飞机结构适坠性是航空安全的重要关注点之一,通过材料性能试验和复合材料波纹板准静态压溃试验,获得了T700/3234复合材料力学性能参数及波纹板压溃吸能结果;基于试验数据验证了复合材料波纹板有限元模型和材料模型的正确性;建立了机身框段有限元模型,将复合材料波纹板用作机身下部吸能结构,分析机身框段有限元模型在7m/s时的坠撞动态响应.仿真结果表明:在试验条件下,建立的复合材料波纹板模型可以准确模拟渐进失效过程;复合材料波纹板布局机身框段破坏过程较为稳定,其加速度值在人体耐受极限范围内,能够有效改善飞机结构的适坠性能.
参考文献
| [1] | HUANG J C;WANG X W .Numerical and experimental investigations on the axial crushing response of composite tubes[J].Computers & Structures,2009,91:222-228. |
| [2] | 李喆,孙凌玉.复合材料薄壁管冲击断裂分析与吸能特性优化[J].复合材料学报,2011(04):212-218. |
| [3] | TERRY J E;HOOPER S J;NICHOLSON M .Design and test of an improved crashworthiness small composite airframe-phase ii report[R].NASA SBIR Contract NAS1-20427,Terry Engineering,Andover,Kansas,1997. |
| [4] | TERRY J E.Design and test of an improved crashworthiness small composite airplane[A].Wichita,KS,2000:9-11. |
| [5] | Brite-Euram project CRASURV,Commercial aircraft-design for crash survivability[R].CT96-0207,1996-1999 |
| [6] | WIGGENRAAD J F M;SANTORO D;LEPAGE F et al.Development of a crashworthy composite fuselage concept for a commuter aircraft[R].NLR-TP-2001-108 |
| [7] | Karen E. Jackson;Edwin L. Fasanella .Development of a Scale Model Composite Fuselage Concept for improved Crashworthiness[J].Journal of aircraft,2001(1):95-103. |
| [8] | 陈永刚,许亚洪,益小苏.引发角对碳纤维/环氧复合材料圆管件轴向压溃性能的影响[J].材料工程,2004(12):36-39. |
| [9] | ILCEWICZ L B;BRIAN M.Safety & certification initiatives for composite airframe structure[A].Austin,Texas,2005 |
| [10] | 龚俊杰,王鑫伟.薄弱环节对复合材料波纹梁吸能能力的影响[J].材料工程,2006(05):28-31. |
| [11] | Tianchun Zou;Haolei Mou;Zhenyu Feng .Research on Effects of Oblique Struts on Crashworthiness of Composite Fuselage Sections[J].Journal of aircraft,2012(6):2059-2063. |
| [12] | M. Waimer;D. Kohlgriiber;D. Hachenberg;H. Voggenreiter .Experimental study of CFRP components subjected to dynamic crash loads[J].Composite structures,2013(Nov.):288-299. |
| [13] | Zhenyu Feng;Haolei Mou;Tianchun Zou;Jian Ren .Research on effects of composite skin on crashworthiness of composite fuselage section[J].International journal of crashworthiness,2013(5):459-464. |
| [14] | Feraboli P .Development of a corrugated test specimen for composite materials energy absorption[J].Journal of Composite Materials,2008(3):229-256. |
| [15] | Paolo Feraboli;Bonnie Wade;Francesco Deleo .LS-DYNA MAT54 modeling of the axial crushing of a composite tape sinusoidal specimen[J].Composites, Part A. Applied science and manufacturing,2011(11):1809-1825. |
| [16] | DAVID D;DIDIER J;MICHEL M.Evaluation of finite element modeling methodologies for the design of crashworthy composite commercial aircraft fuselage[A].,2004 |
| [17] | LSTC.LS-DYNA Theoretical Manual[M].California:Livermore Software Technology Corporation,2012 |
| [18] | ADAMS A;LANKARANI H M .A modern aerospace modeling approach for evaluation of aircraft fuselage crashworthiness[J].INTERNATIONAL JOURNAL OF CRASHWORTHINESS,2003,8(04):401-413. |
| [19] | Ikuo Kumakura;Masakatsu Minegishi;Kazuo Iwasaki .Impact Simulation of Simplified Structural Models of Aircraft Fuselage[J].SAE transactions,2000(1):1238-1243. |
| [20] | Department of defense joint service specification guide.JSSG-2010-7 Crew Systems Crash Protection Handbook[S].,1998. |
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