航天推进技术研究院主办
QIN Yongtao,SONG Yang,SU Hongfang,et al.Method of man-machine-environment control over foreign object debris in pipelines used in rocket engine test[J].Journal of Rocket Propulsion,2015,41(06):80-85.
火箭发动机试验管道多余物人机环境控制方法
- Title:
- Method of man-machine-environment control over foreign object debris in pipelines used in rocket engine test
- 分类号:
- V434-34
- 文献标志码:
- A
- 摘要:
- 为消减液氧/煤油火箭发动机试验过程中工艺管道的多余物,消除试车隐患,基于人机环境系统理论,从人机环境综合考虑,对多余物产生的主要环节进行分析,探寻工艺管道多余物产生的根源。根据集对理论,分析影响因素间的同一度、对立度、波动度,探讨人机环境因素间耦合关系,确定多余物产生的关键因素。针对多余物的人机环境关键因素,结合实际工作,制定液体火箭发动机试验过程的多余物控制及检查方法,有效减少或消除发动机试验过程多余物的产生,保证发动机试验过程顺利安全进行。
- Abstract:
- On the basis of man-machine-environment system theory, the main links to result in foreign object debris are analyzed in the aspect of man-machine-environment influencing factors to search the root of producing the foreign object debris in the process pipes for removing the foreign object debris in the pipes and eliminating the potential danger in the process of liquid oxygen-kerosene rocket engine test. The identity, opposing degree, fluctuating degree of influencing factors are analyzed by means of set pair theory to research the coupling relationship among the influencing factors, and determinate the key factors of resulting in the foreign object debris. The foreign object debris control and inspecting methods were established in accordance with the man-machine-environment key factors and practical work in the testing process of liquid oxygen-kerosene rocket engine, so that the
参考文献/References:
[1]LIU Song, YAO Bin. Adaptive robust control of program- mable valves with manufacturer supplied flow mapping only[C]// The 43rd IEEE Conference on Decision and Control. [S.l.]: IEEE, 2004: 1117-1122.
[2]LIU Kun, ZHANG Yulin. A study on versatile simulation of liquid propellant rocket engine systems transients, AIAA 2000-3771[R]. USA: AIAA, 2000.
[3]李进, 赵宇, 李文钊, 等. 基于权重系数的液体火箭发动机可靠性验证方案[J]. 航空动力学报, 2011, 26(4): 931-934.
[4]ZHANG Hui, WANG Shujuan, ZHAI Guofu. Test condi- tion discussion of particle impact noise detection for space relay[J]. Chinese Journal of Aeronautics, 2007, 20(1): 35- 39.
[5]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.
[6]李琦芬. 低温推进剂管道输送系统特性研究[D]. 杭州: 浙江大学, 2005.
[7]CUI Jinshi, ZHA Huangbing. Fusin of detection and mat- ching based approaches for laser based multiple people tracking[C]// Proceeding of IECON. [S.l]: Industrial Elec- tronics Society, 2204: 2566-2572.
[8]KNAPP J Z. Particle detection method for detection of contraction particle in seal containers: US, 5694221[P]. 2011-11-22.
[9]熊涛. 航天器总装多余物控制方法探讨[J]. 航天器环境工程, 2006, 23(5): 277-280.
[10]李大南. 航天型号产品多余物及其预防和控制标准的实施检查[J]. 航天标准化, 2006, 1: 17-20.
[11]唐虎, 张敏贵, 张金容. 液体火箭发动机汽蚀管堵塞仿真研究[J]. 火箭推进, 2012, 38(3): 46-58.
TANG HU, ZHANG Mingui, ZHANG Jinrong.Simulation study on jamming of liquid rocket engine venturi[J]. Journal of Rocket Propulsion, 2012, 38(3): 46- 58.
[12]陈静. 复杂背景下器件多余物城乡检测若干关键技术研究[D]. 武汉: 华中科技大学. 2010.
[13]BOSNYATSKIJ G P, BARINUD V B, PARSADANOV G M, et al. Optimization of inter-relations of man- machine-external environment-reserve of reliability of system[J]. Gazovaya Promyshlennost, 2001 (12): 35-40.
[14]龙升照. 钱学森与人机环境系统工程[C]. 第八届中国人-机-环境系统工程大会, 深圳: 2007: 3-10.
