期刊文献+

航天器产品限流电阻保护设计方法研究

Research on Design Method of Current Limiting Resistor Protection for Spacecraft Products
下载PDF
导出
摘要 针对小功率负载的限流电阻保护设计不规范问题,给出了基本设计原则,提出了限流电阻功率接近和远超额定功率2种工况下的详细设计方法,并以3种常用传感器限流电阻保护电路为例,采用不同阻值、同封装,同阻值、不同封装进行试验验证。试验结果表明:该设计方法有效,试验数据对航天器产品限流电阻的选取提供了数据支持。 To solve the non-standard design problem of current-limiting resistance protection for small power load,the basic design principles were given,and the detailed design methods were put forward under two working conditions:the power of current-limiting resistance was close to or far beyond the rated power.Taking three kinds of current-limiting resistance protection circuits for common sensors as examples,different resistance values with the same package and the same resistance value with different packages were used to verify the proposals.The test results showed that the design method was effective and the test data could provide data support for the selection of current limiting resistors of spacecraft products.
作者 王栋 王伟荣 刘向阳 罗亚斌 傅巍 石慧杰 WANG Dong;WANG Weirong;LIU Xiangyang;LUO Yabin;FU Wei;SHI Huijie(China Astronaut Research and Training Center,Beijing 100094,China;The 49thResearch Institute of China Electronics Technology Group,Harbin 150001,China;The 48th Research Institute of China Electronics Technology Group,Changsha 410111,China)
出处 《载人航天》 CSCD 北大核心 2021年第1期113-118,共6页 Manned Spaceflight
关键词 小功率负载 过流保护 限流电阻 烧断倍数 low power load over current protection current limiting resistor burn-out multiple
  • 相关文献

参考文献4

二级参考文献30

  • 1熊晓英,申小存,彭梅,张大鹏.神舟飞船供配电及电缆网设计与研制[J].航天器工程,2004,13(4):34-40. 被引量:7
  • 2Hopkins D C. Current limiting remote power control module,NASA N19-8987[R].{H}Washington,DC:NASA,1990.
  • 3Henze C B,Mohan N,Henze C P. A programmable solid state active current limiting circuit breaker for spaceapplications[A].NewYork:IEEE,2002.2849-2854.
  • 4Komatsu M,Ide N,Yanabu S. A solid state current limiting switch for application of large-scale space powersystems[A].NewYork:IEEE,2007.1471-1476.
  • 5Jin Chunlian,Dougal R. A solid state over current pro tection for industrial DC distribution systems[A].Washington D.C.:AIAA,2006.26-29.
  • 6Hirofumi M,Fujio K,Mutsuyoshi A. Ovecurrent liraiting characteristics of the DC-DC converter with a new digital current injected control circuit[J].Transactions on Power Systems,1998,(04):645-650.
  • 7Dolce J L,Mellor P A,Kish J A. Automated electric power management and control for space station Freedom,NASA TM-103151[R].{H}Washington,DC:NASA,1990.
  • 8Greg C,Frank D. X2000 power system electronics development[A].New York:IEEE,2000.341-354.
  • 9何宇,王林涛,张大鹏.一种载人航天器高压供电系统接地方法[J].航天器工程,2009,18(5):54-60. 被引量:9
  • 10吴旭涛,艾绍贵,李小燕,李勇.35kV电容式电压互感器一次熔断器异常熔断原因的试验研究[J].高压电器,2009,45(6):102-105. 被引量:24

共引文献15

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部