Mechanism analysis and suppression of the outlet pressure rise of the large flux pressure reducing valve
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摘要: 大流量气调式气体减压器是飞行器地面试验系统的关键设备,针对减压器在大流量长程试验过程中出现的出口压力上漂问题进行了建模分析、控制系统设计与试验验证。对减压器活动组件进行力学分析,建立活动组件稳态工作模型,分析得到由于气源压力下降导致了减压器出口压力上漂,并可以通过调节控制腔压力的方式加以抑制。基于可编程逻辑控制器(PLC)设计了一套压力反馈式控制系统,通过传感器采集出口压力信号,并利用带有高速电磁阀的增压罐对控制腔气体压力进行调节,实现了对出口压力的自动稳定控制。在16~27kg/s的气体质量流量下,长程试验结果表明,该控制系统工作稳定可靠,成功地抑制了减压器出口压力的上漂。Abstract: The large flux pressure reducing valve (PRV) is a key part of the aircraft ground testing system. The problem of outlet pressure rise of the PRV is tackled in this paper by modeling analysis, control system design and experimental verification. First, the force analysis of the PRV kinetic components is conducted, which is utilized to establish the steady working model. It is observed from the expression that the sustaining decrease of the inlet pressure can cause the rise of the outlet pressure and the influence factors of the PRV outlet pressure is obtained. This problem can be solved by adjusting the control chamber pressure. Second, the control system framework is constructed based on Programmable Logic Controller (PLC). The outlet pressure feedback control is conducted by acquiring the outlet pressure signal via sensors and adjusting control chamber pressure using the booster jar with high-speed solenoid valves. At last, a series of long-term experiments of 30~60 seconds are designed to test the feasibility of the control system at a large mass flow rate of 16~27kg/s. Results show that this control system effectively stabilizes the outlet pressure and successfully solves the outlet pressure rise problem in the testing process.
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图 3 入口管路、入口腔、卸荷腔压力曲线[19]
Fig. 3 The pressure variation of the inlet pipe, inlet chamber and unloading chamber
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[1] 郑丽, 李清廉, 沈赤兵.大流量气体减压器响应特性的仿真研究[J].火箭推进, 2008, 34(2):18-23. http://www.cnki.com.cn/Article/CJFDTOTAL-HJTJ200802005.htm Zheng L, Li Q L, Shen C B. Analysis on responding characteristics of large flux pressure reducing valve[J]. Journal of Rocket Propulsion, 2008, 34(2):18-23. http://www.cnki.com.cn/Article/CJFDTOTAL-HJTJ200802005.htm
[2] 祝汝松, 汤更生, 陈志强, 等.燃烧加热器气动阀门阀后压力的模糊控制[J].实验流体力学, 2010, 24(1):89-94. http://www.syltlx.com/CN/abstract/abstract9788.shtml Zhu R S, Tang G S, Chen Z Q, et al. The fuzzy control of pressure after the air-driven valve in combustion heater[J]. Journal of Experiments in Fluid Mechanics, 2010, 24(1):89-94. http://www.syltlx.com/CN/abstract/abstract9788.shtml
[3] 王宣银, 陈奕泽, 刘荣, 等.超高压气动比例减压阀的设计与仿真研究[J].浙江大学学报(工学版), 2005, 39(5):614-617. http://www.cnki.com.cn/Article/CJFDTOTAL-ZDZC200505005.htm Wang X Y, Chen Y Z, Liu R, et al. Design and simulation of pneumatic proportional extra high pressure valve[J]. Journal of Zhejiang University(Engineering Science), 2005, 39(5):614-617. http://www.cnki.com.cn/Article/CJFDTOTAL-ZDZC200505005.htm
