The extreme conditions of aircraft bearing steel M50 have been simulated by a two-disk test rig for investigating the surface damage of the ball/raceway contact surfaces. The slide/roll ratio are 0.12 and 0.15, correspondingly, the rolling speed are 43.2m/s and 49.5m/s. Aircraft engine oil 4050 as the supplied oil has been maintained at approximately 80°C in the tests. The ultimate Hertzian contact stresses of the surface damage obtained from the experiments are 3.8GPa in 0.12 slide/roll ratio and 3.5GPa in 0.15 slide/roll ratio. The damage mode is scuffing in 0.12 slide/roll ratio and it is oxidation, thermal fatigue and scuffing in 0.15 slide/roll ratio. Cracks in the contact areas originate from surface layer in the two slide/roll ratios.
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STLE/ASME 2010 International Joint Tribology Conference
October 17–20, 2010
San Francisco, California, USA
Conference Sponsors:
- Tribology Division
ISBN:
978-0-7918-4419-9
PROCEEDINGS PAPER
Surface Damage Under Extreme Conditions Existed in Aircraft Bearings
Bo Peng,
Bo Peng
Harbin Institute of Technology, Harbin, China
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Liqin Wang,
Liqin Wang
Harbin Institute of Technology, Harbin, China
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Le Gu,
Le Gu
Harbin Institute of Technology, Harbin, China
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Dezhi Zheng
Dezhi Zheng
Harbin Institute of Technology, Harbin, China
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Bo Peng
Harbin Institute of Technology, Harbin, China
Liqin Wang
Harbin Institute of Technology, Harbin, China
Le Gu
Harbin Institute of Technology, Harbin, China
Dezhi Zheng
Harbin Institute of Technology, Harbin, China
Paper No:
IJTC2010-41127, pp. 215-217; 3 pages
Published Online:
April 14, 2011
Citation
Peng, B, Wang, L, Gu, L, & Zheng, D. "Surface Damage Under Extreme Conditions Existed in Aircraft Bearings." Proceedings of the STLE/ASME 2010 International Joint Tribology Conference. STLE/ASME 2010 International Joint Tribology Conference. San Francisco, California, USA. October 17–20, 2010. pp. 215-217. ASME. https://doi.org/10.1115/IJTC2010-41127
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