民用飞机典型机身段适坠性仿真分析
摘要
<正>飞机耐撞性是民用运输机安全性能的一个重要体现,在飞机设计初始阶段已经被当作和静强度性能、疲劳强度性能同等的因素来考虑。世界各国的研究机构及学者对飞机适坠性展开了大量的试验和仿真分析研究。20世纪70年代开始,美国国家航空航天局(NASA)将登月着陆模拟装置改装为轻型飞机和旋翼飞机坠撞试验平台,开展了全尺寸坠撞试验以及机身段试验~([1-5]);90年代中后期,欧盟开展了"CRASURV"计划,研究了复合材料机身结构的抗坠撞设计以及坠撞安全评估
引文
[1] Jackson K E, Fasanella E L. A survey of research performed at NASA langley research center’s impact dynamics research facility[R]. AIAA-2003-1896, 2003.
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[3] Abramowitz A, Smith T G, Vu T. Vertical drop test of a narrow-body transport fuselage section with conformable auxiliary fuel tank onboard[R]. DOT/FAA/AR-00/56, 2000.
[4] Jackson K E, Edwin L. Crash simulation of a vertical drop test of a B737 fuselage section with overhead bins and luggage[R]. NASA, 2001.
[5] Abramowitz A, Smith T G, Vu T, et al. Vertical drop test of a narrow-body transport fuselage section with overhead stowage bins[R]. DOT/FAA/AR-01/100, 2002.
[6] Labeas G, Kermanidis T H. Crushing behaviour of the energy absorbing tensor skin panels[J]. Fatigue & Fracture of Engineering Materials & Structures, 2003,26(5):449-457.
[7] 刘小川,郭军,孙侠生,等.民机机身段和舱内设施坠撞试验及结构适坠性评估[J].航空学报,2013,34(9):2130-2140.
[8] 刘小川,周苏枫,马君峰,等.民机客舱下部吸能结构分析与试验相关性研究[J].航空学报,2012,33(12):2202-2210.
[9] 牟让科,刘小川.民机机身结构和内部设施适坠性设计评估与验证指南[M].西安:西北工业大学出版社,2016.
[10] Fasanella E L, Jackson K E. Crash simulation of vertical drop tests of two boeing 737 fuselage sections[R]. U. S. Army Research Laboratory, Vehicle Technology Center, Langley Research Center, 2002.
[11] 何欢,陈国平,张家滨.带油箱结构的机身框段坠撞仿真分析[J].航空学报,2008(3):627-633.
[12] 王跃全,朱书华,王涛,等.大型民机机身结构适坠性仿真分析[J].南京航空航天大学学报,2013,45(2):186-190.
[13] 冯振宇,解江,李恒晖,等.大飞机货舱地板下部结构有限元建模与适坠性分析[J].航空学报,2019,40(2):523394-52239.
[2] Logue V, Mc Guire R J, Reinhardt J W, et al. Vertical drop test of a narrow-body fuselage section with overhead stowage bins and auxiliary fuel tank on board[R]. DOT/FAA/CT-94/116, 1995.
[3] Abramowitz A, Smith T G, Vu T. Vertical drop test of a narrow-body transport fuselage section with conformable auxiliary fuel tank onboard[R]. DOT/FAA/AR-00/56, 2000.
[4] Jackson K E, Edwin L. Crash simulation of a vertical drop test of a B737 fuselage section with overhead bins and luggage[R]. NASA, 2001.
[5] Abramowitz A, Smith T G, Vu T, et al. Vertical drop test of a narrow-body transport fuselage section with overhead stowage bins[R]. DOT/FAA/AR-01/100, 2002.
[6] Labeas G, Kermanidis T H. Crushing behaviour of the energy absorbing tensor skin panels[J]. Fatigue & Fracture of Engineering Materials & Structures, 2003,26(5):449-457.
[7] 刘小川,郭军,孙侠生,等.民机机身段和舱内设施坠撞试验及结构适坠性评估[J].航空学报,2013,34(9):2130-2140.
[8] 刘小川,周苏枫,马君峰,等.民机客舱下部吸能结构分析与试验相关性研究[J].航空学报,2012,33(12):2202-2210.
[9] 牟让科,刘小川.民机机身结构和内部设施适坠性设计评估与验证指南[M].西安:西北工业大学出版社,2016.
[10] Fasanella E L, Jackson K E. Crash simulation of vertical drop tests of two boeing 737 fuselage sections[R]. U. S. Army Research Laboratory, Vehicle Technology Center, Langley Research Center, 2002.
[11] 何欢,陈国平,张家滨.带油箱结构的机身框段坠撞仿真分析[J].航空学报,2008(3):627-633.
[12] 王跃全,朱书华,王涛,等.大型民机机身结构适坠性仿真分析[J].南京航空航天大学学报,2013,45(2):186-190.
[13] 冯振宇,解江,李恒晖,等.大飞机货舱地板下部结构有限元建模与适坠性分析[J].航空学报,2019,40(2):523394-52239.