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Influence of oxidation on the cracks of DZ125L nickel-based superalloy thin-walled parts in laser metal direct forming

Bin He (State Key Laboratory for Manufacturing Systems Engineering, Xi'an Jiaotong University, Xi'an, China)
Dichen Li (State Key Laboratory for Manufacturing Systems Engineering, Xi'an Jiaotong University, Xi'an, China)
Anfeng Zhang (State Key Laboratory for Manufacturing Systems Engineering, Xi'an Jiaotong University, Xi'an, China)
Zhongliang Lu (State Key Laboratory for Manufacturing Systems Engineering, Xi'an Jiaotong University, Xi'an, China)
Jiangbo Ge (State Key Laboratory for Manufacturing Systems Engineering, Xi'an Jiaotong University, Xi'an, China)
Doan Tat Khoa (State Key Laboratory for Manufacturing Systems Engineering, Xi'an Jiaotong University, Xi'an, China)

Rapid Prototyping Journal

ISSN: 1355-2546

Article publication date: 30 September 2013

484

Abstract

Purpose

The purpose of this paper is to investigate the influence of the oxidation on the cracks of DZ125L nickel-based superalloy thin-walled parts in laser metal direct forming (LMDF).

Design/methodology/approach

Thin-walled cylinders were fabricated in protective atmosphere with different oxygen contents in order to reveal the influence of oxidation on the morphology of cracks. The influence of oxidation on the cracks was investigated in detail by measuring the wall thicknesses of cylinders, the residual stress in the top surface of the cylinders and the composition of the cracks. Finally, the validity of the results was verified by fabricating a thin-walled turbine blade in protective atmosphere.

Findings

The experimental results showed that wall thickness fluctuation of cylinders, unequal residual stress distribution of cylinders and the oxides in the crack were all the critical factors which led to crack of DZ125L thin-walled parts. Thin-walled turbine blades with no cracks can be fabricated when the oxygen content was about less than 150 ppm in protective atmosphere.

Research limitations/implications

The appropriate oxygen content in protective atmosphere is helpful for fabricating thin-walled parts of nickel-based superalloy like DZ125L, and the results can show what will happen at different oxygen levels. Moreover, the results show that the cracks can be eliminated as the oxygen content reduce to less than 150 ppm rather less than 10 ppm or even less, which can reduce the cost of protective gas as forming thin-walled parts of nickel-based superalloy such as DZ125L.

Practical implications

The appropriate oxygen content in protective atmosphere is helpful for fabricating thin-walled parts of nickel-based superalloy like DZ125L. However, when heavy solid parts of some other material other than DZ125L were fabricated, the oxygen content of less than 150 ppm may be not suitable.

Originality/value

The influence of oxidation on the cracks of DZ125L thin-walled parts in LMDF was investigated in detail, and a DZ125L thin-walled turbine blade with no cracks was fabricated by adjusting the oxygen content in protective atmosphere.

Keywords

Acknowledgements

The authors gratefully acknowledge the State Basic Research Key Projects (973) of China through Grant No. 2007CB707704, Program for Changjiang Scholars and Innovative Research Team in University (PCSIRT0646), National Natural Science Foundations of China through Grant No. 50675171 and National Natural Science Foundations of China through Grant No. 51275392.

Citation

He, B., Li, D., Zhang, A., Lu, Z., Ge, J. and Tat Khoa, D. (2013), "Influence of oxidation on the cracks of DZ125L nickel-based superalloy thin-walled parts in laser metal direct forming", Rapid Prototyping Journal, Vol. 19 No. 6, pp. 446-451. https://doi.org/10.1108/RPJ-12-2011-0133

Publisher

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Emerald Group Publishing Limited

Copyright © 2013, Emerald Group Publishing Limited

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