留言板

尊敬的读者、作者、审稿人, 关于本刊的投稿、审稿、编辑和出版的任何问题, 您可以本页添加留言。我们将尽快给您答复。谢谢您的支持!

姓名
邮箱
手机号码
标题
留言内容
验证码

民机飞行载荷谱编制方法

刘晓明 万少杰 熊峻江 李强

刘晓明, 万少杰, 熊峻江, 等 . 民机飞行载荷谱编制方法[J]. 北京航空航天大学学报, 2013, 39(5): 621-625.
引用本文: 刘晓明, 万少杰, 熊峻江, 等 . 民机飞行载荷谱编制方法[J]. 北京航空航天大学学报, 2013, 39(5): 621-625.
Liu Xiaoming, Wan Shaojie, Xiong Junjiang, et al. New approach for generating flight load spectrum of civil aircraft[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(5): 621-625. (in Chinese)
Citation: Liu Xiaoming, Wan Shaojie, Xiong Junjiang, et al. New approach for generating flight load spectrum of civil aircraft[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(5): 621-625. (in Chinese)

民机飞行载荷谱编制方法

基金项目: 国家自然科学基金资助项目(51075019); 航空科学基金资助项目(20095251024)
详细信息
  • 中图分类号: V214.11

New approach for generating flight load spectrum of civil aircraft

  • 摘要: 探索了由同类机型的飞行实测载荷统计数据,推断新设计机型的飞行谱,进而编制其载荷谱的新途径.采用国外同类飞机的飞行实测载荷统计数据,依据类比法,分析和推断出某民机的飞行谱以及各飞行状态连续应力谱;在此基础上,根据民用运输机的TWIST编谱方法,编制了各飞行状态的突风和机动载荷谱,最终,随机生成了其飞行谱对应的5×5地-空-地载荷谱,从而验证了探索途径的可行性与有效性.采用该方法可以加快民机研制周期.

     

  • [1] 熊峻江.飞行器结构疲劳与寿命设计[M].北京:北京航空航天大学出版社,2004:5,12,16
    Xiong Junjiang.Fatigue life design for aircraft structure[M].Beijing:Beijing University of Aeronautics and Astronautics Press,2004:5,12,16(in Chinese)
    [2] 张福泽.飞机载荷谱编制的新方法研究[J].航空学报,1998,19(5):518-524
    Zhang Fuze.New method of drawing up aircraft load spectrum[J].Acta Aeronautica et Astronautica Sinica,1998,19(5): 518-524(in Chinese)
    [3] 阎楚良,高镇同.飞机高置信度中值随机疲劳载荷谱的编制原理[J].航空学报,2000,21(2):118-123
    Yan Chuliang,Gao Zhentong.Compilation theory of median stochastic fatigue load-spectrum with high confidence level for airplane[J].Acta Aeronautica et Astronautica Sinica,2000, 21(2): 118-123 (in Chinese)
    [4] Xiong J J,Shenoi R A.An integrated and practical reliability-based data treatment system for actual load history[J].Fatigue and Fracture of Engineering Materials and Structures,2005, 28(10): 875-889
    [5] Xiong J J,Shenoi R A.A load history generation approach for full-scale accelerated fatigue tests[J].Engineering Fracture Mechanics,2008,75(10):3226-3243
    [6] 隋福成,刘文珽.飞机等幅疲劳试验载荷谱编制技术研究[J].机械强度,2008,30(2):266-269
    Sui Fucheng,Liu Wenting.Study on the technique of developing constant amplitude load spectrum for aircraft fatigue test[J].Journal of Mechanical Strength,2008,30(2):266-269 (in Chinese)
    [7] Klemenc J,Fajdiga M.Improved modelling of the loading spectra using a mixture model approach[J].International Journal of Fatigue,2008,30(7):1298-1313
    [8] Jensen J J.Extreme value predictions using Monte Carlo simulations with artificially increased load spectrum[J].Probabilistic Engineering Mechanics,2011,2692:399-404
    [9] Le Divenah L,Beaufils J Y.Large commercial aircraft loading spectra:overview and state of the art[J].Journal of ASTM International,2004,1(10):1-13
    [10] Heulera P,Klätschke H.Generation and use of standardised load spectra and load-time histories[J].International Journal of Fatigue,2005,27(8):974-990
    [11] 李元镜.飞-续-飞试验载荷谱(5乘5谱)编制方法初探[J].民用飞机设计与研究,2002(3):1-11
    Li Yuanjing.Study of designing flight load spectrum (five multiply five spectrum)[J].Civil Aircraft Design and Research,2002(3):1-11(in Chinese)
    [12] 潘庆荣.飞-续-飞试验谱编制方法——TWIST方法中对数正态极值分布的实现[J].民用飞机设计与研究,2004(3):21-32
    Pan Qingrong.Method of generating flight spectrum:realization of logarithmic normal extreme value distribution in TWIST method[J].Civil Aircraft Design and Research,2004(3): 21-32(in Chinese)
    [13] 潘庆荣.TWIST编谱方法中阵风载荷谱形状相似准则的实现[J].民用飞机设计与研究,2005(3):5-18
    Pan Qingrong.Realization of similarity shape of gust load spectrum in TWIST method[J].Civil Aircraft Design and Research,2005(3):5-18(in Chinese)
    [14] 穆志韬,曾本银.直升机结构疲劳[M].北京:国防工业出版社,2009
    Mu Zhitao,Zeng Benyin.Fatigue of helicopter structure[M].Beijing:National Defence Industry Press,2009 (in Chinese)
    [15] FAA.Statistical loads data for Boeing 737-400 aircraft in commercial operations[R].DOT/FAA/AR-98/28,1998
    [16] FAA.Statistical loads data for MD-82&83 aircraft in commercial operations[R].DOT/FAA/AR-98/65,1999
    [17] FAA.Statistical loads data for the Airbus A-320 aircraft in commercial operations[R].DOT/FAA/AR-02/35,2002
  • 加载中
计量
  • 文章访问数:  2112
  • HTML全文浏览量:  61
  • PDF下载量:  1025
  • 被引次数: 0
出版历程
  • 收稿日期:  2012-04-19
  • 修回日期:  2013-05-07
  • 网络出版日期:  2013-05-31

目录

    /

    返回文章
    返回
    常见问答