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Full Length Article | Open Access

An electrochemical machining method for aero-engine blades based on four-directional synchronous feeding of cathode tools

Jia LIU( )Libing HUIDongqian JIAYan LIUDi ZHU
College of Mechanical and Electrical Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China

Peer review under responsibility of Editorial Committee of CJA.

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Abstract

Blades are critical components of modern aero-engine. Among the many characteristic structures of the blade, the leading/trailing edges are key structures that have the greatest influence on the aerodynamic effect and power conversion of the blade. Electrochemical machining (ECM) is regarded as one of the most important techniques in blade manufacturing due to its process characteristics of high material removal rates, virtually no tool wear, and no areas of thermal or mechanical damage to the workpiece rim zones. Herein, an ECM method based on the four-directional synchronous feeding of four cathode tools is proposed to improve the machining accuracy of the leading and trailing edges of the blade. During blade ECM using this method, four cathode tools feed toward the basin/back surfaces and leading/trailing edges respectively. The dynamic processing simulation and flow field simulation results of the ECM process show that the proposed method eliminates the sharp changes in the electric field and electrolyte flow field at the leading and trailing edges seen in traditional machining methods. Thus, the electric field and flow field stability of the leading and trailing edges at the final stage of machining is greatly improved. Experimental comparison of the conventional and proposed ECM methods showed that four-directional synchronous feeding results in improved profile accuracy over repeated machining processes and good surface quality.

References

1

Hamakhan IA, Korakianitis T. Aerodynamic performance effects of leading-edge geometry in gas-turbine blades. Appl Energy 2010;87:1591–601.

2

Zhong JJ, Han SB, Lu HW, et al. Effect of tip geometry and tip clearance on aerodynamic performance of a linear compressor cascade. Chin J Aeronaut 2013;26(3):583–93.

3

Zhang WH, Zou ZP, Ye J. Leading-edge redesign of a turbomachinery blade and its effect on aerodynamic performance. Appl Energy 2012;93:655–67.

4

Ma C, Gao LM, Wang HH, et al. Influence of leading edge with real manufacturing error on aerodynamic performance of high subsonic compressor cascades. Chin J Aeronaut 2021;34(6):220–32.

5

Ezugwu EO, Bonney J, Yamane Y. An overview of the machinability of aeroengine alloys. J Mater Process Technol 2003;134:233–53.

6

Pradhan S, Singh S, Prakash C, Królczyk G, Pramanik A, Pruncu CI. Investigation of machining characteristics of hard-to-machine Ti-6Al-4V-ELI alloy for biomedical applications. J Mater Res Technol 2019;8:4849–62.

7

Aspinwal DK, Dewes RC, Mantle AL. The machining of γ-TiAl intermetallic alloys. CIRP Ann - Manuf Technol 2005;54:99–104.

8

Suárez A, Veiga F, Polvorosa R, et al. Surface integrity and fatigue of non-conventional machined Alloy 718. J Manuf Process 2019;48:44–50.

9

Rajurkar KP, Sundaram MM, Malshe AP. Review of electrochemical and electrodischarge machining. Procedia CIRP 2013;6:13–26.

10

Klocke F, Klink A, Veselovac D, Aspinwall DK, et al. Turbomachinery component manufacture by application of electrochemical, electro-physical and photonic processes. CIRP Ann 2014;63:703–26.

11

Zhu D, Liu J, Wang DY, et al. Pulse dynamic electrochemical machining. Acta Aeronaut Astronaut Sin 2022;43 525959.

12

Xu ZY, Wang YD. Electrochemical machining of complex components of aero-engines: developments, trends, and technological advances. Chin J Aeronaut 2021;34(2):28–53.

13

Demirtas H, Yilmaz O, Kanber B. Experimental investigation of the effects of dedicated electrochemical machining parameters on freeform surface machining. J Manuf Process 2019;43:244–52.

14

Brusilovski Z. Adjustment and readjustment of electrochemical machines and control of the process parameters in machining shaped surfaces. J Mater Process Technol 2008;196:311–20.

15

Paczkowski T, Zdrojewski J. Monitoring and control of the electrochemical machining process under the conditions of a vibrating tool electrode. J Mater Process Technol 2017;244:204–14.

16

Fujisawa T, Inaba K, Yamamoto M, et al. Multiphysics simulation of electrochemical machining process for three-dimensional compressor blade. J Fluids Eng 2008;130 081602.

17

Li ZY, Niu ZW. Convergence analysis of the numerical solution for cathode design of aero-engine blades in electrochemical machining. Chin J Aeronaut 2007;20(6):570–6.

18

Ernst A, Heib T, Hall T, et al. Simulation of the tool shape design for the electrochemical machining of jet engine vanes. Procedia CIRP 2018;68:762–7.

19

Liu J, Xu ZY, Wan LK, et al. Design and experiment of electrolyte flow mode in electrochemical machining of blisk. Acta Aeronaut Astronaut Sin 2014;35:259–67.

20

Klocke F, Zeis M, Harst S, et al. Modeling and simulation of the electrochemical machining (ECM) material removal process for the manufacture of aero engine components. Procedia CIRP 2013;8:265–70.

21

Klocke F, Harst S, Zeis M, et al. Modeling and simulation of the microstructure evolution of 42CrMo4 steel during electrochemical machining. Procedia CIRP 2018;68:505–10.

22

Klocke F, Zeis M, Klink A. Interdisciplinary modelling of the electrochemical machining process for engine blades. CIRP Ann 2015;64:217–20.

23

Zhu D, Zhu D, Xu ZY, et al. Trajectory control strategy of cathodes in blisk electrochemical machining. Chin J Aeronaut 2013;26(4):1064–70.

24

Zhu D, Liu C, Xu ZY, et al. Cathode design investigation based on iterative correction of predicted profile errors in electrochemical machining of compressor blades. Chin J Aeronaut 2016;29(4):1111–8.

25

Wang H, Zhu D, Liu J. Improving the accuracy of the blade leading/trailing edges by electrochemical machining with tangential feeding. CIRP Ann 2019;68:165–8.

26

Wang H, Liu J, Zhu D. A study of precision current efficiency curve measurement with a casing-type anode. Appl Sci 2021;11:1425.

27

Kuzmin D, Mierka O, Turek S. On the implementation of the k–ε turbulence model in incompressible flow solvers based on a finite element discretisation. Int J Comput Sci Math. 2007;1:193–206.

Chinese Journal of Aeronautics
Pages 380-391
Cite this article:
LIU J, HUI L, JIA D, et al. An electrochemical machining method for aero-engine blades based on four-directional synchronous feeding of cathode tools. Chinese Journal of Aeronautics, 2023, 36(9): 380-391. https://doi.org/10.1016/j.cja.2022.10.003

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Received: 08 July 2022
Revised: 27 July 2022
Accepted: 27 August 2022
Published: 21 October 2022
© 2022 Chinese Society of Aeronautics and Astronautics.

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

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