Forming Process Simulation and Optimization of Nickel-Base Superalloy Turbine Disk

Wan Lin Zhou; Wen Hao Chen; Fu Jun Zhang

doi:10.4028/www.scientific.net/AMR.1004-1005.1156

Paper Titles

Effect of Porosity on Compressive Properities of Porous Titanium with Helical Pores Structure
p.1137

Effect of Process Parameters on Warpage of Printer Board with Metal-Insert
p.1141

Effects of Grain Size on Crack Tip Mechanical Fields of Intergranular Cracking
p.1147

Fabrication of the Sheet-Metal Part with Non-Horizontal End Face Based on the CNC Incremental Forming
p.1152

Forming Process Simulation and Optimization of Nickel-Base Superalloy Turbine Disk
p.1156

Foundry Technique Designing of the Nodular Cast Iron Casting
p.1162

Microscopic Stress Analysis of Body-Centered Cubic Crystal under High Cycle Fatigue
p.1166

Numerical Simulation and Optimization of Low Pressure Die Casting of Aluminum Alloy Cylinder Block
p.1172

Research on Al Particles Reinforced Thermal Stress Aging Treatment Behavior of Composite Lead-Free Solder
p.1178

HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 1004-1005Forming Process Simulation and Optimization of...

Forming Process Simulation and Optimization of Nickel-Base Superalloy Turbine Disk

Abstract:

Turbine disc is the key component of aviation engine, its performance is important to ensure the reliability and safety of the whole aviation engine. In this paper, forging forming of GH4169 alloy turbine disks of certain type aero-engine are discsimulated by DEFORM-3D soft system,these forming methods include next three kinds: common hot die forging, isothermal forging and composite sheath hot die forging.The influences of various forging ways on turbine disk forging quality and the used die are analyzed in order to find the most suitable way of forging. The forging defects in the forging process are analyzed . For basically eliminating these defects, the forging process of superalloy turbine disk are optimized based on the most economical and simple principles and some useful methds are gained，which will provide a reference to actual superalloy turbine disk forging process.

You might also be interested in these eBooks

View Preview

Info:

Periodical:

Advanced Materials Research (Volumes 1004-1005)

Pages:

1156-1161

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.1004-1005.1156

Citation:

Cite this paper

Online since:

August 2014

Authors:

Wan Lin Zhou*, Wen Hao Chen, Fu Jun Zhang

Keywords:

Celluar Automata, Dynamic Recrystallization, Microstructure Simulation, Superalloy, Turbine Disc

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

* - Corresponding Author

References

[1] Burger J L, Biederman R R, et al. The Effects of Starting Condition on The Aging Response of As-Forged Alloy 718[J]. Superalloy 718-Metallurgy and Applications, 1989: 207~217.

DOI: 10.7449/1989/superalloys_1989_207_217

Google Scholar

[2] Jong Taek Yeom, Chong Soo Lee, et al. Finite-element analysis of microstructure evolution in the cogging of an Alloy 718 ingot[J]. Materials Science and Engineering, 2007: 772~726.

DOI: 10.1016/j.msea.2006.02.415

Google Scholar

[3] Radhakrishnan B, Zzcharia T. Simulation of curture-drvien grain growth by using a modified Monte Carlo algorithm[J]. Metallurgical and Materials Transactions A, 1995, 26A(1): 167~180.

DOI: 10.1007/bf02669802

Google Scholar

[4] Radhakrishnan B, Sarma G B, Zacharia T. Monte Carlo simulation of deformation substructure evolution during recrystallzation[J]. Scripta Materials Letters, 2002, 56: 47~52.

Google Scholar

[5] N. Yazdipour C.H. J,P.D. Hodgson. Microstructural modeling of dynamic recrystallization using irregular celluar automata. Computation Materials Science, 2008, 44: 566~576.

DOI: 10.1016/j.commatsci.2008.04.027

Google Scholar