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Creep Rupture Properties of Superalloys Developed for Nuclear Steelmaking
13
Citations
4
References
1984
Year
Materials ScienceHigh Temperature MaterialsCreep Rupture TestsEngineeringIntermediate Heat ExchangersSevere Plastic DeformationSuperalloyMechanical EngineeringAlloy DesignCreep Rupture PropertiesAlloy PhaseWork HardeningCreep Rupture StrengthsMechanics Of MaterialsMicrostructureStructural Materials
Creep rupture tests on six candidate alloys for intermediate heat exchangers of high-temperature gas-cooled reactors were carried out at 1173 to 1323 K in helium with small amounts of H2, CH4, CO, and C02, and at 1173K in H2 + 15% CO + 5% C02. The creep rupture strengths of each alloy were scarcely different at 1173 K in both environments. At higher temperatures in helium environments, the degradation of the creep rupture strengths appeared in carbide-strengthened alloys because of decarburization. The alloy, which mainly uses α-W as a strengthener, showed stable creep rupture strength up to 1323 K in spite of severe decarburization.
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