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军用飞机结构耐久性严重谱编制与应用研究进展 被引量:5

Advances in durability severe spectrum:Development and application for military aircraft structures
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摘要 耐久性载荷谱是进行飞机结构耐久性设计、分析和试验的前提,是飞机结构耐久性研究的核心问题之一。美国空、海军联合使用规范指南JSSG-2006和中国国军标GJB 67.6A-2008均建议采用“耐久性严重谱”进行飞机结构定延寿,严重谱具有诸多优点,是目前国内外载荷谱编制研究的热点。本文以标准、规范要求为指引,以服务型号研制为目标,对国内外军用飞机结构耐久性严重谱编制和应用技术现状进行了系统总结。首先,阐述了严重谱的概念,总结了国内外军用飞机结构定延寿采用的2类载荷谱和分散系数取值,介绍了严重谱严重程度确定方法研究现状;然后,概述了国内外提出和发展的严重谱编制方法及耐久性严重谱在型号定延寿中的应用;最后,指出了当前严重谱编制与应用技术的难点和发展趋势,为严重谱编制与应用技术的发展提供参考。 Load spectrum is a basis for durability design,analysis and testing,and has always been one of the core issues of military aircraft structural durability research.To conduct the fatigue life evaluation and extension,the durability severe spectrum has been recommended in the Jointed Service Specification and Guideline JSSG-2006 and Chinese national military standard GJB 67.6 A-2008,becoming a hotspot in both domestic and foreign load spectrum research because of its multiple advantages compared to the average spectrum.To serve the research and development of aircraft models,this paper systematically summarizes the status of durability severe spectrum development and applications under the guidance of relevant standards and specifications.First,the concept of severe spectrum is elaborated,two types of load spectra and corresponding scatter factors used for life evaluation and extension are summarized,and the determination method of the severity of the severe spectrum are introduced.Secondly,the developing methods and applications of the severe spectrum are reviewed.Finally,the technical challenges and future research directions of severe spectrum development and application are pointed out.
作者 贺小帆 朱俊贤 HE Xiaofan;ZHU Junxian(School of Aeronautical Science and Engineering,Beihang University,Beijing 100191,China)
出处 《航空学报》 EI CAS CSCD 北大核心 2022年第12期57-70,共14页 Acta Aeronautica et Astronautica Sinica
基金 国家自然科学基金(11772027) 航空科学基金(201909051002)。
关键词 耐久性 严重谱 疲劳 飞机结构 平均谱 分散系数 durability severe spectrum fatigue aircraft structure average spectrum scatter factor
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  • 1王智,李京珊,张福泽.用代表中值损伤的“飞行大纲”编排飞机载荷谱的方法[J].机械强度,2004,26(5):517-521. 被引量:9
  • 2张福泽.疲劳分散系数的分类及其取值[J].航空学报(工程增刊),1987,(6):239-243.
  • 3国防科学技术工业委员会.GJB 67.6-1985军用飞机强度和刚度规范:可靠性要求和疲劳载荷[S].北京:国防科学技术工业出版社,1986:3-4.
  • 4British Ministry of Defence. DEF STAN 00-970 Part 1/3 Section 3 Leaflet 35: Fatigue safe-life substantiation[S]. Kentigem House 65 Brown Street GLASGOW G28EX: Ministry of Defence Stan BM&D, 1998: 2.
  • 5British Ministry of Defence. Standard 00-970 vols. 1 and 2 leaflet 201: Design and airworthiness requirements for service aircraft [ S ]. Kentigem House 65 Brown Street GLASGOW G28EX: Ministry of Defence Stan BM&D, 1987: 3.
  • 6U.S. Department of Defence. MIL-HDBK-SD Metallic materials and elements for aerospace vehicle structure[S]. U.S. : Department of Defance, 1983: 4.
  • 7吴学仁.飞机结构金属材料力学性能手册:第1卷:静强度疲劳,耐久性[M].北京:航空工业出版社,1997:199-353.
  • 8U.S. Department of Defence. JSSG-2006 Joint service specification guide: Aircraft structures[S]. U.S. : Department of Defance, 1998: 388-392.
  • 9刘文埏.结构可靠性设计手册[M].北京:国防工业出版社,2008.
  • 10Weibull W. A statistical representation of fatigue failure in solids[J]. Acta Polytech, 1949, 9(1): 39-49.

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