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Open Access

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

Yang CAOaYejun ZHUbWenfeng DINGa ( )Yutong QIUaLifeng WANGcJiuhua XUa
National Key Laboratory of Science and Technology on Helicopter Transmission, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
College of Engineering, Nanjing Agricultural University, Nanjing 210032, China
College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China

Peer review under responsibility of Editorial Committee of CJA.

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Abstract

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 comparative 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. Compared 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. Furthermore, under the current experimental conditions, the optimal ultrasonic vibration amplitude is determined as 6 μm, with which the minimum surface roughness is achieved.

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Chinese Journal of Aeronautics
Pages 332-345

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Cite this article:
CAO Y, ZHU Y, DING W, et al. Vibration coupling effects and machining behavior of ultrasonic vibration plate device for creep-feed grinding of Inconel 718 nickel-based superalloy. Chinese Journal of Aeronautics, 2022, 35(2): 332-345. https://doi.org/10.1016/j.cja.2020.12.039

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Received: 30 September 2020
Revised: 24 October 2020
Accepted: 01 December 2020
Published: 14 January 2021
© 2021 Chinese Society of Aeronautics and Astronautics and Beihang University.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).