Microstructure and Tensile Properties of Oxide Dispersion Strengthened Molybdenum Alloys Prepared by Different Doping Process
p.481
p.481
Crack Growth in Stainless Steel 304 under Creep-Fatigue Loading
p.485
p.485
Effect of Microstructure on Thermo-Mechanical and Isothermal Low Cycle Fatigue Failures of a Single Crystal Ni-Base Superalloy
p.491
p.491
Residual Stress Characteristics of Plasma Sprayed CoNiCrAlY Coatings by X-Ray Diffraction
p.495
p.495
The Study on Failure Behavior and Low Cycle Fatigue Life of Hot Gas Casing for Gas Turbine
p.499
p.499
Microstructure and Strength of Oxidation-Bonded Porous Silicon Nitride Ceramics
p.503
p.503
Microstructure and High Temperature Stress Rupture Properties of Ru-Containing Directionally Solidified Ni-Base Superalloy
p.507
p.507
Microstructural Evolution during Tensile Creep of a Single-Crystal Nickel-Base Superalloy
p.511
p.511
Effect of Original Microstructure on the Hot Compression Behavior of Superalloy 718
p.515
p.515
The Study on Failure Behavior and Low Cycle Fatigue Life of Hot Gas Casing for Gas Turbine
Abstract:
In this study, failure behavior of hot gas casing for gas turbine was investigated. The microstructure and damage mechanism of serviced hot gas casing were examined. Also low cycle fatigue tests of the Inconel 617 super alloy is used for structural material of hot gas casing were performed. To predict the low cycle fatigue life, Coffin-Manson and strain energy density methods were used.
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Info:
Periodical:
Key Engineering Materials (Volumes 353-358)
Pages:
499-502
Citation:
Online since:
September 2007
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Сopyright:
© 2007 Trans Tech Publications Ltd. All Rights Reserved
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