Evaluation of Inconel 718 Creep Behavior

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Abstract:

Superalloys are used primarily in aerospace applications. These applications require a material with high mechanical strength, good resistance to fatigue and creep, good corrosion resistance and ability to operate continuously at elevated temperatures. These alloys were developed for elevated temperature service, where relatively severe mechanical stressing is encountered, and where high surface stability is frequently required. Inconel 718 has being investigated because it is one of the most widely used superalloys. Constant load creep tests were conducted on a standard creep machine at 600 and 700°C and stress levels of 300 MPa. Sets of curves and experimental parameters for the primary, secondary and tertiary regions, as a function of stress and temperature applied were obtained. The ductility, the creep rate and lifetime was evaluated.

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Periodical:

Defect and Diffusion Forum (Volumes 326-328)

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525-529

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April 2012

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© 2012 Trans Tech Publications Ltd. All Rights Reserved

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[1] T. Giampaolo: The gas turbine handbook: Principles and practices 2. ed., Marcel Dekker Inc. (2002).

Google Scholar

[2] D.G. Backman, J.C. Williams: Science Vol. 255 (1992), p.1082.

Google Scholar

[3] American Society for Testing and Materials, Philadelphia. B 265-89. Standard specification, sheet and plate. Philadelphia, (1990).

Google Scholar

[4] ASTM E-8, American Association State Highway and Transportation Officials Standard - Annual Book of ASTM Standards.

Google Scholar

[5] ASTM E-139/83, American Society for Testing and Materials, 1990, Surface Engineering, v. 5, Philadelphia.

Google Scholar

[6] T. Psugahara, C. Moura Neto, , D.A.P. Reis, A.O. Hirschmann, F. Piorino Neto, Estudo do comportamento em fluência da superliga Inconel 718, ENCITA 2009, São José dos Campos.

DOI: 10.5151/2594-4711-23253

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