- 专利标题: ELECTRIC POWER SYSTEM FOR A SPACE VEHICLE
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申请号: US15348413申请日: 2016-11-10
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公开(公告)号: US20180131192A1公开(公告)日: 2018-05-10
- 发明人: Gregory I Rozman , Michael Anthony Futrell
- 申请人: Hamilton Sundstrand Corporation
- 申请人地址: US NC Charlotte
- 专利权人: Hamilton Sundstrand Corporation
- 当前专利权人: Hamilton Sundstrand Corporation
- 当前专利权人地址: US NC Charlotte
- 主分类号: H02J3/38
- IPC分类号: H02J3/38 ; H02J3/36 ; H02J3/14 ; H02J9/06 ; B64G1/42 ; B64G1/44
摘要:
An electrical power system may comprise a first plurality of power sources, a first collector bus configured to receive power from the plurality of power sources, an unregulated DC bus configured to receive power from the first collector bus, a regulated high voltage direct current (HVDC) bus configured to receive power from the unregulated DC bus, and a first power distribution unit (PDU) configured to receive power from the regulated HVDC bus. The regulated HVDC bus may be configured to supply power to a high voltage load. The first plurality of power sources may comprise a first solar array, a first supercapacitor, and/or a first battery.
公开/授权文献
- US10103549B2 Electric power system for a space vehicle 公开/授权日:2018-10-16
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