航天推进技术研究院主办
[1]魏京芳,刘 军,孙海智,等.液氧煤油发动机步进电机测控仪设计与应用[J].火箭推进,2020,46(03):68-74.
WEI Jingfang,LIU Jun,SUN Haizhi,et al.Design and application of stepper motor measurement and controlling instrument for LOX/kerosene rocket engine[J].Journal of Rocket Propulsion,2020,46(03):68-74.
点击复制
WEI Jingfang,LIU Jun,SUN Haizhi,et al.Design and application of stepper motor measurement and controlling instrument for LOX/kerosene rocket engine[J].Journal of Rocket Propulsion,2020,46(03):68-74.
液氧煤油发动机步进电机测控仪设计与应用
《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]
卷:
46
期数:
2020年03期
页码:
68-74
栏目:
研究与设计
出版日期:
2020-06-25
- Title:
- Design and application of stepper motor measurement and controlling instrument for LOX/kerosene rocket engine
- 文章编号:
- 1672-9374(2020)03-0068-07
- Keywords:
- LOX/kerosene; stepper motor; measurement and controlling instrument; two-way motor shift control; synchronous measurement; interrupt nesting
- 分类号:
- V433
- 文献标志码:
- A
- 摘要:
- 针对液氧煤油发动机在地面热试车过程中对工况变化和极限工况条件下工作性能的考核需求,提出采用集成一体化隔离技术的电机测控仪对流量调节器和燃料节流阀步进电机实施控制,并完成从电机检测、调节组件试验、发动机装配、热试车到交付出厂的测量和控制工作。研究过程采用定时器变频中断电机变速控制、PWM斩波细分驱动、多级中断嵌套和远距离测量等关键技术,解决了步进电机长距离、大驱动力矩下快速启停平稳控制要求,以及试车双路电机同时基下独立调节和角度同步测量,实现液氧煤油发动机试车过程推力和混合比稳定调节。400余次热试车及各项试验验证,电机控制频率偏差小于±2 Hz,角度控制精度小于±0.25
- Abstract:
- To meet the requirements to qualify the characteristics of LOX/kerosene engine under changing working conditions and extreme working conditions during ground hot tests, a motor measuring and controlling instrument with an integrated isolation technology was proposed to different types of flow regulators and fuel throttle valve. The flow valve stepper motor was controlled to complete the measurement and control work ranged from motor detection, adjustment component test, engine assembly, hot test to the delivery. In the research process, key technologies such as variable speed control of timer frequency conversion interrupt motor, PWM chopper subdivision drive, multi-level interrupt nesting and long-distance measurement were adopted. As result, the requirements of fast start-stop smooth control of stepper motor under long distance and large driving torque, and the independent test of the two-way motor at the same time and the simultaneous measurement of the angle were fulfilled, thus the thrust and mixing ratio of the LOX/kerosene engine test process were stably adjusted. More than 400 hot tests and various verified tests had been conducted, and the motor control frequency deviation is less than ±2 Hz, and the angle control accuracy is better than ±0.25
参考文献/References:
[1] 范瑞祥, 郑立伟, 宋强, 等. 发动机推力调节能力对系列构型运载火箭总体性能影响研究[J]. 载人航天, 2014, 20(5): 393-398.
[2] 谭永华, 杜飞平, 陈建华, 等. 液氧煤油高压补燃循环发动机深度变推力系统方案研究[J]. 推进技术, 2018, 39(6): 1201-1209.
[3] 陈维宇, 程亚威, 李小明, 等. 高压小流量稳流型调节器特性研究[J]. 火箭推进, 2011, 37(4): 40-44.
CHEN W Y, CHENG Y W, LI X M, et al. Characteristics of low-output flow-stabilized regulator under high working pressure[J]. Journal of Rocket Propulsion, 2011, 37(4): 40-44.
[4] 许志宇, 李小明. 过载对流量调节器静态特性的影响研究[J]. 火箭推进, 2016, 42(3): 63-67.
XU Z Y, LI X M. Effects of overload on static characteristics of liquid-flow regulator[J]. Journal of Rocket Propulsion, 2016, 42(3): 63-67.
[5] 樊留强, 惠延波, 王莉. 步进电机加减速控制新方法的研究[J]. 电机与控制应用, 2017, 44(3): 36-39.
[6] 杜家熙, 陈艳锋, 李国厚. 基于单片机的步进电机控制器设计[J]. 煤矿机械, 2007, 28(2): 88-91.
