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材料工程  2008 

X-cor夹层结构复合材料力学性能实验研究进展

, PP. 76-80

Keywords: X-cor夹层结构,Z-pin,力学性能,失效

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Abstract:

作为一种新型复合材料夹层结构,X-cor夹层结构具有高刚性、抗冲击、损伤容限大等优点,可以取代传统蜂窝夹层结构作为航空航天器主承力结构材料。X-cor夹层结构的突出优点是具有可设计性,通过改变面板、芯材和增强物的几何物理参数,可以获得需要的力学性能。本文综述了国内外X-cor夹层结构力学性能的实验研究进展,讨论了静态载荷和动态载荷下X-cor夹层结构的力学性能、损伤机理和失效模式,提出了X-cor夹层结构尚需深入研究的各类问题。

References

[1]  李顺林,王兴业.复合材料结构设计基础[M].武汉:武汉理工大学出版社,1993.
[2]  黄涛,矫桂琼,徐婷婷.Z向增强泡沫夹层结构复合材料[J].纤维复合材料,2005,(3):19-23.
[3]  ADAMS D O,STANLEY L E.Development and evaluation of stitched sandwich panels,NASA/CR-2001-211025[R].Washington:NASA,Langley Research Center,2001.
[4]  CARSTENSEN T C,KUNKEL E,MAGEE C.X-corTM advanced sandwich core material[R].In:33rd International SAMPE Technical Conference,Seattle:SAMPE,2001.
[5]  FREITAS G.Z-fiberTM technology and products for enhancing composite design[R].In:83rd Meeting of AGARD SMP,Florence:AGARD,1996.
[6]  孙先念,郑长良.层合复合材料Z-pinning增强技术的力学进展[J].航空学报,2006,27(7):1194-1202.
[7]  KAY B F.RWSTD airframe technology foundation for the 21st century[R].In:American Helicopter Socity 57th Annual Forum,Washington:American Helicopter Society,2001.
[8]  MARASCO A I,CARTIE DENIS D R,PARTRIDGE I K,et al.Mechanical properties balance in novel Z-pinned sandwich panels:Out-of-plane properties[J].Composites Part A:Applied Science and Manufacturing,2006,37:295-302.
[9]  PARTRIDGE I K,CARTIE D D R,BONNINGTON T.Manufacture and performance of Z-pinned composites[M].In:ADVANI S,SHONAIKE G,Editors,Advanced Polymeric Materials.USA Florida Boca Raton:CRC Press,2003,103-138.
[10]  KOCHER C,WATSON W,GOMEZ M,et al.Integrity of sandwich panels and beams with truss-reinforced cores[J].Journal of Aerospace Engineering,2002,15(3):111-117.
[11]  MOURITZ A P.Compression properties of z-pinned sandwich composites[J].Journal of Materials Science,2006,41:5771-5774.
[12]  O'BRIEN T K,PARIS ISABE L L.Exploratory investigation of failure mechanisms in transition regions between solid laminates and X-cor truss sandwich[J].Composite Structures,2002,57:189-204.
[13]  田旭,肖军,李勇.X-cor夹层结构试制与性能研究[J].飞机设计,2004,(3):22-25.
[14]  杜龙.X-cor夹层复合材料力学性能研究[D].西安:西北工业大学,2007.
[15]  杜龙,矫桂琼,黄涛.X状Z向碳pin增强泡沫夹层结构剪切刚度预报[J].固体力学学报,2007,28(4):370-374.
[16]  杜龙,矫桂琼,黄涛,等.X状Z-pin增强泡沫夹层结构的剪切性能[J].复合材料学报,2007,24(6):140-146.
[17]  VAIDYA U K,MAHFUZ H,JEELA N S.Damage tolerance of resin transfer molded composite sandwich constructions,AFRL-VA-WP-TR-1999-3053[R].USA,Ohio:Tuskegee University Center for Advanced Materials,1999.
[18]  VAIDYA U K,KAMATH M V,HOSUR M V,et al.Low-velocity impact response of cross-ply laminated sandwich composites with hollow and foam-filled Z-pin reinforced core[J].Journal of Composites Technology and Research,1999,21(2):84-97.
[19]  VAIDYA U K,KAMATH M V,HOSUR M V,et al.Low velocity and compression-after-impact response of pin-reinforced sandwich composites[R].The ASME International Mechanical Engineering Congress and Exposition,Tennessee,Nashville:ASME,1999.
[20]  VAIDYA U K,PALAZATTO A,GUMMADI L N B.Low velocity impact response and nondestructive evaluation of sandwich composite structures[R].International Mechanical Engineering Congress and Exposition,ASME Winter Annual Meeting,Dallas:ASME,1997.
[21]  PALAZOTTO A N,HERUP E J,HARRINGTON T.An experimental investigation of sandwich panel under low velocity impact[R].In:ASCE 11th Engineering Mechanics Conference,Florida:ASCE,1996.
[22]  PALAZOTTO A N,GUMMADI L N B,VAIDYA U K,et al.Low velocity impact damage characteristic of Z-fiber reinforced sandwich panels-an experimental study[R].In:38th AIAA/ASME/ASCE/AHS SDM Conference,KissimMee:AIAA,1997.
[23]  PALAZOTTO A N,GUMMADI L N B,VAIDYA U K,et al.Low velocity impact damage characteristic of Z-fiber reinforced sandwich panels-an experimental study[J].Composite Structures,1999,43:275-288.
[24]  VAIDYA U K,PALAZOTTO A N,GUMMADI L N B.Low velocity impact and compressionafter-impact response of Z-pin reinforced core sandwich composites[J].Journal of Engineering Materials and Technology,2000,122(10):434-442.
[25]  VAIDYA U K,KUNAR P,HOSUR M V,et al.Low velocity and high strain rate impact of pin reinforced foam core sandwich composite[R].In:Proceedings of the Eighth Japan-US Conference on Composite Materials,Baltimore:Technomic Publication,1998.

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