BEHAVIOR OF GAS-TURBINE BLADE MATERIALS UNDER LONG-TERM CREEP-FATIGUE LOADING

被引：1
作者：
KLOOS, KH
GRANACHER, J
HARTFIEL, R
机构：
来源：
MATERIALWISSENSCHAFT UND WERKSTOFFTECHNIK | 1993年 / 24卷 / 07期
关键词：
D O I：
10.1002/mawe.19930240708
中图分类号：
T [工业技术];
学科分类号：
08 ;
摘要：
The long-term creep fatigue behaviour of the gas turbine blade material IN-738 LC HIP is investigated by a service-type strain cycle up to a test duration of about 12 000 h. Further, it is reported about shorter tests of the same type on alloy IN-100 HIP The cyclic deformation of alloy IN-738 LC HIP in the long-term region is analysed and the creep fatigue crack initiation is described by the generalized damage accumulation rule using two different methods.
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收藏
页码：250 / 257
页数：8
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