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半豆荚杆先进拉挤预处理工艺研究 被引量:6

STUDY ON THE PRETREATMENT PROCESS OF ADVANCED PULTRUSION FOR HALF LENTICULAR TUBE
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摘要 以先进拉挤(Advanced Pultrusion,简称ADP)制备复合材料豆荚杆为背景,分析现有工艺的不足,提出了预处理工艺,以减轻制件表面纤维畸变和两侧厚度不足等缺陷。着重研究了预处理温度和时间对制件的作用机理,并以轴向拉伸性能和层间拉伸强度表征预处理工艺对试样的影响。试验结果表明,1100℃保温50min、105℃保温40min、110℃保温25min三组参数符合预处理工艺要求;2经试验验证,相对直接热压成型,上述预处理工艺参数下制得的试样力学性能没有明显的降低,预处理温度越低,相应的预处理条件下制得的试样力学性能越高。 To decrease the defects such as fiber distortion and insufficient thickness on both sides of the half lenticular tube, pretreatment process was proposed by analyzing the shortcoming of the existed advanced puhrusion process. The temperature and time of pretreatment were stydied with an oven and a hot-pressing device, the axial tensile property and interlayer tensile property were carried out to analyze the effects on the samples. The result showed suitable parameters for pretreatment process were 100℃ for 50min, 105℃ for 40min, 110℃ for 25min ; the mechanical properties of the product didn't decrease with pretreatment process; the lower the pretreat temperature was, the better mechanical property the sample could reach.
出处 《玻璃钢/复合材料》 CAS CSCD 北大核心 2015年第8期66-70,共5页 Fiber Reinforced Plastics/Composites
基金 上海航天支撑技术项目(617010806-02)
关键词 半豆荚杆 先进拉挤 预处理 纤维畸变 厚度 half lenticular tube advanced pultrusion pretreatment fiber distortion thickness
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参考文献16

  • 1Dale B. Advanced pultrusion takes off in commercial aircraft structures [J]. High-Performance Composites, 2003, 9: 36-39.
  • 2Kasai T, Asari K. Continuous forming method and device for H- shaped FRP member[ P]. U.S. Patent : 6592795, 2003-7-15.
  • 3Kuriyama S, Okamoto M. Method and apparatus for molding thermo- setting composite material[ P]. U.S. Patent: Application 11/010, 388, 2004-12-14.
  • 4Umeda K, Asari K, Kuriyama S. Method for continuously forming structural member[P]. U.S. Patent: 7,967,932, 2011-6-28.
  • 5Leipold M, Eiden M, Garner C E, et al. Solar sail technology devel- opment and demonstration [ J ]. Acta Astronantica, 2002, 52 ( 2 ) : 317-326.
  • 6Leipold M, Runge H, Sickinger C. Large sar membrane antennas with lightweight deployable booms[ C ]. 28th ESA Antenna Workshop on Space Antenna Systems and Technologies, 2005.
  • 7Block J, Straubel M, Wiedemann M. Ultralight deployable booms for solar sails and other large gossamer structures in space[ J]. Acta As- tronautica, 2010, 68(7): 984-992.
  • 8Seboldt W, Klimke M, Leipold M, et al. European Sail Tower SPS concept[ J]. Acta Astronautica, 2001, 55(5): 785-792.
  • 9白江波,熊峻江,高军鹏,益小苏,张子龙,何先成,刘志真,李雪芹.可折叠复合材料豆荚杆的制备与验证[J].航空学报,2011,32(7):1217-1223. 被引量:18
  • 10Siekinger C, Herbeek L, Strohlein T, et al. Lightweight deployable booms: design, manufacture, verification, and smart materials ap- plication [ C ]. Vancouver, Canada : 55th Imemational Astronautical Congress, IAF/IAA/IISL, 2004.

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