|Table of Contents|

Research on the turbo-pump performance under ultra--low operation condition(PDF)

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

Issue:
2008年03期
Page:
13-16
Research Field:
研究与设计
Publishing date:

Info

Title:
Research on the turbo-pump performance under ultra--low operation condition
Author(s):
Bai Dong'an
Xi'an Aerospace Propulsion Institute,Xi'an 710100,China
Keywords:
turbo-pumpvariable conditionsperformance research
PACS:
V434.21
DOI:
-
Abstract:
The capability of turbo-pump working in variable conditions is required and important for pump—pressurized variable thrust rocket engine and ramjet propulsion.Combining with a test of the upper stage rocket engine,the performance and stability of the turbo-pump at low condition are studied in this paper.Through the full flow characteristic and cavitation tests of pump,it is con— eluded that the pump can work stably in 25%rated flow condition.The analyses of gas parameter, inlet pressure,outlet pressure and efficiency of turbo under varied conditions indicated that the turbo can also work stably.The conclusions made above age verified by engine test.

References:

[1]阿列玛索夫B E.火箭发动机原理[M].北京:机械工业 出版社.1989.
[2]黄智勇,李晶奂,黄红.高工况涡轮泵轴系状态对工作可 靠性的影响[J].火箭推进,2007,33(1):32—35.
[3]沃尔科夫E B.火箭发动机静、动力学[M].北京:机械工 业出版社.1978.
[4]奥夫夏尼科夫B B.高转速叶片泵咖.北京:机械工业出 版社。1975.
[5]莫什金E K.液体火箭发动机动力学过程[M].北京:机 械工业出版社.1964.
[6]严俊峰,陈炜.基于遗传算法的低比转速高速泵优化设 计[J].火箭推进,2006,32(3):1-7.

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Last Update: 1900-01-01