Low Cycle Fatigue and Crack Grow in Powder Nickel Alloy under Turbine Disk Wave Form Loading: Validation of Damage Accumulation Model

Author:

Nikhamkin M.1,Ilinykh A.1

Affiliation:

1. Perm National Research Polytechnic University

Abstract

Experimental verification of the damage accumulation model of low cycle fatigue crack initiation and growth is executed. Loading wave form typical for discs of gas turbine engines is studied. Linear damage accumulation model is found to give acceptable accuracy for crack initiation and growth in powder nickel alloys. This model is acceptable for disc cyclic durability prediction.

Publisher

Trans Tech Publications, Ltd.

Reference7 articles.

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Cited by 3 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Mechanical behavior regularities of an aluminum alloy under biaxial low-cycle loading under conditions of the axial component action of a constant value;PROCEEDINGS OF INTERNATIONAL CONFERENCE OF YOUNG SCIENTISTS AND STUDENTS “TOPICAL PROBLEMS OF MECHANICAL ENGINEERING” ToPME 2021: Mechanical Engineering Research Institute of the Russian Academy of Sciences (IMASH RAN);2023

2. Studying of accumulation damages regularities under low cycle loading and cycle variable parameters conditions;IOP Conference Series: Materials Science and Engineering;2020-01-01

3. Low Cycle Fatigue and Crack Grow in Powder Nickel Alloy under Turbine Disk Wave Form Loading: Validation of Damage Accumulation Model;Applied Mechanics and Materials;2013-12

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