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Laser powder bed fusion of Hastelloy X: effects of hot isostatic pressing and the hot cracking mechanism

Laser powder bed fusion of Hastelloy X: effects of hot isostatic pressing and the hot cracking mechanism
Laser powder bed fusion of Hastelloy X: effects of hot isostatic pressing and the hot cracking mechanism

Hastelloy X is the trademark for a nickel-based, high-temperature superalloy that is increasingly applied in gas turbine engines because of its exceptional combination of oxidation resistance and high-temperature strength. The superalloy suffers from hot cracking susceptibility, however, particularly when processed using additive manufacturing and laser powder bed fusion (LPBF). This paper systematically studies for the first time the effect of post-treatment hot isostatic processing (HIP) on the microstructure and mechanical properties of LPBF-fabricated Hastelloy X, with an emphasis on fatigue performance. The experimental results demonstrate that despite the very small number of remaining gas-filled micropores due to pressure counteraction, the high temperature and high pressure during the HIP process promote recrystallisation and closing of the internal microcracks and gas-free pores. The HIP-processed specimens are shown to be roughly 130 MPa and 60 MPa weaker than the non-processed specimens in yield strength and ultimate tensile strength, respectively. The HIP-processed Hastelloy X exhibits significant improvements in fatigue life, however: the effect of the HIP processing is apparent once the applied stress decreases. This improvement in fatigue performance is attributable to the reduction in stress concentration and residual stress release caused by the HIP process. The paper also studies the hot cracking mechanism and finds that intergranular microcracks generally occur along high angle grain boundaries; the interdendritic liquid pressure drop between dendrite tip and root is found to be a significant factor in the hot crack mechanism. The significance of this research is in developing a comprehensive understanding of HIP processing on the fatigue behaviour of the LPBF-fabricated Hastelloy X. The insights on the cracking mechanism, which presents a significant step towards using additive manufacturing to produce complex crack-free parts from this superalloy.

Fatigue performance, Hastelloy X, Hot cracking, Hot isostatic pressing, Laser powder bed fusion
0921-5093
228-239
Han, Quanquan
50c274a8-a7a1-458c-91d0-e21425824753
Mertens, Raya
3f09123a-947a-4c09-a537-5e408a4308d4
Montero-Sistiaga, Maria L.
3d7a58d1-51d6-4b87-a95e-fc84e3d04cfc
Yang, Shoufeng
e0018adf-8123-4a54-b8dd-306c10ca48f1
Setchi, Rossitza
39fd58ce-d4f5-42a2-959e-0ee4324c4424
Vanmeensel, Kim
275e05a1-05ad-4ab7-b654-f08f8d7dbc07
Van Hooreweder, Brecht
83aa9859-ab65-4eb5-9e4a-1186b3651f43
Evans, Sam L.
962f93bd-5378-4002-aeef-787a5dee2f4c
Fan, Haiyang
eeffcbfc-bee4-4d33-be8f-1c287bf44541
Han, Quanquan
50c274a8-a7a1-458c-91d0-e21425824753
Mertens, Raya
3f09123a-947a-4c09-a537-5e408a4308d4
Montero-Sistiaga, Maria L.
3d7a58d1-51d6-4b87-a95e-fc84e3d04cfc
Yang, Shoufeng
e0018adf-8123-4a54-b8dd-306c10ca48f1
Setchi, Rossitza
39fd58ce-d4f5-42a2-959e-0ee4324c4424
Vanmeensel, Kim
275e05a1-05ad-4ab7-b654-f08f8d7dbc07
Van Hooreweder, Brecht
83aa9859-ab65-4eb5-9e4a-1186b3651f43
Evans, Sam L.
962f93bd-5378-4002-aeef-787a5dee2f4c
Fan, Haiyang
eeffcbfc-bee4-4d33-be8f-1c287bf44541

Han, Quanquan, Mertens, Raya, Montero-Sistiaga, Maria L., Yang, Shoufeng, Setchi, Rossitza, Vanmeensel, Kim, Van Hooreweder, Brecht, Evans, Sam L. and Fan, Haiyang (2018) Laser powder bed fusion of Hastelloy X: effects of hot isostatic pressing and the hot cracking mechanism. Materials Science And Engineering A, 732, 228-239. (doi:10.1016/j.msea.2018.07.008).

Record type: Article

Abstract

Hastelloy X is the trademark for a nickel-based, high-temperature superalloy that is increasingly applied in gas turbine engines because of its exceptional combination of oxidation resistance and high-temperature strength. The superalloy suffers from hot cracking susceptibility, however, particularly when processed using additive manufacturing and laser powder bed fusion (LPBF). This paper systematically studies for the first time the effect of post-treatment hot isostatic processing (HIP) on the microstructure and mechanical properties of LPBF-fabricated Hastelloy X, with an emphasis on fatigue performance. The experimental results demonstrate that despite the very small number of remaining gas-filled micropores due to pressure counteraction, the high temperature and high pressure during the HIP process promote recrystallisation and closing of the internal microcracks and gas-free pores. The HIP-processed specimens are shown to be roughly 130 MPa and 60 MPa weaker than the non-processed specimens in yield strength and ultimate tensile strength, respectively. The HIP-processed Hastelloy X exhibits significant improvements in fatigue life, however: the effect of the HIP processing is apparent once the applied stress decreases. This improvement in fatigue performance is attributable to the reduction in stress concentration and residual stress release caused by the HIP process. The paper also studies the hot cracking mechanism and finds that intergranular microcracks generally occur along high angle grain boundaries; the interdendritic liquid pressure drop between dendrite tip and root is found to be a significant factor in the hot crack mechanism. The significance of this research is in developing a comprehensive understanding of HIP processing on the fatigue behaviour of the LPBF-fabricated Hastelloy X. The insights on the cracking mechanism, which presents a significant step towards using additive manufacturing to produce complex crack-free parts from this superalloy.

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More information

Accepted/In Press date: 3 July 2018
e-pub ahead of print date: 5 July 2018
Published date: 8 August 2018
Keywords: Fatigue performance, Hastelloy X, Hot cracking, Hot isostatic pressing, Laser powder bed fusion

Identifiers

Local EPrints ID: 435637
URI: http://eprints.soton.ac.uk/id/eprint/435637
ISSN: 0921-5093
PURE UUID: ddc1e7df-0d18-4b73-920e-06c5b644f5ec
ORCID for Shoufeng Yang: ORCID iD orcid.org/0000-0002-3888-3211

Catalogue record

Date deposited: 15 Nov 2019 17:30
Last modified: 05 Jun 2024 18:20

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Contributors

Author: Quanquan Han
Author: Raya Mertens
Author: Maria L. Montero-Sistiaga
Author: Shoufeng Yang ORCID iD
Author: Rossitza Setchi
Author: Kim Vanmeensel
Author: Brecht Van Hooreweder
Author: Sam L. Evans
Author: Haiyang Fan

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