期刊文献+

尺寸高稳定性复合材料桁架结构的研制 被引量:10

Development of a high dimensional stable composite truss
下载PDF
导出
摘要 介绍了某卫星复合材料桁架结构的研制情况,通过材料选择、铺层设计、材料的热膨胀系数测试与分析,制造了高精度的复合材料桁架,并测量了结构的热变形。测量结果表明:采用高模量碳纤维复合材料能够制造出热变形只有微米级的高稳定结构。这是针对超稳卫星平台所需的尺寸高稳定性结构的首次成功探索。文章最后对进一步降低结构热变形、提高尺寸稳定性和测量精度提出了建议。 A high dimensional stable composite truss used for a certain satellite is discussed in this paper. Through the material selection, the ply design, and the CTE test & analysis, a high precision composite truss is manufactured, and the thermal deformation of the truss is measured. It is shown that the high dimensional stable structure made of high modulus CFRP with micrometer level accuracy can be obtained through an appropriate ply design. Some suggestions are made for reducing the thermal deformation and improving the dimensional stability & measurement accuracy. It is the first successful practice of the high dimensional stable composite structure being used for the ultra-stable satellite platform.
出处 《航天器环境工程》 2016年第3期229-234,共6页 Spacecraft Environment Engineering
基金 国家自然科学基金项目(编号:41274041)
关键词 尺寸高稳定性 复合材料 桁架 热膨胀系数 微变形测量 high dimensional stability composite materials truss coefficient of thermal expansion(CTE) micro-deformation measurement
  • 相关文献

参考文献17

  • 1Neam D C, Gerber J D. Structural design and analysis foran ultra low CTE optical bench for the Hubble spacetelescope corrective optics[J]. SPIE: Design of OpticalInstruments, 1992, 1690: 273-286.
  • 2Casciello A, Weigel T, Raunhardt M, et al. Ultra stableoff-axis telescope: lessons learnt from the optical designto the correlation of the test results[J]. Proc of SPIE,2012, 8550: 855017-1~855017-6.
  • 3Devilliers C, Nivet M, Coperet H. Advanced carbon/carbon material for space telescopes structures[C]∥52ndInternational Astronautical Congress. Toulouse, France,2001-10.
  • 4Skullney W E, Kreitz H M, Harold M J. Structural design of the MSX spacecraft[J]. Johns Hopkins APL TechnicalDigest, 1996, 17(1): 59-74.
  • 5Stute T, Wulz G, Scheulen D. Recent developments ofadvanced structures for space optics at Astrium Germany[J].Proc of SPIE. Bellingham, USA, 2003, 5179: 292-302.
  • 6Lutz M, Comillon L, Vitupier Y. Evaluation ofultrastable carbon/carbon sandwich structures joinedwith ceramic cement[C]//61st International AstronauticalCongress. Prague, CZ. IAC-10-C2.4.10: 1-4.
  • 7Edeson R, Aglietti G S, Tatnall A R L. Conventionalstable structures for space optics: the state of the art[J].Acta Astronautica, 2010, 66: 13-32.
  • 8Schapery R A. Thermal expansion coefficients ofcomposite materials based on energy principles[J].Composite Materials, 1968, 2(3): 380-404.
  • 9Chamis C C. Simplified composite micromechanicsequations for hygral thermal and mechanical properties[J].SAMPE Quarterly, 1984, 15(3): 14-23.
  • 10Nawab Y, Jacquemin F, Casari P, et al. Study of variationof thermal expansion coefficients in carbon/ epoxylaminated composite plates[J]. Composites, Part B:Engineering, 2013, 50: 144-149.

二级参考文献13

共引文献1

同被引文献102

引证文献10

二级引证文献26

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