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Alloy Design and Characterization of γ′ Strengthened Nickel-based Superalloys for Additive Manufacturing
Linköping University, Department of Management and Engineering, Engineering Materials. Linköping University, Faculty of Science & Engineering.
2021 (English)Licentiate thesis, comprehensive summary (Other academic)
Abstract [en]

Nickel-based superalloys, an alloy system bases on nickel as the matrix element with the addition of up to 10 more alloying elements including chromium, aluminum, cobalt, tungsten, molybdenum, titanium, and so on. Through the development and improvement of nickel-based superalloys in the past century, they are well proved to show excellent performance at the elevated service temperature. Owing to the combination of extraordinary high-temperature mechanical properties, such as monotonic and cyclic deformation resistance, fatigue crack propagation resistance; and high-temperature chemical properties, such as corrosion and oxidation resistance, phase stability, nickel-based superalloys are widely used in the critical hot-section components in aerospace and energy generation industries.

The success of nickel-based superalloy systems attributes to both the well-tailored microstructures with the assistance of carefully doped alloying elements, and the intently developed manufacturing processes. The microstructure of the modern nickel-based superalloys consists of a two-phase configuration: the intermetallic precipitates (Ni,Co)3(Al,Ti,Ta) known as γ′ phase dispersed into the austenite γ matrix, which is firstly introduced in the 1940s.  The recently developed additive manufacturing (AM) techniques, acting as the disruptive manufacturing process, offers a new avenue for producing the nickel-based superalloy components with complicated geometries. However, γ′ strengthened nickel-based superalloys always suffer from the micro-cracking during the AM process, which is barely eliminated by the process optimization.

On this basis, the new compositions of γ′ strengthened nickel-based superalloy adapted to the AM process are of great interest and significance. This study sought to design novel γ′ strengthened nickel-based superalloys readily for AM process with limited cracking susceptibility, based on the understanding of the cracking mechanisms. A two-parameter model is developed to predict the additive manufacturability for any given composition of a nickel-based superalloy. One materials index is derived from the comparison of the deformation-resistant capacity between dendritic and interdendritic regions, while another index is derived from the difference of heat resistant capacity of these two spaces. By plotting the additive manufacturability diagram, the superalloys family can be categorized into the easy-to-weld, fairly-weldable, and non-weldable regime with the good agreement of the existed knowledge. To design a novel superalloy, a Cr-Co-Mo-W-Al-Ti-Ta-Nb-Fe-Ni alloy family is proposed containing 921,600 composition recipes in total. Through the examination of additive manufacturability, undesired phase formation propensity, and the precipitation fraction, one composition of superalloy, MAD542, out of the 921,600 candidates is selected.

Validation of additive manufacturability of MAD542 is carried out by laser powder bed fusion (LPBF). By optimizing the LPBF process parameters, the crack-free MAD542 part is achieved. In addition, the MAD542 superalloy shows great resistance to the post-processing treatment-induced cracking. During the post-processing treatment, extensive annealing twins are promoted to achieve the recrystallization microstructure, ensuring the rapid reduction of stored energy. After ageing treatment, up to 60-65% volume fraction of γ′ precipitates are developed, indicating the huge potential of γ′ formation. Examined by the high-temperature slow strain rate tensile and constant loading creep testing, the MAD542 superalloy shows superior strength than the LPBF processed and hot isostatic pressed plus heat-treated IN738LC superalloy. While the low ductility of MAD542 is existed, which is expected to be improved by modifying the post-processing treatment scenarios and by the adjusting building direction in the following stages of the Ph.D. research.

MAD542 superalloy so far shows both good additive manufacturability and mechanical potentials. Additionally, the results in this study will contribute to a novel paradigm for alloy design and encourage more γ′-strengthened nickel-based superalloys tailored for AM processes in the future.

Place, publisher, year, edition, pages
Linköping: Linköping University Electronic Press, 2021. , p. 63
Series
Linköping Studies in Science and Technology. Licentiate Thesis, ISSN 0280-7971 ; 1896
Keywords [en]
Nickel-based superalloy, Alloy design, Laser powder bed fusion, Cracking susceptibility, Additive manufacturability, Heat treatment, γ′ precipitate, High-temperature mechanical property, Creep.
National Category
Metallurgy and Metallic Materials
Identifiers
URN: urn:nbn:se:liu:diva-173042DOI: 10.3384/lic.diva-173042ISBN: 9789179297268 (print)OAI: oai:DiVA.org:liu-173042DiVA, id: diva2:1523272
Presentation
2021-02-12, ACAS, A-Building, Campus Valla, Linköping, 10:15 (English)
Opponent
Supervisors
Funder
Vinnova, 2018-00804
Note

Additional funding agencies: Agora Materiae Graduate School for multidisiplinary PhD students at Linköping University, and Stiftelsen Axel Hultgren.

Available from: 2021-01-28 Created: 2021-01-28 Last updated: 2021-02-01Bibliographically approved
List of papers
1. Short-term Creep Behavior of an Additive Manufactured Non-weldable Nickel-base Superalloy Evaluated by Slow Strain Rate Testing
Open this publication in new window or tab >>Short-term Creep Behavior of an Additive Manufactured Non-weldable Nickel-base Superalloy Evaluated by Slow Strain Rate Testing
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2019 (English)In: Acta Materialia, ISSN 1359-6454, E-ISSN 1873-2453, Vol. 179, p. 142-157Article in journal (Refereed) Published
Abstract [en]

