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缝合制备有机硅复合材料及其弯曲性能研究

胡春平 姜波 刘丽 周敬杰 黄玉东

固体火箭技术2011,Vol.34Issue(6):786-788,793,4.
固体火箭技术2011,Vol.34Issue(6):786-788,793,4.

缝合制备有机硅复合材料及其弯曲性能研究

Fabrication and bending property of stitched silicone composite

胡春平 1姜波 2刘丽 1周敬杰 1黄玉东2

作者信息

  • 1. 哈尔滨工业大学化工学院,哈尔滨150001
  • 2. 东北林业大学理学院,哈尔滨150040
  • 折叠

摘要

Abstract

The influence of stitched process on the flexural strength of vycor fiber/silicone composites was studied. It is showed that the flexural strength of composite fabricated by two processes is nearly identical at room temperature. The property of composite fabricated by stitched process is obviously higher than that of the unstitched one after treated at 500℃ for 10 min. Instead, the property of composite fabricated by stitched process is lower than that of the unstitched one after treated at 700℃ for 10 min. The results show that the stitched process can effectively prevent the delamination of composites below 500℃. But the property of composites becomes worse with the degradation of PBO fibers at higher temperature. The flexural strength of composite is lower than that of unstitched ones at 700℃.ess

关键词

缝合/硅树脂复合材料/弯曲性能

Key words

stitching /silicone composite/ bending property

分类

航空航天

引用本文复制引用

胡春平,姜波,刘丽,周敬杰,黄玉东..缝合制备有机硅复合材料及其弯曲性能研究[J].固体火箭技术,2011,34(6):786-788,793,4.

基金项目

长江学者奖励计划 ()

国家自然科学基金项目(No.51073047 ()

No.91016015 ()

No.50903025) ()

东北林业大学中央高校基本科研业务费专项资金资助(No.DL09AB13). (No.DL09AB13)

固体火箭技术

OA北大核心CSCDCSTPCD

1006-2793

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