Study on the anti-crash energy absorption characteristic of composite structure in the sub-cargo structure

doi:10.19936/j.cnki.2096-8000.20210928.013

Abstract

Abstract: In a survivable crash, the sub-cargo structure is the main energy-absorbing component in the process of an aircraft crash. As an important energy-absorbing element during a crash, the composite stanchion has an important impact on the crash resistance of the sub-cargo structure. The vertical crash test of the sub-cargo structure was carried out. Comparing the structural deformation failure modes and energy absorption conditions, the relationship between energy absorption characteristics of the sub-cargo structure at a crash speed of 9.144 m/s and the angle of the stanchion, the thickness of the stanchion and the trigger form are obtained. The results show that when the angle of the stanchion is 90 degrees, the thickness of the stanchion varies in sections and the connection between the stanchion and the frame is weak, and the sub-cargo structure has the best energy-absorbing performance.

Key words: composite structures, crashworthiness, energy absorption, crush test, composites failure mode

CLC Number:

TB332

SHI Meng, WANG Yang, WU Zhi-bin, LIU Fu. Study on the anti-crash energy absorption characteristic of composite structure in the sub-cargo structure[J]. COMPOSITES SCIENCE AND ENGINEERING, 2021, 0(9): 83-88.

References

[1] ABROMOWITZ A, SMITH T G, VU T, et al. Vertical drop test of a narrow-body transport fuselage section with conformable auxiliary fuel tank onboard: DOT/FAA/AR00/56[R]. Washington, D, C.: FAA,2000.
[2] ABRAMOWITZ A, SMITH T G, VU T, et al. Vertical drop test of a narrow-body transport fuselage section with overhead stowage bins[C]//World Aviation Congress & Exposition. 2002.
[3] ADAMS A, LANKARANI H M. A modern aerospace modeling approach for evaluation of aircraft fuselage crashworthiness[J]. International Journal of Crashworthiness, 2003, 8(4): 401-413.
[4] LEPAGE F. Results of the airliner sub-passenger floor structure drop test[Z]. CRASURV, CEAT Test Report S98/4449000 part5, 2000.
[5] COLLINS J S, JOHNSON E R. Static and dynamic response of graphite-epoxy curved frames[J]. Journal of Composite Materials, 1992, 26(6): 792-803.
[6] PEREZ J, JOHNSON E, BOITNOTT R. Design and test of semicircular composite frames optimized for crashworthiness[C]//39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit. 1998.
[7] 邹田春, 郝鹏, 冯振宇, 等. 斜撑杆对复合材料机身段适坠性能的影响研究[J]. 机械强度, 2013, 35(4): 546-550.
[8] 刘小川, 周苏枫, 孙侠生, 等. 民用飞机客舱地板下部结构吸能优化[J]. 机械科学与技术, 2011, 30(11): 1968-1972.
[9] 任毅如, 向锦武, 罗漳平, 等. 客舱地板斜撑杆对民机典型机身段耐撞性能的影响[J]. 航空学报, 2010, 31(2): 271-276.
[10] 汪洋, 吴志斌, 刘富. 复合材料货舱地板立柱压溃响应试验[J]. 复合材料学报, 2020, 37(9): 130-136.
[11] 苟仲秋, 孙侠生, 宋笔锋. 民机地板以下结构参数变化对复合材料机身适坠性能的影响研究[J]. 机械科学与技术, 2008, 27(5): 620-624.
[12] 张景新, 邱光荣. 环氧树脂基直升机复合材料耐坠性性能试验研究[J]. 直升机技术, 2008(2): 47-50.
[13] 郑建强, 向锦武, 罗漳平, 等. 民机机身耐撞性设计的波纹板布局[J]. 航空学报, 2010, 31(7): 1396-1402.
[14] 郑建强, 向锦武, 罗漳平, 等. 民机机身下部结构耐撞性优化设计[J]. 航空学报, 2012, 33(4): 640-649.

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