Multi-Class Grain Size Model for Forged Alloy 718 Aircraft Parts

Article Preview

Abstract:

The evolution of microstructural features such as local grain size and local grain size distribution are essential in view of the final physical and mechanical properties of the nickel base alloy 718 for aircraft parts forged in a multi-step production route. Due to increasing standards and the need of the prediction of fracture mechanical properties, a multi-class grain size model for a more detailed microstructure prediction is necessary. Therefore, a multi-class model considers the real initial non-uniform grain size distribution and structure of the pre-material at the beginning of the forging process, which affects the evolution of grain sizes during thermo-mechanical treatment and leads to different results than commonly used uniform grain structures. The initial distribution is defined by grain classes according the ASTM standard. It is shown that the presence of different classes and distributions of grains are as import as the applied strain, strain rate and temperature on dynamic, meta-dynamic and static recrystallization. Additionally, dissolution processes of delta phase and grain growth kinetics are included in the model to properly indicate the recrystallized fractions and represent the resulting multi-class microstructure. A series of simulations with different initial distributions is discussed and compared with examined forged samples in terms of the resulting microstructure for typical forging parameters. Based on these results the microstructure model can be used in combination with collected process data to predict the resulting properties and for the design of new aircraft parts.

You might also be interested in these eBooks

Info:

Periodical:

Materials Science Forum (Volume 1016)

Pages:

499-508

Citation:

Online since:

January 2021

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2021 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

* - Corresponding Author

[1] M. Stockinger, Microstructural Simulation of Closed Die Forging of Nickel Base Alloys Ph.D. thesis, University of Technology Graz, Austria, (2003).

Google Scholar

[2] M. Stockinger, A. Stanojevic, V. Wieser, P. Raninger, Development of an Automated Property Simulation Tool for Direct Aged Alloy 718 Engine Disk Forgings, Proceedings of the 9th International Symposium on Superalloy 718 & Derivatives: Energy, Aerospace, and Industrial Applications, (2018), 353-367.

DOI: 10.1007/978-3-319-89480-5_21

Google Scholar

[3] P. Poelt, C. Sommitsch, S. Mitsche, M. Walter, Dynamic recrystallization of Ni-base alloys—Experimental results and comparisons with simulations, Materials Science and Engineering A420, (2006), 306-314.

DOI: 10.1016/j.msea.2006.01.076

Google Scholar

[4] ASTM standard E 112 – 96 (Reapproved 2004), ASTM International, (2004).

Google Scholar

[5] M. Stockinger, J. Tockner, Optimizing the forging of critical aircraft parts by the use of finite element coupled microstructure modelling, Superalloys 718, 625, 706 and Derivates 2005, TMS, (2005), 87-95.

DOI: 10.7449/2005/superalloys_2005_87_95

Google Scholar

[6] A. Cingara, St. Germain, H.J. McQueen, Comparison of Calculated and Experimental Flow Curves, Proc. Int. Symp. Processing, Microstructure and Properties of HSLA Steels, (1987).

Google Scholar

[7] R.W. Cahn, P. Haasen, Physical Metallurgy, Amsterdam, Elsevier, (1983).

Google Scholar

[8] C.M. Sellars, J.A. Whiteman, Recrystallization and Grain Growth in Hot Rolling, Materials Science, 2 (1979), 187-194.

DOI: 10.1179/msc.1979.13.3-4.187

Google Scholar

[9] A.J. Brand, K. Karhausen, R. Kopp, Microstructural Simulation of Nickel Base Alloy Inconel 718 in Production of Turbine Discs, Materials Science and Technology, 12 (1996), 963-969.

DOI: 10.1179/mst.1996.12.11.963

Google Scholar

[10] D. Huang et al., Computer Simulation of Microstructure Evolution During Hot Forging of Waspaloy and Nickel Alloy 718, Proc. Microstructure Modeling and Prediction During Thermomechanical Processing, (2001), 137-146.

Google Scholar

[11] S.C. Medeiros et al., Microstructural Modeling of Metadynamic Recrystallization in Hot Working of IN 718 Superalloy, Materials Science and Engineering, 293 (2000), 198-207.

DOI: 10.1016/s0921-5093(00)01053-4

Google Scholar