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[1]于海力,张 锐,刘海丽,等.高压高扬程固液两相介质离心泵的设计原则[J].火箭推进,2015,41(02):70-74.
 YU Hai-li,ZHANG Rui,LIU Hai-li,et al.Design philosophy of high-pressure & high-lift centrifugal pump for solid-liquid phase mediums[J].Journal of Rocket Propulsion,2015,41(02):70-74.
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高压高扬程固液两相介质离心泵的设计原则

参考文献/References:

[1]HEINZ P B, ALLAN R B. Pump user's hand book: life extension[M]. 3rd Edition. U.S.A.: The Fairmont Press, INC., 2009.
[2]MATTHEW A G. Addressing pump reliability problems [M]. U.S.A.: Mechanical Solutions Inc., 2006.
[3]JOHANN F G. Centrifugal pumps[M]. 2nd Edition. Ger- many: Springer press, 2010.
[4]KHALID Y A, SAPUAN S M. Wear analysis of centrifugal slurry pump impellers[J]. Industrial Lubrication and Tec- hnology, 2007, 59(1): 18-28.

[5][S.l.] Installation, operation, maintenance and assembly instructions [M]. Australia: Weir Warman, 2000.

[6]何希杰, 劳学苏. 渣浆泵选型方法探讨[J]. 水泵技术,1995(6): 29-35.
[7]卜炎. 机械传动设计手册[M]. 北京: 机械工业出版社,1999.
[8]关醒凡. 现代泵技术手册[M]. 北京: 宇航出版社, 1995.

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备注/Memo

收稿日期:2014-12-17;修回日期:2015-02-05 作者简介:于海力(1978—),男,硕士,高级工程师,研究领域为流体机械

更新日期/Last Update: 1900-01-01