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轮盘低循环疲劳试验器自动控制系统的开发 被引量:2

Development of Automatic Control System for Disk Low Cycle Fatigue Test Rig
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摘要 利用高速旋转试验设备进行轮盘低循环疲劳试验是开展轮盘疲劳寿命及损伤容限性能研究的有效手段。为确保此类试验器能够长时间稳定运行,开发了1套可靠的、无人值守的自动控制系统,以触摸屏为人机接口(HMI)完成试验参数的设置,以可编程逻辑控制器(PLC)为主站控制设备启停及转速循环,监测系统采用工控机(IPC)完成数据显示和保存,并采用第3方控件实现IPC和PLC的串口通信。测试结果表明:该控制系统稳定性高、可靠性好,完全满足设计要求。 The disk Low Cycle Fatigue(LCF) test was conducted using high-speed spinfacility that was a very effective equipment for the disk LCF life and damage tolerance. In order to ensure that such a rig was stable oper- ation for a long time, the stable and unattended automatic control system was developed. Touch screen was used for Human Machine In- terface (HMI) to complete the set of testing parameters, and Programmable Logic Controller (PLC) was used as the master station to control start-stop and speed loop, the monitoring system used IPC was responsible for data display and storage. Third-party component was uti- lized to realize serial communication of IPC and PLC. Testing results show that stability and reliabihty of the control system are well, and fully meet the design requirements.
出处 《航空发动机》 2013年第5期18-21,共4页 Aeroengine
基金 211重点学科建设项目 中央高校基本科研业务专项资金 浙江大学自主科研计划(2011QNA4020)资助
关键词 高速旋转试验器 轮盘 低循环疲劳试验 自动控制系统 人机接口 可编程逻辑控制器 high-speed spin equipment disk LCF test automatic control system Human Machine Interface PLC
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  • 1李建国,叶新农,徐可君.涡扇发动机寿命管理研究[J].海军航空工程学院学报,2005,20(4):468-472. 被引量:9
  • 2Melis M E,Zaretsky E V,August R.Probabilistic Analysis of Aircraft Gas Turbine Disk Life and Reliability[R].NASA/IM-1999-107436,1999.
  • 3Suresh S.材料的疲劳[M].王中光,译.第2版.北京:国防工业出版社,1999.
  • 4Jaske C E,Feddersen C E, Davis K B, et al. Analysis of fatigue, fatigue crack propagation, and fracture Data[R].NASA CR-132332,1973:49-54.
  • 5Shepherd D P. The prediction of fatigue life for arbitrary geometries from the statistical analysis of plain specimen data [R]. NASA/CP - 2002 - 211682, Fifth Annual Workshop on the Application of Probabilistic Methods for Gas Turbine Engines, Editors : Victoria Briscoe, 2002 : 511-538.
  • 6中国航空材料手册:第2卷[Z].第2版:北京:中国标准出版社,2002.
  • 7Melis M E, Zaretsky E V, August R. Probabilistic analysis of aircraft gas turbine disk life and reliability[R]. NASA/TM 1999-107436.
  • 8Xuan Hai-jun, Wu Rong-ren. Aeroengine turbine blade containment tests using high-speed rotor spin testing facility[J]. Aerospace Science and Technology, 2006, 10(6):01-508.
  • 9何庆.ZUST1型高速旋转试验台自动控制系统[D].杭州:浙江大学,2007:6-7.
  • 10蔚夺魁,邵丕仁.某型发动机涡轮盘销钉孔边低循环疲劳寿命分析[J].航空发动机,2000,21(2):37-41. 被引量:17

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