Cyclic Oxidation Behavior of Conventional and Niobium-Modified MAR-M246 Superalloy at 900 and 1000 °C

Author:

de Faria Cunha Filipe Augusto1,de Andrade Reis Rodrigo12,Gonçalves Samantha Pinto1,Fernandes Frederico Augusto Pires3,Baldan Renato4ORCID,de Sousa Malafaia Artur Mariano1ORCID

Affiliation:

1. Campus Santo Antônio, São João del-Rei Federal University (UFSJ), Praça Frei Orlando, 170, Centro, São João del-Rei 36307-352, MG, Brazil

2. Science and Technology of Minas Gerais, Federal Institute of Education, Ouro Branco, R. Afonso Sardinha, 90-Bairro Pioneiros, Ouro Branco 36420-000, MG, Brazil

3. Center for Engineering, Modeling and Applied Social Sciences (CECS), Federal University of ABC (UFABC), Alameda da Universidade, s/n, São Bernardo do Campo 09606-045, SP, Brazil

4. Campus of Itapeva, São Paulo State University (Unesp), Rua Geraldo Alckmin 519, Vila Nossa Senhora de Fátima, Itapeva 18409-010, SP, Brazil

Abstract

Nickel-based superalloys have excellent properties at high temperatures, which makes them appropriate for applications such as turbocharges and aeronautic gas turbines. MAR-M246 is a superalloy developed for these kinds of applications. The objective of this work was to study the total replacement of Ta by Nb in atomic percentage for this superalloy, regarding the oxidation resistance. Although both elements have the same role (form the γ’ precipitates) in nickel-based superalloys, Ta is more expensive than Nb. Thus, this replacement leads to the possibility of a price reduction. This work studied both conventional MAR-M246(Ta) and experimental MAR-M246(Nb) on cyclic oxidation tests at 900 and 1000 °C for up to 180 cycles. The oxide products were characterized by SEM/EDS and XRD analysis. The products of oxidation were mainly TiO2, Al2O3, Cr2O3, NiO, and Ni(Co)Cr2O4. Mass gain variation per unit area was stable for both materials and temperatures. However, spalled areas were detected for tests performed at 1000 °C. The results obtained here suggest that use of Nb instead of Ta can be considered regarding high temperature oxidation for MAR-M246 superalloy.

Funder

São Paulo Research Foundation

Coordination for the Improvement of Higher Education Personnel

Publisher

MDPI AG

Subject

Materials Chemistry,Surfaces, Coatings and Films,Surfaces and Interfaces

Reference26 articles.

1. Solutioning and aging of MAR-M247 nickel-based superalloy;Baldan;J. Mater. Eng. Perform.,2013

2. Bhadeshia, H. (2021, January 16). Nickel Based Superalloys. Available online: http://www.phase-trans.msm.cam.ac.uk/2003/Superalloys/superalloys.html.

3. Campbell, F.C. (2006). Manufacturing Technology for Aerospace Structural Materials, Elsevier.

4. High speed machining of aero-engine alloys;Ezugwu;J. Braz. Soc. Mech. Sci. Eng.,2004

5. Reed, R.C. (2006). The Superalloys Fundamentals and Applications, Cambridge University Press.

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