首页 | 本学科首页   官方微博 | 高级检索  
     

自动铺丝末端缺陷角度对层合板拉伸性能的影响
引用本文:丰亮宽,杨涛,杜宇,李韦清,原文慧. 自动铺丝末端缺陷角度对层合板拉伸性能的影响[J]. 宇航材料工艺, 2020, 50(3): 62-68
作者姓名:丰亮宽  杨涛  杜宇  李韦清  原文慧
作者单位:天津市现代机电装备技术重点实验室,天津 300387;天津工业大学机械工程学院,天津 300387,天津市现代机电装备技术重点实验室,天津 300387;天津工业大学机械工程学院,天津 300387,天津工业大学机械工程学院,天津 300387,天津工业大学机械工程学院,天津 300387,天津工业大学机械工程学院,天津 300387
基金项目:天津市应用基础与前沿技术研究计划重点项目(11JCZDJC23000)
摘    要:自动纤维铺放(AFP)工艺能够有效制造大型复合材料构件,但在铺放过程中因为丝束末端等断面而出现不同角度内嵌缺陷。为解决相关问题,按照[(90°/0°)5/90°]和[(0°/90°)5/0°]的铺层顺序,在0°和90°铺层内分别设置不同丝束末端角度的孔隙缺陷或重叠缺陷。结果表明:不同角度纤维铺层内嵌不同角度缺陷时,导致复合材料构件差异明显。在90°纤维铺层方向上,内嵌90°孔隙缺陷和90°重叠缺陷时,试件拉伸强度最高,拉伸强度比分别为90. 89%和90. 11%。在0°纤维铺层方向上,内嵌±30°孔隙缺陷和30°重叠缺陷时,试件拉伸强度最高,拉伸强度比分别为28. 48%和50. 71%。

关 键 词:复合材料  自动铺放技术  缺陷  力学性能
收稿时间:2019-06-05
修稿时间:2019-08-14

Influence of Defect Angle at the End of Tows on the Tensile Properties of Laminates by Automated Placement
FENG Liangkuan,YANG Tao,DU Yu,LI Weiqing and YUAN Wenhui. Influence of Defect Angle at the End of Tows on the Tensile Properties of Laminates by Automated Placement[J]. Aerospace Materials & Technology, 2020, 50(3): 62-68
Authors:FENG Liangkuan  YANG Tao  DU Yu  LI Weiqing  YUAN Wenhui
Abstract:Automatic fiber placement (AFP) technology could manufacture large composite components effectively,but there are different angle embedded defects due to the same cross-section at the end of the tow in the process of placement.In order to solve the related problems,according to the laying sequence of [(90°/0°)5/90°] and [(0°/90°)5/0°],the gap defects or overlapping defects with different end angles of the tow were set in the 0° and 90° laying sequence respectively.The experimental results show that the difference of the composite components is obvious when the defects are embedded in different angles.In the direction of 90° fiber layer,when 90° void defect and 90° overlapping defect are embedded, the tensile strength of the specimen is the highest,and the tensile strength ratio is 90.89% and 90.11%,respectively.In the direction of 0° fiber layer,the tensile strength of the specimen is the highest when embedded with ± 30° gap defect and 30° overlapping defect,and the tensile strength ratio is 28.48% and 50.71% respectively.
Keywords:Composites  Automated fiber placement  Defects  Mechanical property
本文献已被 CNKI 等数据库收录!
点击此处可从《宇航材料工艺》浏览原始摘要信息
点击此处可从《宇航材料工艺》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号