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Thermal Fatigue of Components with Compositional Gradients of Multiphase NiAl-X and Alloy IN 738

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Published/Copyright: December 2, 2021

Abstract

Following a short evaluation of the advantages and weaknesses of materials based on NiAl for high temperature applications, it is proposed that compositionally graded design of components might be a viable solution to the problem of parts which are subjected to varying loads at both low and high temperature. Following this principle, specimens have been prepared by powder metallurgical techniques with composition and microstructure gradually changing from NiAl reinforced with ternary Laves phases (with Nb and Ta) for the hot section, to superalloy IN 738 for the low temperature section of the component. These specimens have been subjected to thermal fatigue testing between 200 and 1100 °C. Crack initiation and propagation have been observed by SEM and quantitatively evaluated. The advantage of the graded solution with respect to crack arrest is obvious. The different factors governing thermal fatigue behavior of graded components are discussed in detail.


Dedicated to Prof Dr. rer. nat. Volkmar Gerold on the occasion of his 75th birthday

B. Ilschner Laboratoire de Métallurgie Méchanique Ecole Polytechnique Fédérale de Lausanne CH-1015 Lausanne, Switzerland
Knut Barthel Eidgenöss. Materialprüfungs- und Forschungsanstalt, CH-3602 Thun, Switzerland

Funding statement: The authors acknowledge financial support from the Swiss Priority Program on Materials Research (PPM). They would also like to thank Prof. Sauthoff and Ms. Sanders from Max-Planck-Institut Düsseldorf for providing prealloyed NiAl-Ta powder. Helpful discussions with Drs. N. Cherradi, F. Meyer-Olbersleben and F. Rézai-Aria are gratefully appreciated

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Received: 1997-02-20
Published Online: 2021-12-02

© 1997 Carl Hanser Verlag, München

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