李涵, 郭占一. 轻型复合材料上层建筑与钢质船体连接结构设计分析[J]. 中国舰船研究, 2020, 15(4): 36-45. DOI: 10.19693/j.issn.1673-3185.01565
引用本文: 李涵, 郭占一. 轻型复合材料上层建筑与钢质船体连接结构设计分析[J]. 中国舰船研究, 2020, 15(4): 36-45. DOI: 10.19693/j.issn.1673-3185.01565
LI Han, GUO Zhanyi. Design and analysis of joints between light composite superstructure and steel hull[J]. Chinese Journal of Ship Research, 2020, 15(4): 36-45. DOI: 10.19693/j.issn.1673-3185.01565
Citation: LI Han, GUO Zhanyi. Design and analysis of joints between light composite superstructure and steel hull[J]. Chinese Journal of Ship Research, 2020, 15(4): 36-45. DOI: 10.19693/j.issn.1673-3185.01565

轻型复合材料上层建筑与钢质船体连接结构设计分析

Design and analysis of joints between light composite superstructure and steel hull

  • 摘要:
      目的  设计可靠、有效的复合材料上层建筑与钢质主船体连接结构是复合材料上层建筑在舰船上应用面临的难点之一。
      方法  综合考虑各种连接结构的优、缺点,采用“π”型双螺栓、双剪切连接形式设计复合材料与钢连接结构。提取上层建筑与主船体连接位置在浪花飞溅冲击载荷作用下的垂向反力及弯矩作为设计载荷,利用有限元软件ANSYS校核2种工况下的强度。
      结果  计算结果表明,各项需要考核的应力指标均小于材料的极限应力,并且保留了一定的安全裕度,所设计的连接结构较为合理、可靠。
      结论  在2种设计工况的强度校核中,泡沫芯材剪切应力的安全裕度最小;对于芯材较厚的夹芯板,泡沫芯材的剪切应力是薄弱环节,故在设计复合材料夹芯板连接结构时,应重点关注芯材的剪切问题。

     

    Abstract:
      Objectives  Designing effective and reliable composite and steel joints is one of the difficulties faced in the application of composite superstructure in ships.
      Methods  Considering the advantages and disadvantages of various joint structures, the π-type composite and steel joints were designed by using the double-bolt and double-shear. With the vertical reaction force and bending moments of the connecting position between the superstructure and the main hull under the action of wave loads extracted as design loads, the strength under two design conditions was checked by the finite element software ANSYS.
      Results  The calculation results show that the stresses checked are less than the ultimate stresses of the material, and a certain safety margin is retained. The designed joints are reasonable and reliable.
      Conclusions  In the strength check under the two design conditions, the safety margin of the shear stress of foam core is the smallest. Therefore, it is noted that failure of shear of core material for the sandwich panels with thicker core material is the main failure mode.

     

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