Fatigue-creep life analysis for powder metallurgy material with inclusion
To predict the life of the life limit parts is an important work for the airworthiness compliance.The compliance work of life limit parts involves typical flight profile, heat transfer analysis, stress analysis, materials data, and life predict method.In this study, fatigue-creep interaction behaviors of powder metallurgy materials with inclusion have been performed with the Kachanov-Rabotnov damage law to show the life compliance.On the constant fatigue-creep loading, different types of inclusion are investigated in the work.The research shows that the type of inclusion has strong influence on the damage of matrix.Generally, the elliptical inclusion has much more damage than the round inclusion.Furthermore, the fatigue-creep life of powder metallurgy materials is calculated by the damage model, which can be considered for the design of the engine life limit parts.
Engine life limit part Compliance Fatigue-creep interaction
HOU Naixian YANG Kun
AVIC Commercial aircraft engine CO.,LTD ，Shanghai 200241,PR China
国际会议
北京
英文
292-296
2011-10-01（万方平台首次上网日期，不代表论文的发表时间）