Abstract
Creep-fatigue (CF) interaction at elevated temperature is the most damaging structural failure mode for materials under cyclic loads. In the last 40 years, significant efforts have been devoted to elevated temperature code rule development in the American Society of Mechanical Engineers (ASME) Boiler and Pressure Vessel Code (Section III, Division 5, Subsection HB, Subpart B) to ascertain conservative structural designs against CF failure. However, the current CF evaluation procedure is complex and overly conservative. Recently, an alternative CF evaluation method, Simplified Model Test (SMT) based design methodology, is being developed with the purpose of simplifying and improving the CF evaluation process. The concept of this approach is to perform CF evaluation using a set of design curves developed directly from experimental CF data and avoid the separate evaluation of creep and fatigue damage. Experimental CF failure data are the key in finalizing the SMT-based design curves. In assessing available data sources, major data gap was found at low strain ranges of below 0.3% and/or at hold times of longer than one hour. The lack of data under these conditions is due to many practical constraints such as the unrealistically long test duration and difficulties in controlling experimental parameters. In this study, an experimental method is proposed based on the concept of damage summation to generate CF failure life information at low strain ranges and long hold times. The CF test was designed for Alloy 617 at 950°C with elastic follow-up effect to slow down the stress relaxation process during the hold time. The test specimen was cycled at higher strain ranges to accumulate enough CF damage, followed by cycling at lower strain ranges and longer hold times, to allow for a reasonable test time to generate failure data. Results from the CF test are presented, and information generated through this method in verifying the SMT-based design curves is evaluated.
Original language | English |
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Title of host publication | Codes and Standards |
Publisher | American Society of Mechanical Engineers (ASME) |
ISBN (Electronic) | 9780791887448 |
DOIs | |
State | Published - 2023 |
Event | ASME 2023 Pressure Vessels and Piping Conference, PVP 2023 - Atlanta, United States Duration: Jul 16 2023 → Jul 21 2023 |
Publication series
Name | American Society of Mechanical Engineers, Pressure Vessels and Piping Division (Publication) PVP |
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Volume | 1 |
ISSN (Print) | 0277-027X |
Conference
Conference | ASME 2023 Pressure Vessels and Piping Conference, PVP 2023 |
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Country/Territory | United States |
City | Atlanta |
Period | 07/16/23 → 07/21/23 |
Funding
The research was sponsored by the U.S. Department of Energy, Office of Nuclear Energy, under contract No. DEAC05- 00OR22725 with Oak Ridge National Laboratory (ORNL), managed and operated by UT-Battelle, LLC, and under contract No. DE-AC07-05ID14517 with Idaho National Laboratory (INL), managed and operated by Battelle Energy Alliance, LLC. Programmatic direction was provided by the Office of Nuclear Reactor Deployment of the Office of Nuclear Energy. The contribution of Charles S. Hawkins and Brad Hall of ORNL in running the experiments is greatly appreciated. The research was sponsored by the U.S. Department of Energy, Office of Nuclear Energy, under contract No. DE-AC05-00OR22725 with Oak Ridge National Laboratory (ORNL), managed and operated by UT-Battelle, LLC, and under contract No. DE-AC07-05ID14517 with Idaho National Laboratory (INL), managed and operated by Battelle Energy Alliance, LLC. Programmatic direction was provided by the Office of Nuclear Reactor Deployment of the Office of Nuclear Energy. The contribution of Charles S. Hawkins and Brad Hall of ORNL in running the experiments is greatly appreciated. This manuscript has been co-authored by Battelle Energy Alliance, LLC, under Contract No. DE-AC07-05ID14517 and by UT-Battelle LLC, under Contract No. DE-AC0500OR22725, with the U.S. Department of Energy. The United States Government retains and the publisher, by accepting the article for publication, acknowledges that the United States Government retains a nonexclusive, paid-up, irrevocable, world-wide license to publish or reproduce the published form of this manuscript, or allow others to do so, for United States Government purposes.
Keywords
- Alloy 617
- Creep-fatigue
- Elastic follow-up
- High temperature
- Life prediction
- hold time
- low strain range