Abstract

The role of local microstructure is critical in materials performance and integrity in a cast alloy. The grain size and grain boundary distributions as well as local texture can create various microstructure/microtexture clusters that cause deformation localisation in the alloy. Inconel 713C nickel base superalloys are used as turbocharger turbine wheels for modern diesel engines, produced via investment casting. In such an alloy localised deformation is highly expected during service, as the strain distribution is not uniform in the component due to casting geometrical factors in addition to non-homogenous microstructure and microtexture in the cast alloy. In the current investigation Small Punch (SP) tensile tests were carried out on IN713C at room temperature and 650°C in an air environment under stroke control at a rate of 0.02mm/s. The fracture surface examination and microstructure characterisation as well as detailed texture analyses were performed using Scanning Electron Microscopy (SEM) and Electron Backscatter Diffraction (EBSD). Finite Element (FE) analysis of the SP test was also implemented to investigate the role of stress state on the local deformation. It was evident that microstructure parameters such as grain morphology and original texture existed in the disc were the most influential factors in governing the deformation texture in mixed columnar/equiaxed (transition) disc microstructure. Whereas, the temperature was the determining parameter in grain rotations and texture changes for wholly columnar disc microstructures.

Highlights

  • Add to the variation in life cycles observed in stress versus life (S– N) data of the cast components [8,9,10]

  • Small Punch (SP) test has been successfully applied to the study of deformation behaviour of investment casted IN713C turbine blades sectioned from a diesel turbocharger component

  • SP discs of columnar grained and mixed equiaxed/columnar microstructures were tested at Room Temperature (RT) and High Temperature (HT), 650 °C

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Summary

Introduction

Add to the variation in life cycles observed in stress versus life (S– N) data of the cast components [8,9,10]. Despite the dynamic nature of SP testing, yield strength, ultimate tensile strength and tensile elongation can be predicted using the European Code of Practice 2007 [20], which details the most suitable test approaches as well as formula for the calculation of mechanical properties from the SP load/displacement data [21]. This investigation utilises small punch disc testing as a technique for evaluating the mechanical properties of different areas in turbo charger turbine wheel components. The deformation mechanisms and possible causes of crack initiation and propagation are investigated

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