Design, manufacture and analysis of variable-stiffness composite structures

被引：0
|
作者：
Kong B. [1 ,2 ]
Gu J. [1 ]
Chen P. [1 ]
Yang J. [2 ]
Gan X. [2 ]
机构：
[1] State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing
[2] AVIC Chengdu Aircraft Design and Research Institute, Chengdu
来源：
Fuhe Cailiao Xuebao/Acta Materiae Compositae Sinica | 2017年 / 34卷 / 10期
关键词：
Analysis; Design; Manufacture; Progress; Review; Variable-stiffness composite structures;
D O I：
10.13801/j.cnki.fhclxb.20170829.006
中图分类号：
学科分类号：
摘要：
A research progress review of design, manufacture and analysis of variable-stiffness composite structures is provided in this paper. There are some special issues in variable-stiffness composite structures compared with traditional ones. First, the concept of variable-stiffness structure and the mechanism of Automated Fiber Placement (AFP) technology were introduced. Second, the definition of tow path was described and the key points to be considered during design and manufacture were summarized. Third, the modeling and analysis methods for variable-stiffness composite structures were curtly described. The current research situation of the mechanical properties of variable-stiffness composite structures was presented from the aspects of optimization method, stiffness and buckling, failure, and vibration. At last, the research work in the area was summarized and the future prospects of this field were proposed. © 2017, Chinese Society for Composite Materials. All right reserved.
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页码：2121 / 2133
页数：12
相关论文
共 92 条
  • [1] Langley T., Finite element modeling of tow-placed variable-stiffness composite laminates, (1999)
  • [2] Leissa A.W., Martin A.F., Vibration and buckling of rectangular composite plates with variable fiber spacing, Composite Structures, 14, 4, pp. 339-357, (1990)
  • [3] Biggers S.B., Srinivasan S., Compression buckling response of tailored rectangular composite plates, AIAA Journal, 31, 3, pp. 590-596, (1993)
  • [4] Curry J.M., Johnson E.R., Starnes J.H., Effect of dropped plies on the strength of graphite-epoxy laminates, AIAA Journal, 30, 2, pp. 449-456, (1987)
  • [5] Cairns D.S., Mandell J.F., Scott M.E., Design and manufacturing considerations for ply drops in composite structures, Composites Part B: Engineering, 30, 5, pp. 523-534, (1999)
  • [6] Xiao J., Li Y., Li J., Application of automatic fiber placement in manufacture of composite structures in large aircraft, Aeronautical Manufacturing Technology, 1, pp. 50-53, (2008)
  • [7] Ribeiro P., Akhavan H., Teter A., Et al., A review on the mechanical behaviour of curvilinear fibre composite laminated panels, Journal of Composite Materials, 48, 22, pp. 2761-2777, (2014)
  • [8] Liu R., Research on the mechanical performance of fiber reinforced composite variable angle laminates, (2012)
  • [9] Evans D.O., Fiber Placement, (2001)
  • [10] Gurdal Z., Olmedo R., In-plane response of laminates with spatially varying fiber orientations-variable stiffness concept, AIAA Journal, 31, 4, pp. 751-758, (1993)
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