Abstract

Ti-6242 is a near alpha titanium alloy, which has excellent high-temperature creep resistance and is widely used in jet engine compressors. This alloy is susceptible to creep fatigue failure under dwell loading below 473 K. The existence of microtextured regions (MTRs) contributes significantly to this fast crack propagation. Mechanical processing in the alpha + beta region has been employed to eliminate MTRs, but the efficiency depends significantly on the applied strain path. Previous investigations based on crystal plasticity finite element (CPFE) simulations have demonstrated the relationship between breakdown efficiency and loading direction. Therein, MTRs with regular geometry and pure initial orientation were used to isolate the effect of loading direction from initial microstructure. In this paper, the behavior of MTRs with realistic initial microstructure was investigated using a hierarchical multiscale modeling framework, and the microscale results were analyzed in detail to understand the behavior of MTRs under different loading conditions. It was shown that a hierarchical multiscale model with realistic initial microstructure at the microscale can reflect the influences from different strain paths, initial orientation distributions, and positions of the region simultaneously. The combined effect of initial orientation distribution and loading direction on the MTR breakdown efficiency is discussed in detail.

Highlights

  • Near alpha titanium alloy Ti-6242 (Ti–6Al–2Sn–4Zr–2Mo) is widely used as a primary structural material in high-pressure compressors of aircraft gas-turbine engines due to its high specific strength and excellent high-temperature creep resistance [1]

  • This paper extends the previous work by considering the distributed nature of α p particles within microtextured regions (MTRs) to more precisely capture the morphology evolution of MTRs under different strain paths

  • The MTR breakdown efficiency varies within each region and is affected by the initial microstructure, both of which can be captured by the hierarchical multiscale modeling simultaneously

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Summary

Introduction

Near alpha titanium alloy Ti-6242 (Ti–6Al–2Sn–4Zr–2Mo) is widely used as a primary structural material in high-pressure compressors of aircraft gas-turbine engines due to its high specific strength and excellent high-temperature creep resistance [1]. In another study [12], the evolution of MTRs under different processing conditions was investigated using the crystal plasticity finite element method, and an optimal strain path was determined to effectively eliminate MTRs. Idealized MTRs consisting of two ellipsoid α phase regions embedded in a uniformly textured matrix were employed, and all α p particles were assumed to have identical initial orientation. The initial orientation distribution and particle size distribution of α p particles were extracted from the billet material [13] These distributions were further employed to generate a statistically equivalent representative volume element (RVE) for the microscale problem of a hierarchical multiscale modeling framework.

Crystal Plasticity Model and Simulation Setup
Titanium Crystal Plasticity Model Calibration
Statistically Equivalent Microstructure
Hierarchical Multiscale Modeling Framework
High-Temperature Compression Experiment
Results and Discussion
Comparison between Idealized MTR and Statistically Equivalent MTR
Disorientation Evolution of Statistically Equivalent MTR
Conclusions
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