Effects of austempering temperature on fatigue crack rate propagation in a series of modified (Cu, Ni, and/or Mo) nodular irons
- 1. Universidad Nacional Autónoma de México. Instituto de Física (Mexico)
- 2. San Fandila, Pedro Escobedo. Instituto Mexicano del Transporte (Mexico)
Description
Studies on austempered nodular cast irons were carried out to establish the optimum isothermic heat treatment at a given chemical composition that rendered the highest fatigue crack propagation resistance. Seven nodular iron chemical compositions with different concentrations of copper, nickel, and or molybdenum were tested at three austempering temperatures achieving ausferritic microstructures. Three-point bend tests for crack growth rates were performed at room temperature in a close loop servo hydraulic machine. Crack opening displacement measurements were performed using a controlled displacement telescope. A simple linear statistical analysis indicated that the lower the austempering isothermal temperature, the higher the fatigue strength of the alloys. Cu and Mo additions along with a good spheroidicity of graphite nodules in the iron favored this effect.
Additional details
Identifiers
Publishing Information
- Journal Title
- Journal of Materials Engineering and Performance
- Journal Volume
- 11
- Journal Issue
- 6
- Journal Page Range
- p. 651-658
- ISSN
- 1059-9495
- CODEN
- JMEPEG
INIS
- Country of Publication
- United States
- Country of Input or Organization
- International Atomic Energy Agency (IAEA)
- INIS RN
- 55080461
- Subject category
- S36: MATERIALS SCIENCE;
- Descriptors DEI
- BENDING; CAST IRON; CHEMICAL COMPOSITION; COPPER; COPPER ALLOYS; CRACK PROPAGATION; CRACKS; FATIGUE; GRAPHITE; HEAT TREATMENTS; IRON; MICROSTRUCTURE; MOLYBDENUM; MOLYBDENUM ALLOYS; NICKEL BASE ALLOYS; TEMPERATURE DEPENDENCE
- Descriptors DEC
- ALLOYS; CARBON; CARBON ADDITIONS; DEFORMATION; ELEMENTS; IRON ALLOYS; IRON BASE ALLOYS; MECHANICAL PROPERTIES; METALS; MINERALS; NICKEL ALLOYS; NONMETALS; REFRACTORY METALS; SILICON ALLOYS; TRANSITION ELEMENT ALLOYS; TRANSITION ELEMENTS
Optional Information
- Copyright
- Copyright (c) 2002 © ASM International 2002