Effect of Stacking Sequence on Layer Defect of Carbon Fiber-Reinforced Plastics

WANG Gongdong; ZHONG Qiang

doi:10.16080/j.issn1671-833x.2017.07.101

您当前的位置：

首页 >

文章列表页 >

Effect of Stacking Sequence on Layer Defect of Carbon Fiber-Reinforced Plastics

更新时间：2026-04-17

- Effect of Stacking Sequence on Layer Defect of Carbon Fiber-Reinforced Plastics
- Aeronautical Manufacturing Technology Vol. 60, Issue 7, Pages: 101-104(2017)
- 作者机构：
  
  1. 沈阳航空航天大学航空航天工程学部,沈阳,110136
  2. 沈阳航空航天大学航空制造工艺数字化国防重点实验室,沈阳,110136
- 作者简介：
- 基金信息：
- DOI：10.16080/j.issn1671-833x.2017.07.101
  CLC：
- Published：2017
- 稿件说明：
移动端阅览
王共冬1,2，种强1，周丽1，熊需海2. 铺层顺序对碳纤维复合材料钻削分层制孔的影响[J]. 航空制造技术, 2017, 60(7): 101-104.

WANG Gongdong1,2, ZHONG Qiang1, ZHOU Li1, XIONG Xuhai2. Effect of Stacking Sequence on Layer Defect of Carbon Fiber-Reinforced Plastics. Aeronautical Manufacturing Technology, 2017, 60(7): 101-104.
王共冬1,2，种强1，周丽1，熊需海2. 铺层顺序对碳纤维复合材料钻削分层制孔的影响[J]. 航空制造技术, 2017, 60(7): 101-104. DOI： 10.16080/j.issn1671-833x.2017.07.101.

WANG Gongdong1,2, ZHONG Qiang1, ZHOU Li1, XIONG Xuhai2. Effect of Stacking Sequence on Layer Defect of Carbon Fiber-Reinforced Plastics. Aeronautical Manufacturing Technology, 2017, 60(7): 101-104. DOI： 10.16080/j.issn1671-833x.2017.07.101.

摘要

在碳纤维环氧树脂基复合材料的钻削制孔加工过程中会产生很多种类的缺陷，其中分层损伤是最难以控制的缺陷，严重影响机械连接的有效性和材料的使用性能。将铺层规则尤其是防分层规则应用于层合板铺层顺序优化中，使用Memetic 算法得出防止碳纤维板分层的铺层顺序，并设计CFRP 制孔试验加以论证。试验结果表明，复合材料铺层角度对分层缺陷有重要影响，优化后的碳纤维复合材料可有效减少分层、毛刺缺陷。

Abstract

In the process of carbon fiber reinforced plastics (CFRP) drilling

layer is the most important class of defect

which seriously affects the connection performance of the holes and the service life of materials. Rule especially antilayer rule is used for optimization design of laminated composite plate structures. The stacking sequence of composite laminate is optimized by applying Memetic algorithm

and drilling experiment of carbon fiber reinforced plastics is made to check the validity. The result indicates that the stacking sequence has great influence on layer

and the optimized composite laminate can effectively restrain layer and burrs.

关键词

Keywords

references

Views

381

下载量

CSCD

Alert me when the article has been cited

提交

Tools

Publicity Resources

Study on Properties of Discharge Crater of CFRP Under Single Pulse Discharge

Electromechanical Behavior of Open-Hole Three-Dimensional Angle-Interlock Woven Carbon Fiber Reinforced Polymer Under Tensile Loading

Research Progress on Matrix Composition Regulation of SiC/SiC Composites

Research Progress on Ceramic Matrix Composites for Aviation Applications

Modulation of Pore Structure and Properties in Phenolic Aerogels by Cationic Polyelectrolytes

Related Author

YANG Xiaodong

HUANG Xiaonan

Related Institution

School of Mechatronics Engineering, Harbin Institute of Technology

The platform construction and operation are provided by Beijing Founder electronics co., LTD 京ICP备09064830号-19 京公网安备11010802024621
It is recommended to read the content of this site in Chrome&IE9+. Please switch to extreme mode in browser 360.
Cookies We use cookies to help provide and enhance our service and tailor content. By continuing, you agree to the use of cookies.
Total Visits：34634 Visits Today：112

⁰