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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：US09532235B1
公开(公告)日：2016-12-27
申请号：US14927801
申请日：2015-10-30
申请人： The Boeing Company
发明人： Michael A. Whelan
CPC分类号： H04W16/28 , H04B7/18513 , H04B7/18515
摘要： A spacecraft, having a satellite receiver, that is configured so that the direction of the downlink beams transmitted from the satellite receiver depends on the location of the uplink signals transmitted from the ground and not the attitude of the spacecraft in space.
摘要翻译： 具有卫星接收机的航天器被配置为使得从卫星接收机发射的下行链路波束的方向取决于从地面发射的上行链路信号的位置，而不是航天器在空间中的姿态。
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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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4.发明授权Method and apparatus for improving leakage performance of a multi-port amplifier 有权改善多端口放大器泄漏性能的方法和装置公开(公告)号：US09319000B2
公开(公告)日：2016-04-19
申请号：US13955664
申请日：2013-07-31
申请人： The Boeing Company
发明人： Michael A. Whelan
摘要： A method and apparatus for managing a multi-port amplifier. In one illustrative embodiment, an apparatus comprises the multi-port amplifier and a controller. The multi-port amplifier is configured to amplify a plurality of signals to form a plurality of amplified signals. The controller is configured to send a plurality of control adjustments to a plurality of equalizers in the multi-port amplifier to improve leakage performance of the multi-port amplifier.
摘要翻译： 一种用于管理多端口放大器的方法和装置。 在一个说明性实施例中，一种装置包括多端口放大器和控制器。 多端口放大器被配置为放大多个信号以形成多个放大信号。 控制器被配置为向多端口放大器中的多个均衡器发送多个控制调整以改善多端口放大器的泄漏性能。
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公开(公告)号：US20150207465A1
公开(公告)日：2015-07-23
申请号：US14158553
申请日：2014-01-17
申请人： The Boeing Company
CPC分类号： H03F3/21 , F28D15/0266 , H01L23/427 , H01L2924/0002 , H03F2200/447 , H01L2924/00
摘要： In one aspect a satellite comprises a body, a solid state power amplifier, a heat acquisition and transfer device positioned proximate at least one heat generating element on the solid state power amplifier, and a heat rejection device in thermal communication with the heat acquisition and transfer device to reject heat acquired from the solid state power amplifier. Other aspects may be described.
摘要翻译： 在一个方面，卫星包括主体，固态功率放大器，靠近固态功率放大器上的至少一个发热元件定位的热采集和传输装置，以及与热采集和传输热连通的散热装置 用于排除从固态功率放大器获取的热量的装置。 可以描述其它方面。
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6.发明申请Method and Apparatus for Improving Leakage Performance of a Multi-Port Amplifier 有权提高多端口放大器泄漏性能的方法和装置公开(公告)号：US20150035594A1
公开(公告)日：2015-02-05
申请号：US13955664
申请日：2013-07-31
申请人： The Boeing Company
发明人： Michael A. Whelan
摘要： A method and apparatus for managing a multi-port amplifier. In one illustrative embodiment, an apparatus comprises the multi-port amplifier and a controller. The multi-port amplifier is configured to amplify a plurality of signals to form a plurality of amplified signals. The controller is configured to send a plurality of control adjustments to a plurality of equalizers in the multi-port amplifier to improve leakage performance of the multi-port amplifier.
摘要翻译： 一种用于管理多端口放大器的方法和装置。 在一个说明性实施例中，一种装置包括多端口放大器和控制器。 多端口放大器被配置为放大多个信号以形成多个放大信号。 控制器被配置为向多端口放大器中的多个均衡器发送多个控制调整以改善多端口放大器的泄漏性能。
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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：US09590573B2
公开(公告)日：2017-03-07
申请号：US14158553
申请日：2014-01-17
申请人： The Boeing Company
IPC分类号： H03F3/04 , H03F3/21 , H01L23/427 , F28D15/02
CPC分类号： H03F3/21 , F28D15/0266 , H01L23/427 , H01L2924/0002 , H03F2200/447 , H01L2924/00
摘要： In one aspect a satellite comprises a body, a solid state power amplifier, a heat acquisition and transfer device positioned proximate at least one heat generating element on the solid state power amplifier, and a heat rejection device in thermal communication with the heat acquisition and transfer device to reject heat acquired from the solid state power amplifier. Other aspects may be described.
摘要翻译： 在一个方面，卫星包括主体，固态功率放大器，靠近固态功率放大器上的至少一个发热元件定位的热采集和传输装置，以及与热采集和传输热连通的散热装置 用于排除从固态功率放大器获取的热量的装置。 可以描述其它方面。
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