Prediction of Thermal Fatigue Life of Engine Exhaust Manifold under Thermo-mechanical Cyclic Loading

Choi, Bok Lok; Chang, Hong Suk

doi:10.3795/ksme-a.2010.34.7.911

Cited by 3 publications

(1 citation statement)

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“…Moreover, precise experimental techniques are required to obtain the hysteresis loop. [2] Therefore, thermo-mechanical fatigue tests were performed for IN738LC, which is widely applied in actual gas turbine blades. The hysteresis loop of the material was derived using finite element analysis.…”

Section: Introductionmentioning

confidence: 99%

Evaluation on Thermo-Mechanical Fatigue Life of IN738LC Using Finite Element Analysis

Lee

Koo

et al. 2013

AMM

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In this paper, thermo-mechanical fatigue tests were performed for the nickel-based super alloy IN738LC, after which the thermo-mechanical fatigue life was evaluated using finite element analysis. Nickel-based super alloy is used as the main material of turbine blades, which are important equipment in thermal power generation plants. In general, such materials receive three types of damage under thermo-mechanical fatigue loading. In the case of low-cycle fatigue behavior in which large plastic deformation mainly occurs, the lifetime can be decided by its relationship with the plastic strain amplitude. In order to obtain the plastic strain amplitude from the measured strain amplitude, a hysteresis loop should be derived. However, low-cycle fatigue tests are difficult. Moreover, precise experimental techniques are required to obtain the hysteresis loops. In this study, after thermo-mechanical fatigue tests were performed, thermal mechanical fatigue tests on IN738LC were simulated using finite element analysis. The results of analysis were verified by comparing with the hysteresis loops of an experiment

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Section: Introductionmentioning

confidence: 99%