Vibration coupling effects and machining behavior of ultrasonic vibration plate device for creep-feed grinding of Inconel 718 nickel-based superalloy

被引:132
作者
Cao, Yang [1 ]
Zhu, Yejun [2 ]
Ding, Wenfeng [1 ]
Qiu, Yutong [1 ]
Wang, Lifeng [3 ]
Xu, Jiuhua [1 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Natl Key Lab Sci & Technol Helicopter Transmiss, Nanjing 210016, Peoples R China
[2] Nanjing Agr Univ, Coll Engn, Nanjing 210032, Peoples R China
[3] Nanjing Univ Aeronaut & Astronaut, Coll Aerosp Engn, Nanjing 210016, Peoples R China
基金
中国国家自然科学基金;
关键词
Apparent elastic method; Machining behavior; Ultrasonic vibration-assisted grinding; Ultrasonic vibration plate device; Vibration coupling effects; FINITE-ELEMENT SIMULATION; FORCE; MODEL; MICROSTRUCTURE; LUBRICATION; COMPOSITES; MECHANISM; DESIGN; ANGLE; CFRP;
D O I
10.1016/j.cja.2020.12.039
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Ultrasonic vibration-assisted grinding (UVAG) is an effective and promising method for machining of hard-to-cut materials. This article proposed an ultrasonic vibration plate device enabling the longitudinal full-wave and transverse half-wave (L2T1) vibration mode for UVAG. The characteristics of two-dimensional coupled vibration in different directions were analyzed on the basis of apparent elastic method and finite element method. Furthermore, a correction factor was applied to correct the frequency error caused by the apparent elastic method. Finally, the com-parative experiments between the conventional creep-feed grinding and UVAG of Inconel 718 nickel-based superalloy were carried out. The results indicate that the apparent elastic method with the correction factor is accurate for the design of plate device under the L2T1 vibration mode. Com-pared with the conventional creep-feed grinding, the UVAG causes the reduction of grinding force and the improvement of machined surface quality of Inconel 718 nickel-based superalloy. Further-more, under the current experimental conditions, the optimal ultrasonic vibration amplitude is determined as 6 lm, with which the minimum surface roughness is achieved. (c) 2021 Chinese Society of Aeronautics and Astronautics and Beihang University. Production and hosting by Elsevier Ltd. This is an open access article under the CC BY-NC-ND license (http://creativecommons. org/licenses/by-nc-nd/4.0/).
引用
收藏
页码:332 / 345
页数:14
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