[7] 陈志聪. 步进电机驱动控制技术及其应用设计研究[D]. 厦门: 厦门大学, 2008.
[8] 唐佳伟. 两相混合式步进电机细分控制器的设计[D]. 杭州: 浙江理工大学, 2015.
[9] 李玲娟. 多细分二相混合式步进电机驱动器的研制[D]. 西安: 西北工业大学, 2007.
[10] 王祖麟, 李志雄. 步进电机一体化控制系统的设计与实现[J]. 电子技术, 2014, 43(8): 49-51.
[11] 林瑞燊, 孙兴进. 步进电动机的细分电流波形及其实现[J]. 上海大学学报(自然科学版), 1999, 5(6): 501-504.
[12] MAN Z H, YU X H, ESHRAGHIAN K, et al. A robust adaptive sliding mode tracking control using an PBF neural network for robotic manipulators[C]// IEEE International Conference on Neural Networks.[S.l.]:IEEE,1995.
[13] 魏京芳.液氧煤油发动机电机测控技术研究[C]//首届中国空天推进技术论坛2018年学术年会.西安:航天推进技术研究院,2018.
[14] 李彦丽. 步进电机失步原因分析及常见故障检测[J]. 电子工业专用设备, 2014, 43(12): 39-42.
[15] 宋波, 韦薇, 张孝其. 两相混合式步进电机驱动器的设计[J]. 电子工业专用设备, 2014, 43(2): 53-56.
[16] 赵涛, 季宁一, 刘汉忠, 等. 步进电动机SPWM微步距细分控制的研究[J]. 微特电机, 2018, 46(4): 72-74.
[17] 李玲娟, 刘景林, 王灿. 两相混合式步进电机恒转矩细分驱动技术研究[J]. 微电机, 2007, 40(3): 48-50.
[18] PICKUP I E D, RUSSELL A P. Nonlinear model for predicting settling time and pull-in rate in hybrid stepping motors[J]. Proceedings of the Institution of Electrical Engineers, 1979, 126(4): 307.
相似文献/References:
[1]李 程,杨永强,徐浩海,等.500 t级液氧煤油补燃发动机起动过程仿真研究[J].火箭推进,2014,40(06):1.
LI Cheng,YANG Yong-qiang,XU Hao-hai,et al.Numerical simulation of start-up process for 500 t thrust LOX/kerosene staged combustion cycle rocket engine[J].Journal of Rocket Propulsion,2014,40(03):1.
[2]雷 恒,贾景卫,谢 宁.液氧煤油发动机蒸发器路单向阀结构优化[J].火箭推进,2012,38(01):27.
LEI Heng,JIA Jing-wei,XIE Ning.Structure optimization of check valve in evaporator pipeline of LOX/kerosene engine[J].Journal of Rocket Propulsion,2012,38(03):27.
[3]范瑞祥,田玉蓉,黄 兵.新一代运载火箭增压技术研究[J].火箭推进,2012,38(04):9.
FAN Rui-xiang,TIAN Yu-rong,HUANG Bing.Study on pressurization of new generation launch vehicle[J].Journal of Rocket Propulsion,2012,38(03):9.
[4]谭永华.中国重型运载火箭动力系统研究[J].火箭推进,2011,37(01):1.
TAN Yong-hua.Research on power system of heavy launch vehicle in China[J].Journal of Rocket Propulsion,2011,37(03):1.
[5]蒲星星,王建设,高玉闪,等.液氧煤油发动机故障监控特征参数提取研究[J].火箭推进,2017,43(06):26.
PU Xingxing,WANG Jianshe,GAO Yushan,et al.Research on feature extraction for fault monitoring of LOX/kerosene rocket engine[J].Journal of Rocket Propulsion,2017,43(03):26.
[6]雷 征,陈 赟,雷博娟,等.液氧煤油发动机碟形金属密封特性[J].火箭推进,2019,45(04):52.
LEI Zheng,CHEN Yun,LEI Bojuan,et al.Sealing characteristic of dish-shaped metal seal in LOX/kerosene rocket engine[J].Journal of Rocket Propulsion,2019,45(03):52.
备注/Memo
收稿日期:2019-07-02; 修回日期:2019-11-09
作者简介:魏京芳(1973—),女,硕士,高级工程师,研究领域为液体火箭发动机测控技术
更新日期/Last Update:
2020-06-25