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公开(公告)号：US10819430B1
公开(公告)日：2020-10-27
申请号：US16801075
申请日：2020-02-25
申请人： The Boeing Company
IPC分类号： H04J14/02 , H04B10/2575 , H04B10/118 , H04B10/27
摘要： A satellite payload system is presented. The system includes plurality of optical processing modules, including a plurality of ring-connected optical processing modules and at least one inter-satellite optical processing module, and at least one optical fiber ring communicatively coupled to each of the ring-connected optical processing modules. At least one of the ring-connected optical processing modules is configured to provide on-board signal processing of signals conveyed on the at least one optical fiber ring. At least one of the ring-connected optical processing modules is communicatively coupled to a respective inter-satellite optical processing module. Each inter-satellite optical processing module is configured to optically communicatively couple to a respective remote satellite.
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公开(公告)号：US10594430B1
公开(公告)日：2020-03-17
申请号：US16392105
申请日：2019-04-23
申请人： The Boeing Company
IPC分类号： H04J14/02 , H04B10/2575 , H04B10/118 , H04B10/27
摘要： A satellite payload system is disclosed. The satellite payload system includes a plurality of optical processing modules, each including: a module input including an optical splitter, a module output including an optical coupler, a dynamic gain equalizer, an output bank of optical filters, and an input bank of optical filters; where the plurality of optical processing modules include ring-connected optical processing modules and inter-satellite optical processing modules; and at least one optical fiber ring communicatively coupled to each of the ring-connected optical processing modules; where at least one of the ring-connected optical processing modules is configured to provide on-board signal processing of wavelengths; where a plurality of the ring-connected optical processing modules are each communicatively coupled to a respective inter-satellite optical processing module; where each inter-satellite optical processing module is configured to optically communicatively couple to a respective remote satellite via its module input and via its module output.
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公开(公告)号：US10483654B2
公开(公告)日：2019-11-19
申请号：US15888196
申请日：2018-02-05
申请人： The Boeing Company
发明人： Paul C. Werntz , Dennis L. Gould , Patrick K. Bailleul , Brian M. Park , Andre C. Houle , Raenaurd D. Turpin
摘要： An antenna platter comprises a plurality of antenna elements arranged as a thin array according to a polygonal grid. The polygonal grid comprises a plurality of paired polygons arranged symmetrically about a central polygon of the grid. In each polygon of the grid, the plurality of antenna elements is arranged in symmetrical pairs about a center point such that the first and second antenna elements of each symmetrical pair are complex conjugates of one another.
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公开(公告)号：US20200343991A1
公开(公告)日：2020-10-29
申请号：US16801075
申请日：2020-02-25
申请人： The Boeing Company
IPC分类号： H04J14/02 , H04B10/27 , H04B10/118 , H04B10/2575
摘要： A satellite payload system is presented. The system includes plurality of optical processing modules, including a plurality of ring-connected optical processing modules and at least one inter-satellite optical processing module, and at least one optical fiber ring communicatively coupled to each of the ring-connected optical processing modules. At least one of the ring-connected optical processing modules is configured to provide on-board signal processing of signals conveyed on the at least one optical fiber ring. At least one of the ring-connected optical processing modules is communicatively coupled to a respective inter-satellite optical processing module. Each inter-satellite optical processing module is configured to optically communicatively couple to a respective remote satellite.
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公开(公告)号：US20190245274A1
公开(公告)日：2019-08-08
申请号：US15888196
申请日：2018-02-05
申请人： The Boeing Company
发明人： Paul C. Werntz , Dennis L. Gould , Patrick K. Bailleul , Brian M. Park , Andre C. Houle , Raenaurd D. Turpin
摘要： An antenna platter comprises a plurality of antenna elements arranged as a thin array according to a polygonal grid. The polygonal grid comprises a plurality of paired polygons arranged symmetrically about a central polygon of the grid. In each polygon of the grid, the plurality of antenna elements is arranged in symmetrical pairs about a center point such that the first and second antenna elements of each symmetrical pair are complex conjugates of one another.
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