Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
13419299 | Composite Structures | 2020 | 20 Pages |
Abstract
The Ti/CFRP stacks are widely used in the field of aerospace since their excellent properties. However, it is quite a challenge work to obtain quality holes in one-shot drilling due to the tremendous differences in material properties of Ti and CFRP. In this paper, a novel step drill structure which could reduce the delamination and burr by controlling step diameters ratio is proposed. Considering the geometric structure of step drill and the properties of the materials, the cutting loads prediction model and three simplified drill-exit damage model are established in order for confirming critical condition of the defect. Consequently, the relationship between the burr height, delamination length and the diameter of step-drill bit are clarified. Then a novel step drill with variation step ratio is designed. And geometrical analysis proved that it could effectively improve the quality of drill-exit. In addition, comparative experiments were carried out, the result showed that the proposed step drill structure can effectively reduce the damages such as the burr and delamination as expected.
Keywords
Related Topics
Physical Sciences and Engineering
Engineering
Civil and Structural Engineering
Authors
Zhen-yuan Jia, Chong Zhang, Fu-ji Wang, Rao Fu, Chen Chen,