大尺寸整体C/SiC复合材料蒙皮骨架松动问题分析
作者:
作者单位:

北京航天长征飞行器研究所,北京 100076

作者简介:

通讯作者:

中图分类号:

TB33

基金项目:


Analysis on the Looseness of the Skin and Skeleton of Large-scale Integral Carbon/Silicon Carbide Composite
Author:
Affiliation:

Beijing Institute of Space Long March Vehicle, Beijing 100076

Fund Project:

  • 摘要
  • |
  • 图/表
  • |
  • 访问统计
  • |
  • 参考文献
  • |
  • 相似文献
  • |
  • 引证文献
  • |
  • 资源附件
  • |
  • 文章评论
    摘要:

    针对大尺寸整体C/SiC复合材料骨架和蒙皮结构在165 dB热噪声试验调试过程中出现的蒙皮松动问题进行分析,提出了蒙皮与骨架装配时空悬面积过大引起蒙皮呼吸振动幅度增加,从而导致噪声振动环境中蒙皮松动的现象。仿真分析表明,在相同的加速度激励下随着蒙皮与骨架局部空悬面积变大,位移响应增大约1.72倍;通过装配间隙为0.2、0.6、1 mm的3组平板试验件进行验证,当蒙皮与骨架间隙较大时,其胶层厚度也较大,经过多次热加载后,胶层粘接性能下降,蒙皮与骨架之间空悬现象显现,在振动激励下导致蒙皮松动。最后提出了大尺寸复合材料蒙皮与骨架装配时需保证最大间隙不超过0.3 mm的改进措施。

    Abstract:

    The skin looseness of large-scale integral carbon/silicon carbide composite skeleton and skin structure in 165 dB thermal noise test was analyzed. The mechanism of skin looseness in noise and vibration environment was proposed, which was caused by the increase of breathing vibration amplitude of skin due to the large free hanging area of skin and skeleton assmbly.The simulation results show that the displacement response increase about 1.72 times with the increase of local free hanging area of the skin and skeleton under the same acceleration excitation. Three groups of flat plate test pieces with assembly clearance of 0.2, 0.6 and 1 mm are used to verify that the skin looseness problem is repeated. When the gap between the skin and the skeleton is large, the thickness of the adhesive layer is also larger. After several times of thermal loading, the adhesive performance of the adhesive layer decreases, and the air suspension phenomenon between the skin and the skeleton appears, which leads to the skin loosening under the vibration excitation. Finally, the improvement measures are put forward to ensure that the maximum gap between the large-scale skin and the skeleton is not more than 0.3 mm.

    参考文献
    相似文献
    引证文献
引用本文

张利鹏,侯保江,辛克浩,孙亦璋,王成华.大尺寸整体C/SiC复合材料蒙皮骨架松动问题分析[J].宇航材料工艺,2021,51(4):154-158.

复制
分享
文章指标
  • 点击次数:
  • 下载次数:
  • HTML阅读次数:
  • 引用次数:
历史
  • 收稿日期:2021-05-19
  • 最后修改日期:2021-06-22
  • 录用日期:2021-06-24
  • 在线发布日期: 2021-08-25
  • 出版日期: 2021-08-30
第十一届航天复合材料成形与加工工艺技术中心交流会 征文通知

关闭