Study of tapping process of carbon fiber reinforced plastic composites/AA7075 stacks

被引:1
作者
D'Orazio, Alessio [1 ]
El Mehtedi, Mohamad [1 ]
Forcellese, Archimede [1 ]
Nardinocchi, Alessia [2 ]
Simoncini, Michela [3 ]
机构
[1] Univ Politecn Marche, Via Brecce Bianche, I-60100 Ancona, Italy
[2] HP Composites, Zona Ind, Via Lampo, I-63100 Frazione Campolungo, Ascoli Piceno, Italy
[3] Univ eCampus, Via Isimbardi 10, I-22060 Novedrate, CO, Italy
来源
PROCEEDINGS OF 21ST INTERNATIONAL ESAFORM CONFERENCE ON MATERIAL FORMING (ESAFORM 2018) | 2018年 / 1960卷
关键词
METAL-MATRIX COMPOSITES; PREDICTION; FORCES; OPERATIONS; TORQUE;
D O I
10.1063/1.5034906
中图分类号
O59 [应用物理学];
学科分类号
摘要
The present investigation aims at studying the tapping process of a three-layer stack constituted by two CFRP layers and a core plate in AA7075 aluminum alloy. The CFRP laminates were obtained by a pre-impregnated woven sample made up of T700 carbon fibers and a thermoset epoxy matrix. Tapping experiments were performed on a 5-axis machining center instrumented with a dynamometer to measure thrust force generated during process. A high-speed steel tool, coated with nanocomposite TiAlN, was used. According to the tool manufacturer recommendations, rotational speed and feed rate were 800 rpm and 1000 mm/min, respectively. Similar thrust force time history responses were obtained by tapping different holes, even though the vertical force increases with number of threaded holes. Furthermore, a quantitative evaluation of delamination at the periphery of entry holes was carried out. The delamination at the entry hole strongly increases with number of threaded holes.
引用
收藏
页数:6
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