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DYNAMIC BEHAVIOR ANALYSIS FOR LANDING-GEAR WITH DIFFERENT TYPES OF DUAL-CHAMBER SHOCK-STRUTS 被引量:10
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作者 Nie Hong Qiao Xin +1 位作者 Gao Zejun Zhou Lanqin 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 1991年第2期235-244,共10页
In this paper three types of dual- chamber shock- struts are considered in dynamic analyses of landing-gear behavior during impact and taxi. Their dynamic characteristics are compared with each other according to calc... In this paper three types of dual- chamber shock- struts are considered in dynamic analyses of landing-gear behavior during impact and taxi. Their dynamic characteristics are compared with each other according to calculation results, and some conclusions are presented.It is very helpful for selecting a suitable type of dual-chamber shock-strut in landing-gear design. 展开更多
关键词 DYNAMIC BEHAVIOR ANALYSIS FOR LANDING-GEAR WITH DIFFERENT TYPES OF DUAL-CHAMBER SHOCK-STRUTS
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Energetical Theories on Fatigue Life Prediction
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作者 童小燕 《Journal of Materials Science & Technology》 SCIE EI CAS CSCD 1992年第4期266-272,共7页
Current developments on fatigue life prediction methods have been systematically reviewed.In con- sideration of the irreversibility of energy dissipation during fatigue damage process,the main contents for fatigue dam... Current developments on fatigue life prediction methods have been systematically reviewed.In con- sideration of the irreversibility of energy dissipation during fatigue damage process,the main contents for fatigue damage estimation and localized equivalence as well as simulation models have been established.A frame of energy-based fatigue life prediction method has been proposed,meanwhile, the procedure in application to a practical structure component has been described. 展开更多
关键词 energy dissipation fatigue damage fatigue life prediction local response equivalence
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Method to Monitor Helicopter Rotor Fault Using Diagnostic Matrix
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作者 朱旭程 马强 侯志强 《Defence Technology(防务技术)》 SCIE EI CAS 2010年第2期126-132,共7页
An efficient method for helicopter rotor fault diagnosis was proposed using diagnostic matrix and its software framework was developed.The diagnostic matrix was extracted by the way of simulating the quantitative mode... An efficient method for helicopter rotor fault diagnosis was proposed using diagnostic matrix and its software framework was developed.The diagnostic matrix was extracted by the way of simulating the quantitative models of damaged and undamaged rotor systems.The conflicts were recognized by the virtual symptom sensor based on the dependencies between symptoms and faults.Diagnostic candidates were generated by the Boolean hitting algorithm.The proposed method provides multi-fault real-time diagnostic capability and it is suitable for the synthetic health monitoring of complex systems. 展开更多
关键词 test technique for air vehicle diagnostic matrix HELICOPTER ROTOR
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