8th International Symposium on Superalloy 718 and Derivatives (2014) 2014
DOI: 10.7449/2014/superalloys_2014_67_77
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Development of a New Cast and Wrought Alloy (Rene 65) for High Temperature Disk Applications

Abstract: Rene 65 was developed as a nickel-base, gamma prime strengthened, aerospace turbine disk superalloy to provide increased temperature capability compared to direct age (DA) 718 and bridge the performance and cost gap between traditional cast and wrought alloys and powder alloys. A full scale development program was successfully executed to define a robust processing window resulting in successful production introduction of the alloy. Conventional hot die forging, over a wide range of strain rate processes, has … Show more

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Cited by 23 publications
(14 citation statements)
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“…René 65 TM is a commercial polycrystalline γ-γ' nickel based superalloy, which nominal composition in wt% is 13 Cr-16 Co-3.7 Ti-2.1 Al-4 Mo-4 W-1 Fe-0.7 Nb-0.05 Zr, 0.016 B, balance Ni [31]. Double-cone shaped samples were withdrawn from an industrially forged piece.…”
Section: Materials and Experimental Setupmentioning
confidence: 99%
“…René 65 TM is a commercial polycrystalline γ-γ' nickel based superalloy, which nominal composition in wt% is 13 Cr-16 Co-3.7 Ti-2.1 Al-4 Mo-4 W-1 Fe-0.7 Nb-0.05 Zr, 0.016 B, balance Ni [31]. Double-cone shaped samples were withdrawn from an industrially forged piece.…”
Section: Materials and Experimental Setupmentioning
confidence: 99%
“…René 65 TM is a γ–γ’ polycrystalline nickel‐based superalloy that has been derivated from the René 88 TM PM alloy for allowing the casting and forging processing route (Heaney et al ., ). γ–γ’ nickel‐based superalloys are basically composed of a γ matrix (FCC solid solution) and second‐phase γ’ precipitates adopting a L1 2 crystal structure.…”
Section: Introductionmentioning
confidence: 97%
“…a, with dimensions following ASTM E1820. The material was a Nickel superalloy with yield strength of 1213 MPa (176 ksi) at 0.2% offset, Young's modulus of 219.9 GPa (31.9 Msi), Poisson's ratio of 0.3 and density of 27 680 kg m −3 (14.15 lb/in 3 ) . Prior to fatigue crack experiments, a similar setup was used in accordance to ASTM E1820 to grow pre‐cracks of approximately 60 mils (1.52 mm), which were monitored using the DIC system with a field of view (FOV) of 10 × 8 mm (393.70 × 314.96 mils).…”
Section: Methodsmentioning
confidence: 99%