Additive manufacturing of Ni-base superalloys: Processing, heat treatment, productivity, and properties
Doktorsavhandling, 2025

Nickel-base superalloys are essential materials for the energy and aerospace industries. The additive manufacturing (AM) of these materials using powder bed fusion – laser beam (PBF-LB) offers a valuable opportunity to improve component performance and simplify manufacturing and supply chain complexities in these industries. However, several challenges are encountered during PBF-LB processing of superalloys, including microcracking, deficient mechanical performance, and low productivity. The aim of the research in this thesis is to develop a better understanding of the extent of these issues in different superalloys, uncover their causes, and propose potential remedies.

The challenge of microcracking susceptibility was investigated for a γ´ strengthened superalloy IN738LC, where the alloying of minor grain boundary strengthening elements B and Zr was systematically varied. PBF-LB processing tests indicated that alloying with B and Zr together promoted severe microcracking, while omitting either or both elements from the composition reduced the susceptibility to microcracking. Importantly, the creep resistance of the alloy was maximized only with alloying of both B and Zr. This presented a conundrum where microcracking could only be prevented at the expense of the most desirable properties of the alloy. Based on the fine grain size and poor creep resistance in PBF-LB processed IN738LC, an alternative approach was proposed in the form of a modified IN738LC with heavily increased B alloying. Processability tests showed that microcracking was mitigated in the modified alloy, and CALPHAD solidification simulations suggested this was potentially due to a liquid backfilling effect in the last stages of solidification. The modified alloy also showed enhanced creep resistance relative to the standard composition, thus showcasing a novel method of overcoming microcracking susceptibility while simultaneously improving high temperature capability.

Investigations into heat treatment optimization were made for the alloy Haynes® 282®, since the application of the standard wrought heat treatment to the PBF-LB material was shown to produce severe anisotropy in tensile ductility and deficient creep rupture life. The use of solution heat treatments at 1250°C could radically alter the microstructure by coarsening grains, increasing twin boundary fractions, and forming a characteristic carbide structure at grain boundaries. The anisotropy in tensile properties was resultantly reduced, and creep rupture life of the alloy could be enhanced even above the level of its wrought counterpart.

The design of heat treatment for PBF-LB superalloys necessitates a detailed understanding of the as-built microstructure, which is often different from the cast or wrought counterpart of the same alloy. This aspect was investigated in the case of IN939, a high γ´-fraction superalloy. No γ´ precipitates were observed in the as-built microstructure, however the η phase was found at inter-dendritic regions. This secondary phase was observed to grow when aged without solution treatment, lowering the alloy’s ductility. The study demonstrates the importance of a solution treatment for IN939, regardless of γ´ precipitates in the as-built condition.

Investigations into high productivity PBF-LB processing of IN625 and Haynes® 282® were performed to understand the effect of high layer thickness parameters on porosity and mechanical performance. X-ray Computed Tomography analysis revealed that high density parts with porosity volume fractions < 0.05% could be produced with high productivity processing. However, the large size and sharp morphology of the porosity resulted in degraded mechanical properties compared to conventional processing. Despite this, high productivity PBF-LB processing presents an attractive route towards efficient manufacturing, especially if the trade-off in properties can be accepted.

impact toughness

productivity

porosity

powder bed fusion – laser beam

fatigue

layer thickness

zirconium

creep

Inconel 939

Inconel 625

cracking

microstructure

Additive manufacturing

Haynes 282.

boron

superalloys

heat treatment

Inconel 738

VDL, M-huset, Campus Johanneberg
Opponent: Professor K. A. Christofidou, The University of Sheffield, United Kingdom

Författare

Abdul Shaafi Shaikh

Chalmers, Industri- och materialvetenskap, Material och tillverkning

Shaikh, A.S., Mehta, B., Yao, Y., Hryha, E. The impact of B and Zr content on processability, microstructure, and mechanical performance of additively manufactured superalloy IN738LC

Microstructure and mechanical properties of Haynes 282 superalloy produced by laser powder bed fusion

Materials Today Communications,;Vol. 26(2021)

Artikel i vetenskaplig tidskrift

On as-built microstructure and necessity of solution treatment in additively manufactured Inconel 939

Powder Metallurgy,;Vol. 66(2023)p. 3-11

Artikel i vetenskaplig tidskrift

On the effect of building platform material on laser-powder bed fusion of a Ni-base superalloy HAYNES® 282®

European Journal of Materials,;Vol. 3(2023)

