Application of Laser Shock Processing to Improving the Fatigue Performance of Compressor Blade

Qi Peng Li; Ying Hong Li; Wei Feng He; Wei Li; Yu Qin Li

doi:10.4028/www.scientific.net/AMR.135.184

Paper Titles

Researches on Burr Formation in Milling Al-Alloy
p.164

Research on Thermal Error Modeling of CNC Machine Tool
p.170

The Analysis of Fracture Formation on Exit Edge in Pricision Machining
p.174

Study on the Optimized Blanking Allowance of Fine-Blanking with Negative Clearance for AISI-1020 and AISI-1045
p.179

Application of Laser Shock Processing to Improving the Fatigue Performance of Compressor Blade
p.184

Process Parameters Optimization for Micro-Arc Oxidation of Hot-Dip Aluminum Coating on Stainless Steel
p.190

Progress in Theory and Application Research on Microscale Laser Shock Peening
p.194

Numerical Simulation of Temperature Field for Rack Grind-Hardening
p.200

Study on Laser-Clad Al/Cr₃C₂ Compound Powders on the Titanium Alloy Substrate
p.205

HomeAdvanced Materials ResearchAdvanced Materials Research Vol. 135Application of Laser Shock Processing to Improving...

Application of Laser Shock Processing to Improving the Fatigue Performance of Compressor Blade

Abstract:

The vibration strength under allowable value leads to the failure of compressor blade of certain aeroengine. In order to solve the problem, laser shock processing on blade was studied. First, the processed part of blade as well as the laser shock processing (LSP) parameters was established. Second, the influence of LSP and tumbling to the vibrate fatigue capability of blades were researched according to the application of the project. Third, the strengthening mechanism of LSP on improving the fatigue performance of the blade was studied. The results show that, LSP is consistently dependable and can prolong the vibration fatigue life of the blade efficiently. LSP can be placed after tumbling or directly replace it during the manufacturing of blade. The grain refinement, higher hardness and compressive residual stress are the three main reasons that enhance the fatigue capability of blade.

You might also be interested in these eBooks

Surface Finishing Technology and Surface Engineering II

View Preview

Info:

Periodical:

Advanced Materials Research (Volume 135)

Pages:

184-189

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.135.184

Citation:

Cite this paper

Online since:

October 2010

Authors:

Qi Peng Li, Ying Hong Li, Wei Feng He, Wei Li, Yu Qin Li

Keywords:

Compressor Blade, Laser Shock Processing (LSP), Tumbling, Vibration Fatigue Life

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

References

[1] Q.P. Li: Laser Shock Processing in Oblique Angle on Compressor Blades of Certain Aeroengine (Air Force Engineering University, China 2009).

Google Scholar

[2] Y. Li: Aeroengine corporation paper corpus about blade faults of aeroengine. Guiyang: Li-Yang Aeroengine Company. 2007. pp.25-35.

Google Scholar

[3] Z. Ma, Y.H. Li., C. Wang: Key Eng . Mater. Vols. 373-374 (2008), pp.404-40.

Google Scholar

[4] Y. Sano, M. Obata, et al.: Mater . Sci. Eng. A Vol. 417(2006), pp.334-340.

Google Scholar

[5] Y.C. Bu, D.H. Lassila, M.S. Schneider, et al.: Mater. Sci. Eng. A, Vol. 409(2005), pp.270-281.

Google Scholar

[6] G.J. Cheng, M.A. Shehadeh: Int. J. Plasticity Vol. 22 (2006), pp.71-94.

Google Scholar

[7] Aeronautical Manufacture Engineering Handbook, edits committee: Aeronautical Manufacture Engineering Handbook (Aerospace industry press, China 1997).

Google Scholar

[8] Standardization Administration of China: Methods used on Aeroengine Blade and Matrial Vibration Test (Standardization Press of China, China 2001).

Google Scholar

[9] Standardization Administration of China: Statistical Analysis Methods used on Matrial Fatigue Test (Standardization Press of China, China 2001).

Google Scholar

[10] K.M. Ma, N.D. Long: Aerial. Mater. Appl. (Air Force Engineering Institute, China 1999).

Google Scholar