|
|
环境对LY12CZ铝合金典型螺接件疲劳性能的影响 |
刘祖铭 |
中南大学粉末冶金国家重点实验室 |
|
An Effect of Corrosion Environment on fatigue Properties of LY12CZ Al-Alloy Typical Bolted Lap Joints |
Zuming Liu |
中南大学粉末冶金国家重点实验室 |
[1]Corrosioncontrolforaircraft[R].DepartmentofTransportationFederalAviationAdministration,ACNo.43-4,1973 [2]LarryCapt,GriffinD .C -141Aserviceexperience-materialsandprocesses[J].SAMPEJournal,1978,14(2):9-16 [3]LiuZM .AStudyofCorrosionCasesofAircraftStructure[M ].Beijing:PublishingHouseofAviationIndustry,2001:1-9(刘祖铭.飞机结构腐蚀实例分析[M ].北京:航空工业出版,2001:1-9 [4]LiuZM ,CaoDG ,ZhangSP ,etal.Thecurrentsituationandcoun termeasureofournavalaircraftcorrosion[A].In:ProceedingsofSymposiumonAircraftCorrosion[C].Beijing:ChineseSocietyofAeronauticsandAstronautics,1994:20-30(刘祖铭,曹定国,张少平等.我国海军飞机腐蚀现状及对策[A].飞机腐蚀专题研讨会论文集[C].北京:中国航空学会维修工程专业委员会,1994:20-30) [5]WanhillRJH ,LucciaDeJJ ,RussoMT .Thefatigueinaircraftcorrosiontesting(FACT)programme[R].AGARD -R -713,1989 [6]ZhangB ,ZhangZG ,HanEH ,etal.StudyofcorrosionfatigueforLY12CZaluminumalloyrivetedlap-splicejoints[J].ActaMetall.Sin.,2000,36(8):482-486(张波,张正贵,韩恩厚等.LY12CZ铝合金铆接联接件在3.5%NaCl溶液中的腐蚀疲劳失效行为[J].金属学报,2000,36(8):482-486) [7]LiuYM ,JiangJL ,ShanYS .Someeffectsonfatiguepropertiesunderprotection/unprotectioncoatingsystems[J].ActaAeronauticaetAstronauticaSinica,1998,19(4):481-485(刘一明,蒋军亮,山永寿.环境对有/无防护涂层结构疲劳性能的影响[J].航空学报,1998,19(4):481-485) [8]MillerRN ,SelligerGG ,BoggsWA .Protectivesystemsforfasten erareasofcarrier-basednavalaircraft[J].MaterialsPerformance,1975,(8):29-32 [9]ManningSD ,GordonDE ,WeiRP .Developmentoffatigueandcrackpropagationdesign&analysismethodologyincorrosiveenvi ronmentfortypicalmechanically-fastenedjoints[R].NADC -83126-60,1983 [10]ChenQZ ,LiXM ,ZhouXY ,etal.Investigationofcorrosione quivalentrelationshipsbetweentheacceleratedenvironmentandthetypicalserviceenvironmentsofaircraftstructures[J].ActaAeronauticaetAstronauticaSinica,1998,19(4):414-418(陈群志,李喜明,周希沅等.飞机结构典型环境腐蚀当量关系研究[J].航空学报,1998,19(4):414-418) [11]AVICScience&TechnologyAcademy.HandbookofDurabilityandDamageToleranceDesignofAircraftStructure(Ⅱ)[M ].Beijing:TheMinistrgofAeronauticandAstronauticIndustriesofChina,1989,2-15(航空航天工业部科学技术研究院.飞机结构耐久性及损伤容限设计手册(Ⅱ)[M ].北京:航空航天工业部,1989,2-15) [12]SpeidalMD .Corrosionfatigue:chemistry,mechanicsandmi crostructure[M ].McEvily,Stachleeds.NACE ,1972,329 [13]YangHX ,WuJQ .Interferencefitjointandstresscorrosioncracking[J].ActaAeronauticaetAstronauticaSinica,1984,5(1):46-49(杨汉祥,吴金泉.干涉配合连接与应力腐蚀断裂[J].航空学报,1984,5(1):46-49) [14]XiaoST ,ZhouYQ ,FuXJ .Anexperimentalstudyonenhance menteffectivenessofthecold-expansionholesagainstfatigueincorrosionenvironment[J].JournalofMechanicalStrength,1996,18(1):41-43(肖寿庭,周岳泉,付祥炯.3.5%NaCl水溶液腐蚀环境中冷胀孔抗疲劳强化效果的试验研究[J].机械强度,1996,18(1):41-43) [15]TeradaH .Structuralfatigueandjointdegradation[J].Internation alJournalofFatigue,2001,23:S21-S30 |
|
Viewed |
|
|
|
Full text
|
|
|
|
|
Abstract
|
|
|
|
|
Cited |
|
|
|
|
|
Shared |
|
|
|
|
|
Discussed |
|
|
|
|