期刊文献+

基于遗传算法的发动机气路性能模型修正研究 被引量:8

Engine Gas Path Performance Model Modification Based on Genetic Algorithm
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摘要 确定部件修正参数和目标性能参数作为模型修正基础,结合稳态模型的平衡方程,构造修正发动机非线性模型的代价函数,修正发动机稳态模型。计算了在不同工况修正后的特性参数,并与用影响系数矩阵方法所得结果进行对比,经遗传算法修正后参数精度有了较大提高。利用部件修正参数组合对发动机稳态模型进行修正,其结果表明敏感性参数在模型修正中起关键作用。所用修正方法对发动机性能模型修正、提高模型精度有一定指导意义。 Making component modified parameter and objective performance parameter as basis of model modification, stable engine model was modified by establishing cost function of engine nonlinear model modification with balance equation of stable model. Comparison of modified characteristic parameter at dif- ferent work conditions with modified results by influence coefficient matrix method showed that accuracy of parameters modified by genetic algorithm was enhanced greatly. Stable engine model was modified by using component modified parameter. The results indicated that sensitive parameter played key role in model modification. The method is referential to engine performance model modification and model accuracy en- hancement.
出处 《燃气涡轮试验与研究》 北大核心 2012年第4期46-50,共5页 Gas Turbine Experiment and Research
关键词 发动机性能模型 模型修正 遗传算法 影响系数矩阵 engine performance model model modification genetic algorithm intluence coefficient matrix
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参考文献6

  • 1Escher P C, Singh R. An Objective-Oriented Diagnostics Computer Program Suitable for Industrial Gas Turbine [C]//. 2F' International Congress on Combustion Engines. Switzerland, 1995.
  • 2尹大伟,李本威.某型涡扇发动机模型修正研究[c]//.中国航空学会第六届动力年会.2006.
  • 3李本威,尹大伟,王永华,马力,樊照远.某型涡扇发动机状态模型修正[J].海军航空工程学院学报,2008,23(2):213-216. 被引量:8
  • 4付尧明,傅强.非线性航空发动机性能参数估计方法研究[J].机械设计与制造,2006(8):140-141. 被引量:4
  • 5Mathioudakis K, Kamboukos Ph, Stamatis A. Turbofan Performance Deterioration Tracking Using Nonlinear Mod- els and Optimization Technique[J]. Journal of Turboma- chinery, 2002, 124(10) : 580-587.
  • 6谢小平.基于单机修正的某型发动机气路模型的建立研究[D].山东烟台:海军航空工程学院,2011.

二级参考文献9

  • 1刘红政,戴韧,陈康民.向心透平级内流动的数值研究[J].工程热物理学报,2004,25(5):752-756. 被引量:16
  • 2吴虎,肖洪,蒋建军.涡扇发动机部件特性自适应模拟[J].推进技术,2005,26(5):430-433. 被引量:19
  • 3[1]DEOL DAVID L.Temper-A Gas Path Analysis Tool for Commercial Jet Engines[J].Transactions of the ASME Journal of Engineering for Gas Turbines and Power,1994,116(1):82-89.
  • 4[3]SELLERS J F DYNGEN.A Program for Calculating Steady-state and Transient Performance of Turbojet and Turbofan Engine[D].NASA TN-D-7901 1973.
  • 5Glenn B. Gilyard and John S. Orme, Performance Seeking Control: Program Overview and Future Directions. NASA Technical Memorandum 4531, 1993.
  • 6S. Adibhatla and H. Brown, Intelligent Engine Control(IEC), AIAA - 92 - 3484, 1992.
  • 7S. Adlbhatla and K. L. Johnson, Evaluation of a Nonlinear PSC Algorithm on a Variable Cycle Engine, AIAA -93 -2077.
  • 8Matin D. Espana, "On the estimation algorithm for adaptive performance optimization of gas turbine", AIAA - 93 - 1823.
  • 9李松林,孙健国,黄金泉,李健民.涡扇发动机机载自适应建模技术研究[J].航空动力学报,1998,13(3):315-318. 被引量:10

共引文献10

同被引文献43

  • 1方昌德.变循环发动机[J].燃气涡轮试验与研究,2004,17(3):1-5. 被引量:69
  • 2郑铁军,王曦,罗秀芹,李其汉.建立航空发动机状态空间模型的修正方法[J].推进技术,2005,26(1):46-49. 被引量:27
  • 3黄顺洲,王永明,江和甫.核心机及其派生发动机发展的方法研究[J].燃气涡轮试验与研究,2005,18(2):1-5. 被引量:4
  • 4袁春飞,姚华,杨刚.航空发动机机载实时自适应模型研究[J].航空学报,2006,27(4):561-564. 被引量:25
  • 5谢小平.某型发动机气路模型修正研究[D].烟台:海军航空工程学院飞行工程系,2011.
  • 6Stamatis A. Mathioudakis K, Papailiou K D. Adaptive simulation of gas turbine performance[ J]. Gas Turbine Power. 1990:112 (2) :168-175.
  • 7Lambiris B, Mathioudakis K, Papailiou K D. Adaptive modeling of jet engine performance with application to condition monitoring [J]. ISABE. 1991(NO91-7058).
  • 8Stamatis A. Mathioudakis K, Papailiou K D. Optimal measuredparameter and health index selection for gas turbine performance status and fault diagnosis [ J ]. Gas Turbine Power. 1992 ( 114 ) : 209 - 216.
  • 9Escher P C, Singh R. An objective-oriented diagnostics computer program suitable for industrial gas turbine[ C ]. 21 st ( CIMAC ) In- ternational Congress on Combustion Engines. Switzeland, 1995, May 15 - 18.
  • 10谢小平.某型发动机气路模型修正研究[D].烟台:海军航空工程学院,2011:23—25.

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