Castability of 718Plus(®) Alloy for Structural Gas Turbine Engine Components
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Publisher
John Wiley & Sons, Inc.
Link
http://onlinelibrary.wiley.com/wol1/doi/10.1002/9781118495223.ch9/fullpdf
Reference6 articles.
1. R. L. Kennedy, “Allvac® 718Plus™, Superalloy for the Next Forty Years.” Superalloys 718, 625, 706 and Derivates 2005, p.1. E. A. Loria, ed. TMS 2005
2. Wei-Di Cao, “Solidification and Solid State Phase Transformations of Allvac® 718Plus™ Alloy.” Superalloys 718, 625, 706 and Derivatives 2005. p. 165. E. A. Loria, ed. TMS 2005
3. R. E. Schafrik, D. D. Ward, and J. R. Groh, “Application of Alloy 718 in GE Aircraft Engines: Past, Present and Next Five Years.” Superalloys 718, 625, 706 and Various Derivatives 2001, p. 1. E. A. Loria, ed. TMS (The Minerals, Metals & Materials Society), Warrendale, PA 15086-7528, 2001
4. E.A. Ott, J. Groh, and H. Sizek. ”Metal Affordability Initiative: Application of Allvac Alloy 718Plus® for Aircraft Engine Static Structural Components.” Superalloys 718, 625, 706 and Derivatives 2005 , E.A. Loria, ed. The Mineral Metals and Materails Society, 2005
5. D. F. Paulonis and J. J. Schirra, “Alloy 718 at Pratt and Whitney-Historical Perspective and Future Challenges.” Superalloys 718, 625, 706 and Various Derivatives 2001, p. 13. E. A. Loria, ed. TMS 2001
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1. The Effect of Boron and Zirconium on the Structure and Tensile Properties of the Cast Nickel-Based Superalloy ATI 718Plus;Journal of Materials Engineering and Performance;2018-04-23
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