Artikel i vetenskaplig tidskrift

Shaikh, A.S., Fardan, A., Mishurova, T., Hryha, E. Effect of high productivity processing on microstructure and mechanical performance of additively manufactured Ni-base alloy IN625

Shaikh, A.S., Fardan, A., Mishurova, T., Hryha, E. The impact of high productivity processing on the fatigue failure of an additive manufactured superalloy HAYNES® 282®

De flesta metallegeringar är starka vid rumstemperatur men tappar styrka när temperaturen stiger. Superlegeringar behåller dock sin styrka i tusentals timmar vid temperaturer nära deras smältpunkt. Dessa material är avgörande för flygplansmotorer och turbiner för kraftgenerering. Ingenjörer undersöker 3D-printing av superlegeringar för att förbättra dessa maskiners prestanda och effektivitet. 3D-printatsuperlegeringar är dock utmanande på grund av sprickbildning, förlust av hållbarhet vid hög temperatur och kostnad. Att förstå och lösa dessa metallurgiska frågor är fokus för denna avhandling.

Superlegeringar är komplexa och innehåller ofta över tio grundämnen. Vi fick veta att de kemiska grundämnena bor och zirkonium, som bara utgör 1 av 1000 atomer, påverkar sprickbildningen under 3D-printing. Men dessa element är viktiga för att upprätthålla hållfasthet vid hög temperatur och kan inte tas bort från legeringen. Genom att experimentera med olika sammansättningar och studera smält- och frysbeteenden hittade vi ett sätt att förhindra sprickor samtidigt som vi bevarar styrkan.

Vår forskning visade att storleken och formen på de små kristallerna kornen som utgör superlegeringen är avgörande för långvarig hållbarhet vid höga temperaturer. Den första värmebehandlingen som appliceras direkt efter 3D-printing är särskilt viktig eftersom den kan förändra kornens storlek, form och gränskaraktär.

I 3D-printing smälter en laser lager av metallpulver för att bygga delar. Våra tester visade att ökad tjocklek på metallpulverlagren kan minska kostnaderna men kan befordra defekter. Trots detta förblir egenskaperna jämförbar med konventionellt tillverkad material.

Sammanfattningsvis håller 3D-printing på att bli en värdefull metod för tillverkning av superlegeringar, med potential att förbättra hållbarhet och prestanda inom energi- och flyg.

Most metal alloys are strong at room temperature but lose strength as the temperature rises. Superalloys, however, retain their strength for thousands of hours at temperatures close to their melting point. These materials are crucial for aeroplane engines and turbines for power generation. Engineers are exploring 3D printing of superalloys to improve the performance and efficiency of these machines. However, 3D printing superalloys is challenging due to crack formation, loss of high-temperature durability, and cost. Understanding and solving these metallurgical issues is the focus of this thesis. 
Superalloys are complex, often containing over ten elements. We found that the chemical elements boron and zirconium, which make up only 1 out of every 1000 atoms, significantly affect crack formation during 3D printing. But these elements are essential for maintaining high-temperature strength and cannot be removed from the alloy. By experimenting with different compositions and studying melting and freezing behaviours, we found a way to prevent cracks while preserving strength. 
Our research showed that the size and shape of the small grains that make up the superalloy are critical for long-term durability at high temperatures. The first heat treatment applied directly after 3D printing is especially important as it can alter the size, shape, and boundary character of the grains. 
In 3D printing, a laser melts layers of metal powder to build parts. Our tests showed that increasing the thickness of the layers can reduce costs but may lead to defects. Despite this, the properties remain competitive with conventionally produced materials. 
In summary, 3D printing is becoming a valuable method for manufacturing superalloys, with the potential to enhance sustainability and performance in energy and aerospace applications.

Ämneskategorier (SSIF 2025)

Metallurgi och metalliska material

Bearbetnings-, yt- och fogningsteknik

Keramiska och pulvermetallurgiska material

Materialteknik

Drivkrafter

Hållbar utveckling

Infrastruktur

Chalmers materialanalyslaboratorium

Additiv tillverkning vid Chalmers

Styrkeområden

Materialvetenskap

ISBN

978-91-8103-195-9

Doktorsavhandlingar vid Chalmers tekniska högskola. Ny serie: 5653

Utgivare

Chalmers

VDL, M-huset, Campus Johanneberg

Online

Opponent: Professor K. A. Christofidou, The University of Sheffield, United Kingdom

Mer information

Senast uppdaterat

2025-04-23