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纸基蜂窝模块化固持方法研究 被引量:3

Study on Method of Modularization Fixation for Paper Honeycomb Core
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摘要 基于磁场与摩擦学蜂窝芯材料固持原理,提出复杂型面纸基蜂窝零件固持平台的模块化设计思想。运用移动模块、固定模块、模块夹具以及导磁体和隔磁体解决了该原理中磁路控制问题,实现了复杂曲面零件在模块化固持平台上的加工固持。通过理论分析和有限元仿真研究了固持系统中蜂窝孔格的受力,分析了固持系统的特点和可靠性,以及永磁体厚度、固定平台高度、铁粉填充高度和平台间隙对磁场力的影响规律。实验与仿真结果表明,模块化固持平台能够满足复杂曲面蜂窝铣削加工的固持要求。 Based on magnetic field and frictional-clamping principle,a new modularization design concept is presented for the fixation system of paper honeycomb parts with complex shapes.The problem of controlling the magnetic field circuit existing in the method is solved using fixed modular,movable modular,modularized fixture,magnetic conductor and magnetic insulator.Clamping of paper honeycomb parts with complex contour on the modularized fixture is realized.Then,by theoretical analysis and finite element simulation,the force on the honeycomb grid in the fixation system is studied,the characteristic and reliability of the fixation system are checked,and also the influencing rules of parameters on the magnetic forces are analyzed,including height of magnetic body,height of fixed modular,height of ferrous powder and clearance between modules.Results of the simulation and experiments show that the modularized fixation system can fix the paper honeycomb parts with complex surface during machining process.
出处 《航空学报》 EI CAS CSCD 北大核心 2010年第6期1250-1256,共7页 Acta Aeronautica et Astronautica Sinica
基金 国家自然科学基金(50705085)
关键词 纸基蜂窝 固持 磁场 模块化 有限元方法 paper honeycomb fixation magnetic field modularization finite element method
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参考文献11

  • 1Grove S M, Popham E, Miles M E. An investigation of the skin/core bond in honeycomb sandwich structures using statistical experimentation techniques[J]. Composites Part A.. Applied Science and Manufacturing, 2006, 37 (5) : 804-812.
  • 2Aminanda Y, Castanie B, Barrau J J. Experimental and numerical study of compression after impact of sandwich structures with metallic skins[J].Composites Science and Technology, 2009, 69(1): 50-59.
  • 3Aktay L, Johnson A F, Kroplin B H. Numerical modelling of honeycomb core crush behaviour[J].Engineering Fracture Mechanics, 2008, 75(9): 2616 -2630.
  • 4李焱,何勇.Nomex蜂窝芯零件的数控加工[c]//第二届中国航空协会青年科技论坛文集.2006:451-457.
  • 5Foo C C, Chai G B, Seah L K. Mechanical properties of Nomex material and Nomex honeycomb strueture[J]. Composite Structures, 2007, 80(4): 588-594.
  • 6Liu G, Lin K Y. Study on clamping method for paper honeyeomb based on magnetic field and friction principle[J]. Journal of Materials Processing Technology, 2007, 190 (1-3) ; 65-72.
  • 7Ke Y L, Liu G. Attractive fixture system based on mag netic field and friction force for numerically controlled ma chining of paper honeycomb core[J]. Journal of Manufacturing Science and Engineering, 2005, 127(4): 901-906.
  • 8吴福忠,连晋毅.航空蜂窝芯零件数控加工工艺[J].航空制造技术,2007,50(7):92-95. 被引量:5
  • 9Hirayama A. Method for cutting honeycomb core: US, 6740268B2[P]. 2004-05 25.
  • 10刘刚,柯映林.纸基蜂窝零件夹持方法研究[J].浙江大学学报(工学版),2004,38(4):501-504. 被引量:13

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