[4] 黄知龙, 徐大川, 张国彪.大型暂冲式风洞调压阀设计与特性实验[J].实验流体力学, 2012, 26(6):87-90, 95. http://www.syltlx.com/CN/abstract/abstract10484.shtml Huang Z L, Xu D C, Zhang G B. Aerodynamic design and characteristic test of large intermittent wind tunnel control value[J]. Journal of Experiments in Fluid Mechanics, 2012, 26(6):87-90, 95. http://www.syltlx.com/CN/abstract/abstract10484.shtml
[5] 胡长喜.反向卸荷式减压阀动态建模与仿真[J].火箭推进, 2014, 40(1):60-64. http://www.cnki.com.cn/Article/CJFDTOTAL-HJTJ201401010.htm Hu C X. Dynamic modeling and simulation for converse unloading pressure reducing valve[J]. Journal of Rocket Propulsion, 2004, 19(4):541-545. http://www.cnki.com.cn/Article/CJFDTOTAL-HJTJ201401010.htm
[6] 俞笑, 孙兵, 林贵平, 等.逆向式氧气减压器的性能分析与仿真[J].计算机仿真, 2009, 26(11):89-93. http://www.cnki.com.cn/Article/CJFDTOTAL-JSJZ200911026.htm Yu X, Sun B, Lin G P, et al. Simulation and analysis of reverse-type pressure regulator[J]. Computer Simulation, 2009, 26(11):89-93. http://www.cnki.com.cn/Article/CJFDTOTAL-JSJZ200911026.htm
[7] 张青松, 张振鹏, 杨雪, 等.液体火箭发动机试验台气液管路系统故障仿真及分析[J].航空动力学报, 2006, 21(2):403-409. http://www.cnki.com.cn/Article/CJFDTOTAL-HKDI200602030.htm Zhang Q S, Zhang Z P, Yang X, et al. Fault simulation and analysis for the fluid systems of LPRE Test-Bed[J]. Journal of Aerospace Power, 2006, 21(2):403-409. http://www.cnki.com.cn/Article/CJFDTOTAL-HKDI200602030.htm
[8] Afshari H H, Zanj A, Novinzadeh A B. Dynamic analysis of a nonlinear pressure regulator using bondgraph simulation technique[J]. Simulation Modeling Practice and Theory, 2000, 18:240-252. https://www.researchgate.net/publication/220675054_Dynamic_analysis_of_a_nonlinear_pressure_regulator_using_bondgraph_simulation_technique
[9] Ciraolo G, Ferreri G B. Mathematical modeling of pressure oscillationsin sewer pressurization[C]. 11th International Conference on Urban Drainage, Scotland, 2008.
[10] 尹文娟, 魏延明.减压阀动态响应特性与稳定性研究[J].空间控制技术与应用, 2013, 39(3):24-29, 35. http://www.cnki.com.cn/Article/CJFDTOTAL-KJKZ201303004.htm Yin W J, Wei Y M. On response characteristic and stability of pneumatic pressure-reducing valve[J]. Aerospace Control and Application, 2013, 39(3):24-29, 35. http://www.cnki.com.cn/Article/CJFDTOTAL-KJKZ201303004.htm
[11] 罗强, 刘聪聪, 樊蕾, 等.反向式气体减压阀静态特性仿真分析[J].阀门, 2015, (3):8-11. http://www.cnki.com.cn/Article/CJFDTOTAL-FAME201503004.htm Luo Q, Liu C C, Fan Lei, et al. Simulation analyses on static characteristics of reverse pressure reducing valve[J]. Valve, 2015, (3):8-11. http://www.cnki.com.cn/Article/CJFDTOTAL-FAME201503004.htm
[12] 谭建国, 江燕平, 王振国.减压器增压过程中的振荡抑制措施[J].推进技术, 2013, 34(1):124-129. http://www.cnki.com.cn/Article/CJFDTOTAL-TJJS201301025.htm Tan J G, Jiang Y P, Wang Z G. Suppression approach on oscillation of pressure relief valve during pressurization process[J]. Journal of Propulsion Technology, 2013, 34(1):124-129. http://www.cnki.com.cn/Article/CJFDTOTAL-TJJS201301025.htm
[13] 江燕平.气体减压器动态特性的仿真和试验研究[D].长沙:国防科学技术大学, 2009. Jiang Y P, Experiment and simulation research on the dynamic charateristics of gas pressure reducing valve[D]. Changsha:National University of Defense Technology, 2009.