[15]MA L H, YAN H Z. Comprehensive evaluation of fully mechanized mining face security based on unascertained- Information entropy model[C]// Proceedings of the 2nd IEEE International Conference on Computer Science and Information Technology. Beijing: IEEE, 2009: 268-271.
[16]QIN YT, ZHAO LP, YAO YY. Dynamic quality cha- racteristics modelling based on brittleness theory in complex manufacturing processes[J]. International Journal of Computer Integrated Manufacturing, 2011, 24(10): 915-926.
[17]金鸿章, 李琦, 吴红梅. 基于脆性因子的复杂系统脆性分析[J]. 哈尔滨工程大学学报, 2005, 26(6): 739-744.
[18]荣盘祥. 复杂系统脆性理论及其理论框架的研究[D]. 哈尔滨: 哈尔滨工程大学, 2006.
[19]RONG P X, JIN H Z, WEI Q. Brittleness research on complex system based on brittle link entropy[J]. Journal of Marine Science and Application, 2006, 5(2): 51-54.
相似文献/References:
[1]董 冬,张少博,刘 晓.试验状态信息管理软件设计[J].火箭推进,2013,39(06):72.
DONG Dong,ZHANG Shao-bo,LIU Xiao.Design of information management software for test status[J].Journal of Rocket Propulsion,2013,39(06):72.
[2]王军钢,赵万明,唐丽萍.提高低温压力测量准确度的方法初探[J].火箭推进,2012,38(05):65.
WANG Jun-gang,ZHAO Wan-ming,TANG Li-ping.Discussion on method of improving accuracy of pressure measurement in low temperature[J].Journal of Rocket Propulsion,2012,38(06):65.
[3]姬俊锋,吴光中,马利亚,等.液体推进剂发动机试验多工况流量控制方法[J].火箭推进,2011,37(02):71.
JI Jun-feng,WU Guang-zhong,MA Li-ya,et al.Multiple-working-conditions flowrate control for liquid engine test[J].Journal of Rocket Propulsion,2011,37(06):71.
[4]赵万明,王军钢.液体火箭发动机试验负推力修正[J].火箭推进,2010,36(06):56.
ZHAO Wan-ming,WANG Jun-gang.Correction of negative thrust in liquid rocket engine tests[J].Journal of Rocket Propulsion,2010,36(06):56.
[5]来代初,苏红军,李伟.液氧/煤油发动机煤油高低温试验工艺技术[J].火箭推进,2009,35(04):53.
Lai Daichu,Su Hongjun,Li Wei.High and low temperature test technology of
kerosene of the LOX/kerosene engine[J].Journal of Rocket Propulsion,2009,35(06):53.
[6]曹文庆,谭海林,李伟.低温发动机试验推进剂人口温度控制[J].火箭推进,2009,35(03):52.
Cao Wenqing,Tan Hailin,Li Wei.Propellant inlet temperature control
for cryogenic rocket engine tests[J].Journal of Rocket Propulsion,2009,35(06):52.
[7]赵万明.流量转速参数信号调理技术[J].火箭推进,2008,34(02):49.
Zhao Wanming.Signal modulating technique of flow and
rotating speed parameters[J].Journal of Rocket Propulsion,2008,34(06):49.
[8]张辉,郭立.液氧/煤油发动机摇摆测控系统技术要求及实现[J].火箭推进,2007,33(01):49.
Zhang hui,Guo Li.Development of the swinging measurement system for LOX/kerosene rocket engine[J].Journal of Rocket Propulsion,2007,33(06):49.
[9]胡瑛.液体火箭发动机试验数据曲线绘制软件设计[J].火箭推进,2007,33(01):55.
Hu Ying.Design of data curve drawing software for liquid rocket engine test[J].Journal of Rocket Propulsion,2007,33(06):55.
[10]单黎波,王建昌.内窥镜检测方法技术研究[J].火箭推进,2006,32(04):54.
Shan Libo,Wang Jianchang.Study on endoscope check method[J].Journal of Rocket Propulsion,2006,32(06):54.
备注/Memo
收稿日期:2015-08-13;修回日期:2015-08-29 基金项目:航天支撑技术项目(617010417) 作者简介:秦永涛(1981—),男,博士,研究领域为液体火箭发动机试验技术