| Issue |
MATEC Web Conf.
Volume 321, 2020
The 14th World Conference on Titanium (Ti 2019)
|
|
|---|---|---|
| Article Number | 11093 | |
| Number of page(s) | 9 | |
| Section | Microstructure - Properties Relationships | |
| DOI | https://doi.org/10.1051/matecconf/202032111093 | |
| Published online | 12 October 2020 | |
Advanced Titanium Alloy Fatigue Modeling
1 Rolls-Royce Corporation, Indianapolis, IN
2 General Electric Aviation, Cincinnati, OH
3 Pratt & Whitney, Hartford, CT
4 Honeywell Aerospace, Phoenix, A Z
5 The Boeing Company, St Louis, MO
6 PCC - Wyman-Gordon, Houston, TX
7 ATI Forged Products, Cudahy, WI
8 Titanium Metals Corporation (TIMET), Hend erson, NV
9 Arconic, Niles, OH
10 Scientific Forming Technologies, Columbus, OH
11 Materials Resources LLC, Dayton, OH
12 Johns Hopkins University, Baltimore, MD
14 Air Force Research Laboratory, Materials and Manufactur ing Directorate, AFRL, Wright-Patterson AFB, OH
A summar y of the final progress achieved in two Metals Affordability Initiative (MAI) programs (RR-12 and RR-13) that were funded by the US Air Force to develop the necessary integrated computational materials engineering (ICME) framework, knowledge, and supporting database to model and predict location-specific fatigue properties across the entire titanium supply chain is presented. Validation of this ICME framework which allows for the prediction of location specific low cycle fatigue (LCF) and high cycle fatigue (HCF) behavior on complex production components in electro-polished and shot peened surface conditions will be presented. In addition, validation of a new shot peening capability embedded with the commercial software package DEFORM™ will be presented.
© The Authors, published by EDP Sciences, 2020
This is an Open Access article distributed under the terms of the Creative Commons Attribution License 4.0, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
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