Repair Process Development for Blisk Applications in Aero Engines

Canadian Institute of Mining, Metallurgy and Petroleum
T. Haubold L. Zhu C. Zimmermann C. Mattern I. Kelbassa M. Dahmen S. Kaierle
Organization:
Canadian Institute of Mining, Metallurgy and Petroleum
Pages:
9
File Size:
1293 KB
Publication Date:
Jan 1, 2006

Abstract

Application of integrally bladed disks (blisks) is of increasing interest in compressors of aero engines. Blisks are preferred due to their potential for size and weight reduction, for increased performance and for reduced manufacturing costs compared to conventionally bladed disks. In case of a damage the blisk aerofoils cannot be simply replaced. If the damage is beyond acceptance or blending limits refurbishment is possible only by scrapping the whole blisk assembly, or more cost effective by the application of advanced weld repair methods. Weld repair of blisk aerofoils is challenging as it affects a critical part with specific requirements regarding its mechanical integrity, and as the accessibility is usually limited. The paper describes the ongoing development of advanced weld repair processes as part of a comprehensive repair strategy which have been developed for small-sized blisk assembly to give competitive maintenance cost.
Citation

APA: T. Haubold L. Zhu C. Zimmermann C. Mattern I. Kelbassa M. Dahmen S. Kaierle  (2006)  Repair Process Development for Blisk Applications in Aero Engines

MLA: T. Haubold L. Zhu C. Zimmermann C. Mattern I. Kelbassa M. Dahmen S. Kaierle Repair Process Development for Blisk Applications in Aero Engines. Canadian Institute of Mining, Metallurgy and Petroleum, 2006.

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