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[1]杜大华,黄金平,邢理想,等.液体火箭发动机泵动态特性水力试验研究[J].火箭推进,2013,39(03):50-57.
　DU Da-hua,HUANG Jin-ping,XING Li-xiang,et al.Hydraulic test research on dynamic characteristics of oxygen pump of liquid rocket engine[J].Journal of Rocket Propulsion,2013,39(03):50-57.
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液体火箭发动机泵动态特性水力试验研究

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V] 卷: 39 期数: 2013年03期 页码: 50-57 栏目: 研究与设计 出版日期: 2013-06-30
Title:
Hydraulic test research on dynamic characteristics of oxygen pump of liquid rocket engine
文章编号:
1672-9374(2013)03-0050-08
作者:
杜大华; 黄金平; 邢理想; 徐浩海
西安航天动力研究所，陕西 西安 710100
Author(s):
DU Da-hua;  HUANG Jin-ping;  XING Li-xiang;  XU Hao-hai
Xi’an Aerospace Propulsion Institute, Xi’an 710100, China
关键词:
水力试验; 泵; 液氧/煤油补燃循环发动机; POGO
分类号:
V434-34
文献标志码:
A
摘要:
为了获取新一代大型运载火箭POGO稳定性分析及液体火箭发动机动力学研究等所必需的发动机泵动力学传递函数，进行了以常温水为试验介质、全尺寸降转速液氧/煤油补燃循环发动机氧泵的动态特性水力试验，对试验原理、试验模拟准则、隔离贮箱设计、激励系统设计、控制和测量分析系统设计、试验内容及数据分析方法等进行了深入探讨。通过试验成功地识别出泵的POGO动特性参数及参数的规律特点，为其他水力试验和真实介质试验储备经验。
Abstract:
In order to obtain the essential dynamic transfer function of the engine pump which is necessary for POGO stability analysis of the new generation large launch vehicle and dynamics research of the liquid rocket engine, a hydraulic test for the dynamic characteristics of a full-scale LOX/kerosene staged combustion cycle engine pump with speed drop-down was conducted, in which normal temperature water is taken as the test medium. The hydraulic test theory, simulation criterion, isolation tank design, exciting system design, control and measurement analysis system design, test details and data analysis method are thoroughly discussed in this paper. The POGO dynamic characteristics parameters and their disciplinarian laws of the oxygen pump were successfully identified through the test, which would be helpful to other hydraulic test and the real medium test.

参考文献/References:

[1]OTSUKA S, TSUJIMOTO Y, KAMIJO K, et al. Frequency dependence of mass flow gain factor and cavitation compliance of cavitating inducers[J]. Journal of Fluids Engineering, 1996 (6): 400-408.
[2]DOTSON K W, RUBIN S, SAKO B H. Effects of unsteady pump cavitation on propulsion-structure interaction (POGO) in liquid rockets, AIAA2004-2027[R]. USA: AIAA, 2004.
[3]RUBIN Sheldon. An interpretation of transfer function data for a cavitating pump, AIAA2004-4025[R]. USA: AIAA, 2004.
[4]SHIMURA Takashi. Geometry effects in the dynamic response of cavitating LE-7 liquid oxygen pump[J]. Journal of Propulsion and Power, 1995 (2): 330-336.
[5]IACOPOZZI M, LIGNAROLO V, PREVEL D. POGO characterization of ARIANE Ⅴ turbopump LOX pump with hot water, AIAA 93-2124[R]. USA: AIAA, 1993.

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[1]刘占一,张魏静,杨建文,等.关键间隙对泵性能影响的研究[J].火箭推进,2015,41(02):56.
　LIU Zhan-yi,ZHANG Wei-jing,YANG Jian-wen,et al.Influence of key clearance on pump performance[J].Journal of Rocket Propulsion,2015,41(03):56.

备注/Memo

收稿日期：2012-08-１３；修回日期：2012-12-06
基金项目：国家863项目（2006AA705311）
作者简介：杜大华（1977—），男，高级工程师，研究领域为火箭发动机动力学研究、结构强度与振动分析

更新日期/Last Update: 1900-01-01