IALM(Individual aircraft life management) is commonly applied to the individual aircraft for periodic analysis of fatigue damage,to calculate its equivalent flight hour and its rest service life.The plans for routine checking,general repairing,retiring and mending should be adjusted according to the actual damage of aircraft,so as to ensure the aircraft safe operation,reduce the maintenance cost and maximize the aircraft′s potential.
LU Hua,GUAN Yu
. Adjustment of maintenance plan based on the individual aircraft life management[J]. Journal of Shenyang Aerospace University, 2013
, 30(3)
: 78
-81
.
DOI: 10.3969/j.issn.2095-1248.2013.03.017
[1]许燕菲.浅谈飞机维修方案的优化[J].航空维修与工程,2004(5):54-55.
[2]Christian Boller.Structural health management of ageing aircraft and other infrastructure[C].Bangalore:Monograph on structural health monitoring inst of smart structures and systems,2001.
[3]Armitage S R.Future fatigue monitoring systems[C].Presented at the RTO AVT specialists′ meeting on exploitation of structural loads/heath data for reduced life cycle costs and published in RTO MP-7,1998.
[4]Hunt S R,Hebden I G.Eurofighter 2000:An integrated approach to structural health and usage monitorin[C].Presented at the RTO AVT specialists′ meeting on exploitation of structural loads/heath data for reduced life cycle costs and published in RTO MP-7,1998.
[5]Neumair M.Requirements on Future Structural Health Monitoring Systems[C].NATO RTO-MP-7,1998.
[6]MIL-HDBK-1530A.Aircraft structural integrity program general guidelines for[S].2002.
[7]刘小东,刘文珽.结构使用寿命评定的功能失效概率控制方法[J].北京航空航天大学学报,2002,28(1):105-108.
[8]刘文珽,王智,隋福成,等.单机寿命监控技术指南[M].北京:国防工业出版社,2010.