期刊文献+

先进复合材料格栅结构制造工艺技术的研究进展 被引量:3

New Manufacturing Techniques for Advanced Composite Grid Structures
下载PDF
导出
摘要 介绍了复合材料格栅结构的特点及发展现状,并回顾了传统复合材料成型工艺方法和格栅结构的早期制造方法。另外,介绍2种新型的格栅结构加工方法,即混合加工法、膨胀模块加工法以及改进的格栅结构:互锁复合材料格栅结构、加套管的槽形连接格栅结构和TR IG结构;并分别说明了每种结构的优点。其中重点介绍了混合加工法并从理论上推导其可行性。最后总结了复合材料格栅结构制造工艺的发展趋势。 Properties of and advances in composite grid structures are presented. Traditional composite shaping processes and earlier grid structure fabricating techniques are reviewed. New manufacturing techniques, such as hybrid process and expansion block process, and three improved composite grid structures, such as interlocked composite grids, slotted joint grids with tubes and TRIG structures, are discussed along with their advantages. Emphases are laid upon the hybrid process and its feasibility of theoretical derivation. Finally, the developing trend of composite grid structures is summarized.
出处 《飞机设计》 2007年第6期33-37,55,共6页 Aircraft Design
基金 国家自然科学基金(10572012) 航空科学基金(05B51043)资助项目
关键词 复合材料格栅结构 制造工艺 混合加工法 槽形连接 composite grid structure manufacturing technique hybrid process slotted Joint
  • 相关文献

参考文献10

  • 1[1]Tsai S W,Manne P.Manufacturing of composite grid structures[R].Final Report,F49620-95-1-0202,Stanford,Stanford University,1996.
  • 2张志峰,陈浩然,李煊,蒋元兴.先进复合材料格栅圆柱壳优化设计的混合遗传算法[J].复合材料学报,2005,22(2):166-171. 被引量:28
  • 3[4]Huybrechts S M,Meink T E,Peter M W,et al.Manufacturing theory for advanced grid stiffened structures[J],Composites,2002,Part A 33:155-161.
  • 4[5]Tsai S W,Manufacture and design of composite grids[R],Final Technical Report,F49620-96-1-0258,Stanford,Stanford University,1997.
  • 5古托夫斯基 T G 主编,李宏运等译.先进复合材料制造技术.北京:化学工业出版社,2004:164.
  • 6[8]Meink T E,Huybrechts S.Hybrid tooling for advanced grid stiffened(AGS) Structures[A].1996 SAMPE Technical Conference Proceedings[C].1996.
  • 7[9]Wegner P M,Higgins J E,Vanwest B P.Application of advanced grid-stiffened structures technology to the minotaur payload fairing[A].In:Proceedings of the AIAA/ASME/ASCE/AHS/ASC 43rd Structures.Structural Dynamics,and Materials Conference,AIAA,Denver,Colorado[C].2002.
  • 8[10]Han D,Tsai S.Interlocked composite grids design and manufacturing[J].J Compos Mater 2003,(37):287-315.
  • 9[11]Yoon K J,Park H C,Lee H J,et al.Composite grid structure with near-zero thermally induced deflection[A].In:Proceedings of the AIAA/ASME/ASCE/AHS/ASC 41st Structures.Structural Dynamics,and Materials Conference and Exhibit,AIAA,Atlanta[C].2000.
  • 10[12]Tsai S W,Liu K K S.New processing of composite grids for aerospace applications[R].Final Report,F69620-98-1-0099,Stanford,Stanford University,1999.

二级参考文献12

  • 1黄炎.复合材料三角形加筋圆柱壳的总体失稳分析[J].复合材料学报,1987,4(1):25-31.
  • 2陈浩然 张志峰.先进复合材料格栅加筋结构(AGS)的制造分析和设计理论与方法(SAILR-2003-06)[R].大连:大连理工大学,2003..
  • 3Deb A, Booton M. Finite element models for stiffened plates under transverse loading [J]. Computers & Structures, 1988, 30(6): 110-116.
  • 4Chen H J, Tsai S W. Analysis and optimum design of composite grid structures [J]. Journal of Composite Materials,1996, 30(4): 503-533.
  • 5Troitsky M S. Stiffened Plates: Bending, Stability and Vibrations [M]. Amsterdam: Elsevier Science Publishing Company, 1976. 207-361.
  • 6Reddy A D, Valisetty R R, Rehfield L W. Continuous Filament Wound Composite Concepts for Aircraft Fuselage Structures [J]. Journal of Aircraft, 1985, 22(3): 249-255.
  • 7温玄玲 陈浩然.网格加筋复合材料圆柱壳的总体稳定性和中间框临界刚度计算[J].强度与环境,1986,6:19-25.
  • 8Bazaraa M S, Sherali H D, Shetty C M. Nonlinear Programming: Theory and Algorithms [M]. New York: John Wiley and Sons, 1993. 541-782.
  • 9Jaunky N, Knight N F. Optimal design of grid-stiffened composite panels using global and local buckling analyses [J]. Journal of Aircraft, 1998, 35(3): 478-486.
  • 10Eyassu W, Samuel K, Pang S S. Optimization for buckling loads of grid stiffened composite panels [J]. Composite Structures, 2003, 60: 159-169.

共引文献28

同被引文献30

引证文献3

二级引证文献8

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部