期刊文献+

基于Simulink的柴油机冷却水温度实时仿真模型 被引量:2

A Coolant Temperature Real-Time Model of Diesel Engine Based on Simulink
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摘要 利用Simulink建立了一个柴油机冷却系统模型,利用这一模型对柴油机冷却水温作出预测,为节温器及水温传感器的诊断提供了重要依据。最后在YC6112ZLQ柴油机上进行了试验,证明模型值与实测值的最大误差小于5%,并能满足实时性的要求。 A coolant temperature model based on Simulink was built to predict diesel engine water temperature,which is helpful for ECT and thermostat fault diagnosis.Finally the model was validated on YC6112ZLQ diesel.It was proved to meet the accuracy and reliability.
出处 《车用发动机》 北大核心 2004年第2期32-35,共4页 Vehicle Engine
关键词 柴油机 节温器 冷却水温 模型 diesel engine thermostat coolant temperature model
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参考文献2

  • 1Kwang Yoo, Kenneth Simpson, Myron Bell, et al. An Engine Coolant Temperature Model and Application for Cooling System Diagnosis[C]. Delphi Automotive System. SAE paper, 2001-01-0939.
  • 2Kwang Yoo, Kenneth Simpson, Myron Bell, et al. An Engine Coolant Temperature Model and Application for Cooling System Diagnosis[C]. Delphi Automotive System. SAE paper, 2001-01-0939.

同被引文献22

  • 1陈兵芽,刘莹,孙长存.石蜡的热膨胀驱动特性[J].机械工程材料,2008(7):60-63. 被引量:10
  • 2杨和基.自力式调温器时间常数的分析研究[J].给水排水,1994,20(9):36-39. 被引量:2
  • 3李运泽,魏传锋,袁领双,王浚.应用热电制冷器的微型航天器主动温度控制及仿真[J].机械工程学报,2005,41(10):149-152. 被引量:9
  • 4袁领双,李运泽,刘猛,王浚.行星际航天器主动热控系统模糊控制[J].宇航学报,2006,27(1):81-84. 被引量:6
  • 5侯增祺,胡金刚.航天器热控制技术:原理及其应用[M].北京:中国科学技术出版社,2006,239-253.
  • 6Theodore D, Gajanana S, Birur C. NASA thermal control technologies for robotic spacecraft [ J ]. Applied Thermal Engineering, 2003, 23 (9) : 1055 - 1065.
  • 7Alan G L, Razi N M. Dynamic performance of conventional and electrically activated engine thermostats [ C ]. ASME 2001 ICE Spring Technical Conference, Philadelphia, Pennsylvania, April 29-May 2, 2001.
  • 8Yang B Z, Lin Q. Latchable phase-change actuators for micro- flow control applications [ C ]. The 2005 International Mechanical Engineering Conference and Exhibition, Orlando, FL, November 5 - 15, 2005.
  • 9Zou X, Jordan J, Shillor M. A dynamic model for a thermostat [J. Journal of Engineering Mathematic, 1999, 36(4) : 291 - 310.
  • 10Klintberg L, Karlsson M. A thermally activated-paraffin based actuator for gas-low control in a satellite electrical propulsion system[J]. Sensors and Actuators A, 2003, 105 : 237 -246.

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