| 引用本文: | 张金栋,于海涛,李龙,王庆有,魏鹏,肇研.光纤布拉格光栅监测CF3052/5224复合材料成型过程研究[J].材料科学与工艺,2015,23(4):17-22.DOI:10.11951/j.issn.1005-0299.20150403. |
| ZHANG Jindong,YU Haitao,LI Long,WANG Qingyou,WEI Peng,ZHAO Yan.Study of monitoring CF3052/5224 composites molding process by optical fiber Bragg grating[J].Materials Science and Technology,2015,23(4):17-22.DOI:10.11951/j.issn.1005-0299.20150403. |
|
| 本文已被：浏览 1982次 下载 1288次 |
码上扫一扫！ |
|
|
| 光纤布拉格光栅监测CF3052/5224复合材料成型过程研究 |
|
张金栋1,于海涛2,李龙1,王庆有2,魏鹏3,肇研1
|
|
(1.北京航空航天大学 材料科学与工程学院,北京100191;2.哈尔滨飞机工业集团有限责任公司, 哈尔滨150066;3.北京航空航天大学 仪器科学与光电工程学院,北京100191)
|
|
| 摘要: |
| 温度与应变是监测复合材料热压罐固化成型工艺两个最重要的表征参数,利用光纤布拉格光栅传感原理,采用毛细钢管封装的方法,制备了完全屏蔽应变信号的温度传感器,将温度传感器和应变传感器同时埋植在复合材料内部,实现了对热压罐成型全过程的实时监测,获得了复合材料成型过程中的内部温度和应变信息.对复合材料平板件和T型加筋板三角填充区域进行的温度监测结果表明,复合材料内部温度变化较罐内温度有一定滞后,传统成型工艺控制给出的加压点偏早,可能引起复合材料贫胶等缺陷.应变监测结果表明,平板件内部的应变变化主要反应树脂固化过程中的物理化学变化,在T型加筋板三角填充区域,应变监测在自然冷却阶段出现了不同于平板件的应变“回弹”现象,一定程度上反映出该区域在成型过程中容易出现缺陷的原因. |
| 关键词: 复合材料 光纤布拉格光栅 工艺控制 固化监测 T型加筋板 |
| DOI：10.11951/j.issn.1005-0299.20150403 |
| 分类号:TB332 |
| 基金项目:国防基础科研计划资助项目(A0520110033). |
|
| Study of monitoring CF3052/5224 composites molding process by optical fiber Bragg grating |
|
ZHANG Jindong1, YU Haitao2, LI Long1, WANG Qingyou2, WEI Peng3, ZHAO Yan1
|
|
(1.School of Materials and Engineering,Beihang University,Beijing 100191,China;2. Harbin Aircraft Industry Group Company Limited,Harbin 150066,China;3. School of Instrumentation Science and Opto-electronics Engineering,Beihang University,Beijing 100191,China)
|
| Abstract: |
| Temperature and strain are two of the most important parameters for monitoring the autoclave curing process of composites. The temperature sensor was encapsulated by a steel capillary pipe to shield strain signals. A temperature sensor and a strain sensor were implanted inside the composite simultaneously to monitor the autoclave process in real time so as to obtain internal temperature and strain information. A plate laminate and the triangular region of a T-stiffened panel were monitored. The monitoring results show that the temperature increaseinside the composite was delayed due to the heat transfer. Thus, the pressure applying moment normally determined by the autoclave′s temperature may be improper. This phenomenon may cause the defects such as resin starvation. Strain monitoring results show that the strain changes inside the plate laminate can reflect the physical and chemical varieties of the resin during the curing process. In the triangular region of the T-stiffened panel, there is a "strain rebound" phenomenon during the natural cooling stage, which indicates that the process-induced defects are prone to occur in the triangular region of a T-stiffened panel. |
| Key words: composites fiber Bragg grating process control cure monitoring T-stiffened panels |
