Thermal Cyclic Creep and Long-Term Strength of the Material of Aircraft Gas Turbine Blades after Operation

被引：0
|
作者：
B. S. Karpinos
V. V. Samuleev
B. A. Lyashenko
E. V. Lais’ke
A. V. Rutkovs’kyi
机构：
[1] National Academy of Sciences of Ukraine,Pisarenko Institute of Problems of Strength
[2] Ukrainian Ministry of Education and Science,State Research Institute of Aviation under the Ministry of Defence
[3] State Research and Test Center of the Ukrainian Armed Forces,undefined
来源：
Strength of Materials | 2013年 / 45卷
关键词：
blade; stress; temperature; degree of damage; remaining life;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
The remaining thermal cyclic creep and long-term strength life of the material of aircraft gas turbine blades after operation has been determined experimentally. A considerable degradation of the material properties is noted.
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页码：542 / 548
页数：6
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