • 公开了适用于天线阵列的天线单元电池,天线阵列和诸如包括天线单元电池的飞行器的安装平台也是如此。 在一个实施例中,天线单元包括具有沿着第一轴延伸的长度和沿着第二轴延伸的宽度的电介质基板,设置在电介质基板的第一侧上的第一多个辐射元件,第二多个辐射 设置在所述电介质基板的与所述第一侧相对的第二侧上的元件,耦合到所述第一多个辐射元件中的至少一个辐射元件的馈电引脚,以及耦合到所述第一多个辐射元件中的每一个并连接到地 飞机 可以描述其他实施例。