An Exploration of Surface Integrity Remanufacturing for Aeroengine Components

Qiao Xiang, Yong He, Ting-hong Hou

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PDF(334 KB)
Front. Eng ›› 2016, Vol. 3 ›› Issue (2) : 107-114. DOI: 10.15302/J-FEM-2016025
ENGINEERING MANAGEMENT THEORIES AND METHODOLOGIES
ENGINEERING MANAGEMENT THEORIES AND METHODOLOGIES

An Exploration of Surface Integrity Remanufacturing for Aeroengine Components

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Abstract

Surface integrity is the major factor impacting on the operation quality, service life and reliability of the aeroengine components. The surface integrity of aeroengine component is damaged by the failures such as crack, deformation, oxidation, corrosion, erosion, and microstructural degeneration. It adopts advanced remanufacturing technologies to restore or improve the surface integrity and regenerate these high value parts. This paper firstly puts forward the concept, namely surface integrity remanufacturing for aeroengine components, and its connotation. The key remanufacturing technologies have been developed to repair the components with surface damages. Ultimately, some application examples of surface integrity remanufacturing technologies as well as their effects in aeroengine maintenance are introduced. The discarded components have been reused and their service lives have been extended and their reliability has been increased by implementing surface integrity remanufacturing. It has realized “The Repaired Components Outpacing the New Ones”, material saving, energy saving, and emission reduction.

Keywords

aeroengine component / surface integrity / remanufacturing / surface integrity remanufacturing

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Qiao Xiang, Yong He, Ting-hong Hou. An Exploration of Surface Integrity Remanufacturing for Aeroengine Components. Front. Eng, 2016, 3(2): 107‒114 https://doi.org/10.15302/J-FEM-2016025

References

[1]
ANSI-B211.1. (1986). American national standards on surface integrity. Washington, D.C: American National Standards Institute.
[2]
Axinte, D. A., & Dewes, R. C. (2002). Surface integrity of hot work tool steel after high speed milling experimental data and empirical models. Journal of Materials Processing Technology, 127, 325–335.
[3]
Biller, S. (2011). Innovation in global manufacturing: Sustainability for business success. Como Lake:World Manufacturing Forum.
[4]
Demo, W., & Ferrigno, S. J. (1992). Brazing method helps repair aircraft gas-turbine nozzles. Advanced Materials & Processes, 141, 43–45.
[5]
Duval, D., Owczarski, W., Paulonis, D., & Schaefer, R. (1978). Metallic filler material. U.S. Patent 4, 073, 639.
[8]
Ellison, K. A., Lowden, P., Liburdi, J., & Boone, D. H. (1993). Repair joints in nickel-based superalloys with improved hot corrosion resistance. In: Proceedings of International Gas Turbine and Aeroengine Congress and Exposition. Cincinnati, 93-GT-247.
[6]
Field, M., & Kahles, J. F. (1971). Review of surface integrity of machined components. Annals CIRP, 20, 153–163.
[7]
Griffiths, B. J. (2001). Manufacturing surface technology, surface integrity and functional performance. London: Manufacturing Engineering Modular Series, Penton Press.

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2016 The Author(s) 2016. This article is published with open access at engineering.cae.cn
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