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Time- and Cycle-Dependent Crack Propagation in Haynes 282
Linköping University, Department of Management and Engineering, Engineering Materials. Linköping University, Faculty of Science & Engineering.
Linköping University, Department of Management and Engineering, Engineering Materials. Linköping University, Faculty of Science & Engineering.ORCID iD: 0000-0002-8304-0221
Chalmers University of Technology, Department of Applied Physics, Göteborg, Sweden; GKN Aerospace Engine Systems, R&T Centre, Trollhättan, Sweden.
2016 (English)In: Journal of Materials Science and Engineering: A, ISSN 2161-6213, Vol. 658, 463-471 p.Article in journal (Refereed) Published
Abstract [en]

Haynes 282 is a promising superalloy candidate for several high-temperature applications in both aero and land-based gas turbine engines. To study the crack growth behaviour under time-dependent conditions relevant to such applications, a test program was carried out at room temperature up to 700 °C with conditions ranging from pure cyclic to sustained tensile loading. At 650 °C and high stress intensity factors the crack growth was fully time-dependent for dwell-times of 90 s and longer. At lower stress intensities, the behaviour was mainly controlled by the cyclic loading, even under dwell conditions. The behaviour under dwell-fatigue conditions was well described by a liner superposition model.

Place, publisher, year, edition, pages
Elsevier, 2016. Vol. 658, 463-471 p.
Keyword [en]
Nickel based superalloys, fatigue, fracture, mechanical characterisation, electron microscopy
National Category
Other Materials Engineering
Identifiers
URN: urn:nbn:se:liu:diva-126922DOI: 10.1016/j.msea.2016.01.111ISI: 000372560800054OAI: oai:DiVA.org:liu-126922DiVA: diva2:917773
Note

At the time for thesis presentation publication was in status: Manuscript

Name of manuscript was: Time-dependent crack propagation in Haynes 282

Funding agencies: Agora Materiae, graduate school, Faculty grant SFO-MAT-LiU [2009-00971]; Swedish Energy Agency; Siemens Industrial Turbomachinery AB; GKN Aerospace Engine Systems; Royal Institute of Technology through the Swedish research program TURBO POWER

Available from: 2016-04-07 Created: 2016-04-07 Last updated: 2016-12-09Bibliographically approved
In thesis
1. Effect of Dwell-times on Crack Propagation in Superalloys
Open this publication in new window or tab >>Effect of Dwell-times on Crack Propagation in Superalloys
2015 (English)Licentiate thesis, comprehensive summary (Other academic)
Abstract [en]

Gas turbines are widely used in industry for power generation and as a power source at "hard to reach" locations where other possibilities for electrical supply are insufficient. There is a strong need for greener energy, considering the effect that pollution has had on global warming, and we need to come up with ways of producing cleaner electricity. A way to achieve this is by increasing the combustion temperature in gas turbines. This increases the demand on the high temperature performance of the materials used e.g. superalloys in the turbine. These high combustion temperatures can lead to detrimental degradation of critical components. These components are commonly subjected to cyclic loading of different types e.g. combined with dwell-times and overloads at elevated temperatures, which influence the crack growth. Dwell-times have shown to accelerate crack growth and change the cracking behaviour in both Inconel 718 and Haynes 282. Overloads at the beginning of the dwell-time cycle have shown to retard the dwell time effect on crack growth in Inconel 718. To understand these effects more microstructural investigations are needed.

The work presented in this licentiate thesis was conducted under the umbrella of the research program Turbo Power; "High temperature fatigue crack propagation in nickel-based superalloys", concentrating on fatigue crack growth mechanisms in superalloys during dwell-times, which have shown to have a devastating effect on the crack propagation behaviour. Mechanical testing was performed under operation-like conditions in order to achieve representative microstructures and material data for the subsequent microstructural work. The microstructures were microscopically investigated in a scanning electron microscope (SEM) using electron channeling contrast imaging (ECCI) as well as using light optical microscopy.

The outcome of this work has shown that there is a significant increase in crack growth rate when dwell-times are introduced at the maximum load (0% overload) in the fatigue cycle. With the introduction of a dwell-time there is also a shift from transgranular to intergranular crack growth for both Inconel 718 and Haynes 282. When an overload is applied prior to the dwell-time, the crack growth rate decreases with increasing overload levels in Inconel 718. At high temperature crack growth in Inconel 718 took place as intergranular crack growth along grain boundaries due to oxidation and the creation of nanometric voids. Another observed growth mechanism was crack advance along phase boundaries with subsequent severe oxidation of the phase.

This thesis comprises two parts. The first giving an introduction to the field of superalloys and the acting microstructural mechanisms that influence fatigue during dwell times. The second part consists of two appended papers, which report the work completed so far in the project.

Place, publisher, year, edition, pages
Linköping: Linköping University Electronic Press, 2015. 49 p.
Series
Linköping Studies in Science and Technology. Thesis, ISSN 0280-7971 ; 1739
National Category
Materials Engineering Energy Engineering Metallurgy and Metallic Materials
Identifiers
urn:nbn:se:liu:diva-123306 (URN)10.3384/lic.diva-123306 (DOI)978-91-7685-871-4 (ISBN)
Presentation
2016-01-22, ACAS, A-huset, Campus Valla, Linköping, 10:15 (Swedish)
Opponent
Supervisors
Funder
Swedish Energy Agency
Available from: 2015-12-10 Created: 2015-12-10 Last updated: 2016-12-09Bibliographically approved

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