Creation and control of hydraulic vibration signal withwide frequency range and high amplitude

刘上; 赵瑞国; 付幼明; 徐云飞; 李龙飞; 程晓辉; 张兴军

doi:10.13224/j.cnki.jasp.2018.10.022

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Creation and control of hydraulic vibration signal withwide frequency range and high amplitude

更新时间：2026-07-07

- Creation and control of hydraulic vibration signal withwide frequency range and high amplitude
- Vol. 33, Issue 10, Pages: 2492-2499(2018)
- 作者机构：
  
  中国航天科技集团有限公司西安航天动力研究所液体火箭发动机技术重点实验室,西安,710100
- 作者简介：
- 基金信息：
- DOI：10.13224/j.cnki.jasp.2018.10.022
  CLC：
- Published：2018
- 稿件说明：
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刘上, 赵瑞国, 付幼明, 徐云飞, 李龙飞, 程晓辉, 张兴军. 宽频高幅值水力激振信号的产生与控制[J]. 航空动力学报, 2018, 33(10): 2492-2499.

doi: 10.13224/j.cnki.jasp.2018.10.022
刘上, 赵瑞国, 付幼明, 徐云飞, 李龙飞, 程晓辉, 张兴军. 宽频高幅值水力激振信号的产生与控制[J]. 航空动力学报, 2018, 33(10): 2492-2499. DOI： 10.13224/j.cnki.jasp.2018.10.022.

doi: 10.13224/j.cnki.jasp.2018.10.022 DOI：

摘要

为了研究火箭发动机全尺寸泵后供应系统的动力学特性

运用脉动压力发生器设计了一种宽频水力激振系统

开展了液流试验和数据分析。结果表明：水力激振系统可以在0~1200Hz的频率范围内

产生时域幅值超过1.5MPa、高信噪比的压力脉动信号

达到了宽频率范围、高激励幅值的目的。通过对电动机转速的控制实现激励频率的可控变化

以满足不同频率激励策略的要求。提高管路系统的入口稳态压力

可以提高激振信号的幅值。通过合适的局部流阻分布

可以在宽频范围内提高水力激振信号的幅值

提高信噪比。

Abstract

A hydraulic vibration system with wide frequency range was designed by using the pulsation generator

in order to study the dynamical characteristics of the full scale propellant feed system after the pump in the liquid rocket engine

and the cold fluid tests and data analysis were conducted. Within the range of 0-1200Hz

the hydraulic vibration system can create pressure fluctuation signal with amplitude more than 1.5MPa and high signal-to-noise ratio. The target of wide frequency range and high amplitude was reached. By controlling the electric motor revolving speed

the controlled excitation frequency can be realized to satisfy different frequency actuating methods. Increasing the system inlet steady pressure can improve the hydraulic vibration signal amplitude. By appropriately distributing local resistors

the hydraulic vibration signal amplitude and signal-to-noise ratio can be improved within widefrequency range.

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Related Institution

北京航空航天大学宇航学院

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Jiangsu Polytechnic University

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