|Table of Contents|

Effect of hub shape on performance of inducer(PDF)

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]

Issue:
2012年02期
Page:
38-43
Research Field:
研究与设计
Publishing date:

Info

Title:
Effect of hub shape on performance of inducer
Author(s):
SONG Pei-yuan LI Jia-wen TANG Fei
School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
Keywords:
liquid rocket engine inducer hub head of delivery
PACS:
V434-34
DOI:
-
Abstract:
The inducer mounted in front of the centrifugal pump is a key way to ensure the centrifugal pump to achieve the excellent cavitation performance. In allusion to the inducer of a certain liquid rocket engine, CFD technique was adopted for researching the influence of hub shape on the cavitation performance and pumping head of inducer. The results show that, under the condition of the same inlet flow, changing the inducer-hub shape can make the inducer to generate the different pumping head.

References:

[1]HASHIMOTO T, YOSHIDA M W. Experimental study on rotating cavitation of rocket propellant pump inducers[J]. Journal of Propulsion and Power 1997, 13 (4 ): 488-494.
[2]HASHIMOTO T, YAMADA H, FUNATSU S. Rotating cavitation in three and four-bladed inducers [C]// Proceedings of 33rd AIAA/ASME/SAE/ASEE Joint Propul- sion Conference and Exhibit. Seattle, WA: AIAA, 1997: 111-119.
[3]BAKIR F,KOUIDRI S, NOUGUERA R. Experimental analysis of an axial inducer influence of the shape of the blade leading edge on the performance in cavitating regine[J]. Journal of Fluids Engineering, 2003, 125: 293-301.
[4]SEMENOV Y, FUJII A, TSUJIMOTO Y. Rotating choke in cavitating turbopump inducer transations of the ASME[J]. Journal of Fluids Engineering, 2004, 126: 87-93.
[5]黄建德, 谷传纲. 诱导轮形状对汽蚀特性的影响[J]. 航空动力学报, 2000, 15(2): 31-35.
[6]J K 杰科布森. 液体火箭发动机涡轮泵诱导轮[M]. 傅轶青, 陈炳贵, 译. 北京: 国防工业出版社, 1976.
[7]李向阳, 王晓锋. 液氧/煤油发动机煤油预压涡轮泵技术[J]. 火箭推进, 2009, 35(1): 21-24.
[8]WATANABE Satoshi, KIM Jun-Ho. Numerical/experi- mental investigations on inlet back flow in a helical inducer in partial flow conditions[C]// Proceedings of ASME/JSME Fluids Engineering Conference. San Diego, California, USA: ASME, 2007: 893-898.
[9] 唐飞, 李家文, 陈晖, 等. 采用环形入口壳体的诱导轮汽蚀性能研究[J]. 机械工程学报, 2011 (4): 171-176.
[10] 李斌, 栾希亭, 张小平. 载人登月主动力--大推力液氧煤油发动机研究[J]. 载人航天, 2011 (1): 28-33.
[11] 张民庆, 张蒙正, 毛根旺. 某型液体火箭发动机燃烧不稳定性鉴定实验研究[J]. 航空工程进展, 2011 (2): 226-230.
[12] 窦唯. 液体火箭发动机用过滤器流阻特性及试验[J]. 导弹与航天运载技术, 2011 (1): 10-13.

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Last Update: 1900-01-01