[14] 罗泽明, 郑丽.基于数值模拟的大流量减压器内部流场的特性研究[J].航空计算技术, 2010, 40(2):18-20. http://www.cnki.com.cn/Article/CJFDTOTAL-HKJJ201002006.htm Luo Z M, Zheng L. Analysis on characteristics of flow field of large flux pressure reducing valve based on numerical simulation[J]. Aeronautical Computing Technique, 2010, 40(2):18-20. http://www.cnki.com.cn/Article/CJFDTOTAL-HKJJ201002006.htm
[15] 赖林, 李清廉, 郑丽, 等.大流量气体减压器振动问题研究[J].国防科技大学学报, 2009, 31(2):1-4. http://www.cnki.com.cn/Article/CJFDTOTAL-GFKJ200902002.htm Lai L, Li Q L, Zheng L, et al. Research of vibration failure of the large flux PRV[J]. Journal of National University of Defense Technology, 2009, 31(2):1-4. http://www.cnki.com.cn/Article/CJFDTOTAL-GFKJ200902002.htm
[16] 曹泰岳.火箭发动机动力学[M].长沙:国防科技大学出版社, 2004. [17] 郑丽, 李清廉, 于向财, 等.减压器动态特性试验与仿真研究[J].航空发动机, 2009, 35(2):40-43, 29. http://www.cnki.com.cn/Article/CJFDTOTAL-HKFJ200902013.htm Zheng L, Li Q L, Yu X C, et al. Experiment and simulation of dynamic characteristics for decompressor[J]. Aeroengine, 2009, 35(2):40-43, 29. http://www.cnki.com.cn/Article/CJFDTOTAL-HKFJ200902013.htm
[18] 陈阳, 高芳, 张黎辉, 等.减压器动态仿真的有限体积模型[J].推进技术, 2006, 27(1):9-14. http://www.cnki.com.cn/Article/CJFDTOTAL-TJJS200601002.htm Chen Y, Gao F, Zhang L H, et al. Finite volune model for numerical simulation on dynamic process of pressure reducing regulator[J]. Journal of Propulsion Technology, 2006, 27(1):9-14. http://www.cnki.com.cn/Article/CJFDTOTAL-TJJS200601002.htm
[19] 郑丽.大流量减压器的特性研究及内部流场动态仿真[D].长沙:国防科学技术大学, 2007. http://cdmd.cnki.com.cn/article/cdmd-90002-2008098119.htm Zheng L. Of transient flow field of large flux pressure reducing valve[D]. Changsha:National University of Defense Technology, 2007. http://cdmd.cnki.com.cn/article/cdmd-90002-2008098119.htm
[20] 李平, 芮伟, 秦建华, 等. 2m×2m超声速风洞测量系统与运行管理系统研制[J].实验流体力学, 2012, 26(4):96-100. http://www.syltlx.com/CN/abstract/abstract10527.shtml Li P, Rui W, Qin J H, et al. Development of measurement and operation management system in 2m×2m supersonic wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2012, 26(4):96-100. http://www.syltlx.com/CN/abstract/abstract10527.shtml
[21] 韩斐, 宋笔锋, 喻天翔, 等.阀门可靠性技术研究现状和展望[J].机床与液压, 2008, 36(9):138-144, 178. http://www.cnki.com.cn/Article/CJFDTOTAL-JCYY200809048.htm Han F, Song B F, Yu T X, et al. Present state and prospects for valve reliability technique study[J]. Machine Tool & Hydraulics, 2008, 36(9):138-144, 178. http://www.cnki.com.cn/Article/CJFDTOTAL-JCYY200809048.htm
[22] 周平, 陈天毅, 王帆, 等. 8m×6m风洞特大迎角机构控制系统研制[J].实验流体力学, 2011, 25(3):78-81, 96. http://www.syltlx.com/CN/abstract/abstract10663.shtml Zhou P, Chen T Y, Wang F, et al. The control system design of the high attack angle mechanism for the 8m×6m wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2011, 25(3):78-81, 96. http://www.syltlx.com/CN/abstract/abstract10663.shtml
[23] 叶吉成, 肖京平, 李德祥, 等. 8m×6m低速风洞技术改造研究[J].流体力学实验与测量, 2001, 15(3):72-78. http://www.cnki.com.cn/Article/CJFDTOTAL-LTLC200103012.htm Ye J C, Xiao J P, Li D X, et al. Investigation on technical reformation of the 8m×6m low speed wind tunnel[J]. Experiments and Measurements in Fluid Mechanics, 2001, 15(3):72-78. http://www.cnki.com.cn/Article/CJFDTOTAL-LTLC200103012.htm