Partial dielectric loaded septum polarizer

    公开(公告)号:US10686235B2

    公开(公告)日:2020-06-16

    申请号:US16269907

    申请日:2019-02-07

    申请人: VIASAT, INC.

    摘要: In an example embodiment, a waveguide device comprises: a first common waveguide; a polarizer section, the polarizer section including a conductive septum dividing the first common waveguide into a first divided waveguide portion and a second waveguide divided portion; a second waveguide coupled to the first divided waveguide portion of the polarizer section; a third waveguide coupled to the second divided waveguide portion of the polarizer section; and a dielectric insert. The dielectric insert includes a first dielectric portion partially filling the polarizer section. The conductive septum and the dielectric portion convert a signal between a polarized state in the first common waveguide and a first polarization component in the second waveguide and a second polarization component in the third waveguide.

    True time delay compensation in wideband phased array fed reflector antenna systems

    公开(公告)号:US11165151B2

    公开(公告)日:2021-11-02

    申请号:US16403439

    申请日:2019-05-03

    申请人: VIASAT, INC.

    发明人: Donald L Runyon

    摘要: Systems, devices, and methods for determining and applying true time delay (TTD) values for compensating for free-space path length differences between a phased array and a reflector in wideband communication are disclosed. TTD values are determined for individual and groups of antenna elements in phased array fed reflector (PAFR) antennas based distances from a focal region of the reflector. The distance from the focal region of the reflector and the offset of the phased array from the reflectors focal plane can be used to determine path length differences. Corresponding TTD values for antenna elements are then determined based on the path length difference associated with the antenna elements. Each antenna element can be coupled to a TTD element to provide the corresponding TTD value to the signals received by and generated by the antenna elements of the phased array. The TTD elements include transverse electromagnetic (TEM) mode mechanisms.

    Multi-band, dual-polarization reflector antenna

    公开(公告)号:US10096906B2

    公开(公告)日:2018-10-09

    申请号:US15059214

    申请日:2016-03-02

    申请人: VIASAT, INC.

    IPC分类号: H01Q15/16 H01Q5/55 H01P5/12

    摘要: An antenna may include a reflector and a multi-band feed assembly. A support member may be coupled to the multi-band feed assembly to orient the multi-band feed assembly for direct illumination of the reflector. The multi-band feed assembly may include first and second feeds, each having a respective septum polarizer coupled between a respective common waveguide and a respective pair of waveguides. A housing of the support member may contain the respective septum polarizers and the respective pairs of waveguides.

    Dual-circular polarized antenna system
    6.
    发明授权
    Dual-circular polarized antenna system 有权
    双圆极化天线系统

    公开(公告)号:US09184482B2

    公开(公告)日:2015-11-10

    申请号:US14622430

    申请日:2015-02-13

    申请人: VIASAT, INC.

    摘要: In an example embodiment, an azimuth combiner comprises: a septum layer comprising a plurality of septum dividers; first and second housing layers attached to first and second sides of the septum layer; a linear array of ports on a first end of the combiner; wherein the first and second housing layers each comprise waveguide H-plane T-junctions; wherein the waveguide T-junctions can be configured to perform power dividing/combining; and wherein the septum layer evenly bisects each port of the linear array of ports. A stack of such azimuth combiners can form a two dimensional planar array of ports to which can be added a horn aperture layer, and a grid layer, to form a dual-polarized, dual-BFN, dual-band antenna array.

    摘要翻译: 在示例实施例中,方位组合器包括:隔膜层,包括多个隔膜分隔件; 第一和第二壳体层附接到隔膜层的第一和第二侧; 在组合器的第一端上的端口的线性阵列; 其中所述第一和第二壳体层各自包括波导H平面T形接头; 其中所述波导T形结可以被配置为执行功率分配/组合; 并且其中所述隔膜层将所述线性阵列阵列的每个端口均匀地平分。 这种方位组合器的堆叠可以形成端口的二维平面阵列,其可以添加喇叭孔径层和栅格层,以形成双极化双BFN双频天线阵列。

    True time delay compensation in wideband phased array fed reflector antenna systems

    公开(公告)号:US10333218B2

    公开(公告)日:2019-06-25

    申请号:US15162428

    申请日:2016-05-23

    申请人: VIASAT, INC.

    发明人: Donald L Runyon

    摘要: Systems, devices, and methods for determining and applying true time delay (TTD) values for compensating for free-space path length differences between a phased array and a reflector in wideband communication are disclosed. TTD values are determined for individual and groups of antenna elements in phased array fed reflector (PAFR) antennas based distances from a focal region of the reflector. The distance from the focal region of the reflector and the offset of the phased array from the reflectors focal plane can be used to determine path length differences. Corresponding TTD values for antenna elements are then determined based on the path length difference associated with the antenna elements. Each antenna element can be coupled to a TTD element to provide the corresponding TTD value to the signals received by and generated by the antenna elements of the phased array. The TTD elements include transverse electromagnetic (TEM) mode mechanisms.

    Methods and systems for mitigating interference with a nearby satellite

    公开(公告)号:US10135126B2

    公开(公告)日:2018-11-20

    申请号:US15165539

    申请日:2016-05-26

    申请人: VIASAT, INC.

    摘要: In one embodiment, an antenna system is described. The antenna system includes a primary antenna on an aircraft. The primary antenna is mechanically steerable and has an asymmetric antenna beam pattern with a narrow beamwidth axis and a wide beamwidth axis at boresight. The antenna system also includes a secondary antenna on the aircraft, the secondary antenna including an array of antenna elements. The antenna system also includes an antenna selection system to control communication of a signal between the aircraft and a target satellite via the primary antenna and the secondary antenna. The antenna selection system switches communication of the signal from the primary antenna to the secondary antenna when an amount of interference with an adjacent satellite reaches a threshold due to the wide beamwidth axis of the asymmetric antenna beam pattern.