固体力学与飞行器总体设计

三维全五向编织耳片接头力学性能试验研究

  • 刘振国 ,
  • 林强 ,
  • 亚纪轩 ,
  • 胡龙 ,
  • 王一博
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  • 北京航空航天大学 航空科学与工程学院, 北京 100083
林强 男,硕士研究生。主要研究方向:三维编织复合材料结构连接件工艺及力学性能。Tel.:010-82338049,E-mail:tarloy123@126.com;亚纪轩 男,硕士研究生。主要研究方向:三维编织复合材料切边力学性能。Tel.:010-82338049,E-mail:yajixuan@sina.cn;胡龙 男,博士。主要研究方向:先进三维编织复合材料工艺、性能及结构优化、复合材料细观力学。Tel.:010-82338049,E-mail:hulong0754@gmail.com;王一博 男,博士研究生。主要研究方向:先进三维编织复合材料工艺、性能及结构优化。Tel.:010-82338049,E-mail:wangyibo1111@163.com

收稿日期: 2015-08-17

  修回日期: 2015-09-29

  网络出版日期: 2015-11-03

基金资助

省部级项目

Experimental research on mechanical properties of 3D full 5-direactional braided composites lugs

  • LIU Zhenguo ,
  • LIN Qiang ,
  • YA Jixuan ,
  • HU Long ,
  • WANG Yibo
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  • School of Aeronautic Science and Engineering, Beihang University, Beijing 100083, China

Received date: 2015-08-17

  Revised date: 2015-09-29

  Online published: 2015-11-03

Supported by

Provincial/Ministerial Project Level

摘要

通过单向静力拉伸试验研究了三维全五向编织复合材料耳片接头的力学性能。试件选用T700-12K碳纤维采用四步法编织预制件,以TDE-85环氧树脂为基体,经树脂传递模塑(RTM)工艺固化成型。对两种几何尺寸、两种孔加工方式(编织预留孔和机械制孔)的三维全五向编织复合材料耳片接头试件的力学性能进行了试验研究。试验结果表明,同尺寸三维全五向编织预留孔接头的承载力是机械制孔接头承载力的6倍;对相同孔径及厚度的耳片,增大耳片宽度能大幅提升耳片承载力,但并不能显著提高其初始破坏载荷。

本文引用格式

刘振国 , 林强 , 亚纪轩 , 胡龙 , 王一博 . 三维全五向编织耳片接头力学性能试验研究[J]. 航空学报, 2016 , 37(7) : 2225 -2233 . DOI: 10.7527/S1000-6893.2015.0265

Abstract

The mechanical properties of the 3D full 5-directional braided composites lugs on axial tension are studied based on experiments. The 3D braided composites lugs used for the study are made of T700-12K carbon fiber braided by 4-step braiding technique and solidified with TDE-85 epoxy by resin transfer molding (RTM) technique. The mechanical properties of the experimental samples which consist of two geometries and two methods for the holes (drilled and braided separately) are investigated. The results of these experiments show that the strength of the braided hole lug is six times that of the drilled one lug for the same size and same braiding technique. For the same hole diameter and thickness lug, with the increase of the width of the lug, the final failure load increases significantly, but the initial failure load improves a little.

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