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民机飞行载荷谱编制方法

, PP. 621-625

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Abstract:

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.

References

[1]  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
[2]  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
[3]  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
[4]  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
[5]  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)
[6]  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
[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]  Jensen J J.Extreme value predictions using Monte Carlo simulations with artificially increased load spectrum[J].Probabilistic Engineering Mechanics,2011,2692:399-404
[10]  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
[11]  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
[12]  Heulera P,Kl?tschke H.Generation and use of standardised load spectra and load-time histories[J].International Journal of Fatigue,2005,27(8):974-990
[13]  Heulera P,Kl?tschke H.Generation and use of standardised load spectra and load-time histories[J].International Journal of Fatigue,2005,27(8):974-990
[14]  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)
[15]  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)
[16]  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)
[17]  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)
[18]  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)
[19]  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)
[20]  FAA.Statistical loads data for Boeing 737-400 aircraft in commercial operations[R].DOT/FAA/AR-98/28,1998
[21]  FAA.Statistical loads data for MD-82&83 aircraft in commercial operations[R].DOT/FAA/AR-98/65,1999
[22]  FAA.Statistical loads data for Boeing 737-400 aircraft in commercial operations[R].DOT/FAA/AR-98/28,1998
[23]  FAA.Statistical loads data for the Airbus A-320 aircraft in commercial operations[R].DOT/FAA/AR-02/35,2002
[24]  FAA.Statistical loads data for MD-82&83 aircraft in commercial operations[R].DOT/FAA/AR-98/65,1999
[25]  FAA.Statistical loads data for the Airbus A-320 aircraft in commercial operations[R].DOT/FAA/AR-02/35,2002
[26]  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)
[27]  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)
[28]  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)
[29]  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)
[30]  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)
[31]  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)
[32]  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)
[33]  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)
[34]  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)

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