J. KIMS Technol Search

CLOSE


J. KIMS Technol > Volume 14(1); 2011 > Article
Journal of the Korea Institute of Military Science and Technology 2011;14(1):92-99.
DOI: https://doi.org/10.9766/KIMST.2011.14.1.092   
Development of Fretting Fatigue Parameter
Hyuk-Jae Lee
Materials Research Center for Energy and Green Technology, Andong National University
접촉피로 파라미터의 개발
이혁재
안동대학교 청정에너지소재기술연구센터
Abstract
In this study, new multi-axial, critical plane based, fretting fatigue crack initiation parameter is developed by the addition of a new term into the Modified Shear Stress Range(MSSR) parameter. The newly developed parameter (MSSR') is then used to evaluate fretting fatigue life of titanium alloy, Ti-6A1-4V with various contact conditions. Finite element analysis is also used in order to obtain stress distribution on the contact surface during fretting fatigue test, which is then used for the calculation of fretting fatigue parameter. The MSSR' parameter shows better performance in predicting fretting fatigue lives from the conventional fatigue data, and less scattering within fretting fatigue data with different contact geometries.
Key Words: Fretting Fatigue, Multi-axial Parameter, Critical Plane, Titanium Alloy, Finite Element Analysis


ABOUT
ARTICLE CATEGORY

Browse all articles >

BROWSE ARTICLES
FOR CONTRIBUTORS
Editorial Office
160 Bugyuseong-daero 488beon-gil, Yuseong-gu, Daejeon 34060, Korea
Tel: +82-42-823-4603    Fax: +82-42-823-4605    E-mail: kimst@kimst.or.kr                

Copyright © 2024 by The Korea Institute of Military Science and Technology.

Developed in M2PI

Close layer
prev next