Additive manufacturing (AM) of high γ′ strengthened Nickel-base superalloys, such as IN738LC, is of high interest for applications in hot section components for gas turbines. The creep property acts as the critical indicator of component performance under load at elevated temperature. However, it has been widely suggested that the suitable service condition of AM processed IN738LC is not yet fully clear. In order to evaluate the short-term creep behavior, slow strain rate tensile (SSRT) tests were performed. IN738LC bars were built by laser powder-bed-fusion (L-PBF) and then subjected to hot isostatic pressing (HIP) followed by the standard two-step heat treatment. The samples were subjected to SSRT testing at 850 °C under strain rates of 1 × 10−5/s, 1 × 10−6/s, and 1 × 10−7/s. In this research, the underlying creep deformation mechanism of AM processed IN738LC is investigated using the serial sectioning technique, electron backscatter diffraction (EBSD), transmission electron microscopy (TEM). On the creep mechanism of AM polycrystalline IN738LC, grain boundary sliding is predominant. However, due to the interlock feature of grain boundaries in AM processed IN738LC, the grain structure retains its integrity after deformation. The dislocation motion acts as the major accommodation process of grain boundary sliding. Dislocations bypass the γ′ precipitates by Orowan looping and wavy slip. The rearrangement of screw dislocations is responsible for the formation of subgrains within the grain interior. This research elucidates the short-creep behavior of AM processed IN738LC. It also shed new light on the creep deformation mechanism of additive manufactured γ′ strengthened polycrystalline Nickel-base superalloys.

Place, publisher, year, edition, pages
Elsevier, 2019
Keywords
Nickel-base superalloy, laser processing, creep, grain boundary sliding, dislocations
National Category
Materials Engineering
Identifiers
urn:nbn:se:liu:diva-161742 (URN)10.1016/j.actamat.2019.08.034 (DOI)000488417400013 ()2-s2.0-85071224254 (Scopus ID)
Note

Funding Agencies|Swedish Governmental Agency for Innovation Systems, (Vinnova)Vinnova [2016-05175, 2018-00804]; Linkoping University [2009-00971]

Available from: 2019-11-08 Created: 2019-11-08 Last updated: 2022-04-05Bibliographically approved
2. On the Strengthening and Embrittlement Mechanisms of an Additively Manufactured Nickel-base Superalloy
Open this publication in new window or tab >>On the Strengthening and Embrittlement Mechanisms of an Additively Manufactured Nickel-base Superalloy
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2020 (English)In: Materialia, E-ISSN 2589-1529, Vol. 10, article id 100657Article in journal (Refereed) Published
Abstract [en]

The γ′ phase strengthened Nickel-base superalloy is one of the most significant dual-phase alloy systems for high-temperature engineering applications. The tensile properties of laser powder-bed-fused IN738LC superalloy in the as-built state have been shown to have both good strength and ductility compared with its post-thermal treated state. A microstructural hierarchy composed of weak texture, sub-micron cellular structures and dislocation cellular walls was promoted in the as-built sample. After post-thermal treatment, the secondary phase γ′ precipitated with various size and fraction depending on heat treatment process. For room-temperature tensile tests, the dominated deformation mechanism is planar slip of dislocations in the as-built sample while dislocations bypassing the precipitates via Orowan looping in the γ′ strengthened samples. The extraordinary strengthening effect due to the dislocation substructure in the as-built sample provides an addition of 372 MPa in yield strength. The results of our calculation are in agreement with experimental yield strength for all the three different conditions investigated. Strikingly, the γ′ strengthened samples have higher work hardening rate than as-built sample but encounter premature failure. Experimental evidence shows that the embrittlement mechanism in the γ′ strengthened samples is caused by the high dislocation hardening of the grain interior region, which reduces the ability to accommodate further plastic strain and leads to premature intergranular cracking. On the basis of these results, the strengthening micromechanism and double-edge effect of strength and ductility of Nickel-base superalloy is discussed in detail.

Place, publisher, year, edition, pages
Elsevier, 2020
Keywords
Laser powder-bed-fusion, Nickel-base superalloy, Mechanical property, Cellular structure
National Category
Materials Engineering
Identifiers
urn:nbn:se:liu:diva-166000 (URN)10.1016/j.mtla.2020.100657 (DOI)000537622100022 ()2-s2.0-85082447645 (Scopus ID)
Available from: 2020-06-04 Created: 2020-06-04 Last updated: 2025-08-21Bibliographically approved
3. A Novel Y’ -Strengthened Nickel-Based Superalloy for Laser Powder Bed Fusion
Open this publication in new window or tab >>A Novel Y’ -Strengthened Nickel-Based Superalloy for Laser Powder Bed Fusion
2020 (English)In: Materials, E-ISSN 1996-1944, Vol. 13, no 21, article id 4930Article in journal (Refereed) Published
Abstract [en]

An experimental printable gamma -strengthened nickel-based superalloy, MAD542, is proposed. By process optimization, a crack-free component with less than 0.06% defect was achieved by laser powder bed fusion (LPBF). After post-processing by solution heat treatment, a recrystallized structure was revealed, which was also associated with the formation of annealing twins. After the aging treatment, 60-65% gamma precipitates were obtained with a cuboidal morphology. The success of printing and post-processing the new MAD542 superalloy may give new insights into alloy design approaches for additive manufacturing.

Place, publisher, year, edition, pages
MDPI, 2020
Keywords
nickel-based superalloy; γ ′ phase; laser powder bed fusion; alloy development
National Category
Manufacturing, Surface and Joining Technology
Identifiers
urn:nbn:se:liu:diva-171809 (URN)10.3390/ma13214930 (DOI)000589437500001 ()33147831 (PubMedID)
Note

Funding Agencies|Swedish Agency for Innovation Systems, (Vinnova grant) [2016-05175, 2018-00804]; Linkoping University (SFO-MAT-LiU) [2009-00971]; center for Additive Manufacture-Metal (CAM2)

Available from: 2020-12-07 Created: 2020-12-07 Last updated: 2024-07-04

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Xu, Jinghao

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