1. 北京航空航天大学 能源与动力工程学院,北京,100191
2. 先进航空发动机协同创新中心,北京,100191
3. 中国航天科工集团公司 北京动力机械研究所,北京,100074
纸质出版:2015
移动端阅览
胡良权, 陈敏, 唐海龙, 郭昆. 双轴分排涡扇发动机气路故障诊断测量参数选择方法[J]. 航空动力学报, 2015, 30(8): 1853-1861.
doi: 10.13224/j.cnki.jasp.2015.08.008
胡良权, 陈敏, 唐海龙, 郭昆. 双轴分排涡扇发动机气路故障诊断测量参数选择方法[J]. 航空动力学报, 2015, 30(8): 1853-1861. DOI: 10.13224/j.cnki.jasp.2015.08.008.
doi: 10.13224/j.cnki.jasp.2015.08.008 DOI:
针对地面台架试车气路故障诊断测量参数的优化选择提出了一种四步优化方法.该方法包括测量参数敏感性分析、部件性能参数相关性分析、影响系数矩阵条件数分析和遗传算法检验.第1步选择出了总空气流量;第2步选择出了风扇出口总温和压气机出口总温;第3步选择出了12种对故障诊断有利的测量参数组合;第4步选择出了最有利于故障隔离的测量参数组合.利用遗传算法进行单一故障辨识的结果表明:所选的12种测量参数组合的适应度都大于0.85
接近于最优的适应度1.对于最有利的测量参数组合
利用遗传算法的故障辨识验证结果表明
其适应度均大于0.9
验证了四步优化方法的有效性.
Aiming at measurement parameters optimal selection for gas path fault diagnosis in ground test bed
a four-step optimal method was presented. The four-step optimal method includes measurement parameters sensitivity analysis
component performance parameters correlation analysis
influence coefficient matrix condition number analysis and genetic algorithm validation. According to the first step
total air mass flow was picked out. In the second step
total temperature at fan exit and total temperature at compressor exit were picked out. In the third step
twelve measurement parameters combinations beneficial to fault diagnosis were picked out. In the final step
the best measurement parameters combination was obtained. Based on the genetic algorithm
the simulated diagnostic results show that
with these twelve measurement parameters combinations
all the fitness values for each single fault diagnosis are more than 0.85
which approximate the optimal fitness value 1. As to the most promising measurement parameter combination
all the fitness values are greater than 0.9 by genetic algorithm validation
which demonstrate the validity of this four-step optimal method.
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