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nickel-base superalloys
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Series: ASM Handbook
Volume: 22A
Publisher: ASM International
Published: 01 December 2009
DOI: 10.31399/asm.hb.v22a.a0005459
EISBN: 978-1-62708-196-2
... Abstract This article summarizes the general features of microstructure evolution during the thermomechanical processing (TMP) of nickel-base superalloys and the challenges posed by the modeling of such phenomena. It describes the fundamentals and implementations of various modeling...
Abstract
This article summarizes the general features of microstructure evolution during the thermomechanical processing (TMP) of nickel-base superalloys and the challenges posed by the modeling of such phenomena. It describes the fundamentals and implementations of various modeling methodologies. These include JMAK (Avrami) models, topological models, and mesoscale physics-based models.
Book: Fatigue and Fracture
Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.a0002410
EISBN: 978-1-62708-193-1
... Abstract This article discusses fracture, fatigue, and creep of nickel-base superalloys with additional emphasis on directionally solidified and single-crystal applications. It analyzes the physical metallurgy of these alloys. The effects of grain boundary and grain size on failure...
Abstract
This article discusses fracture, fatigue, and creep of nickel-base superalloys with additional emphasis on directionally solidified and single-crystal applications. It analyzes the physical metallurgy of these alloys. The effects of grain boundary and grain size on failure are summarized. The article also discusses the effects of microstructure and extrinsic parameters on fatigue crack propagation (FCP). It details the modeling of FCP rates and creep and creep-fatigue crack growth rates.
Series: ASM Handbook
Volume: 24
Publisher: ASM International
Published: 15 June 2020
DOI: 10.31399/asm.hb.v24.a0006582
EISBN: 978-1-62708-290-7
... Abstract This article covers the current state of materials development of nickel-base superalloys for additive manufacturing (AM) processes and the associated challenges. The discussion focuses on nickel-base superalloy fusion AM processes, providing information on typically encountered...
Abstract
This article covers the current state of materials development of nickel-base superalloys for additive manufacturing (AM) processes and the associated challenges. The discussion focuses on nickel-base superalloy fusion AM processes, providing information on typically encountered cracking mechanisms in AM nickel-base superalloys, such as solid-solution-strengthened nickel-base superalloys and precipitate-strengthened nickel-base superalloys. The mechanisms include solidification cracking, strain-age cracking, liquation cracking, and ductility-dip cracking. The article also provides a short discussion on binder jet AM and powder recyclability.
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Published: 01 June 2016
Fig. 2 General comparison of creep rupture of conventional nickel-base superalloys. (a) 100 h creep-rupture strength of gamma-prime (γ′) nickel alloys compared to solid-solution and carbide-strengthened alloys. (b) 1000 h creep-rupture strength of some selected nickel superalloys
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in Introduction to Fundamentals of Modeling for Metals Processing
> Fundamentals of Modeling for Metals Processing
Published: 01 December 2009
Fig. 2 Recent discovery of microtwins in nickel-base superalloys after creep deformation has led to further investigation and development of a model that describes this new mechanism. Courtesy of M. Mills, The Ohio State University
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Published: 01 December 1998
Fig. 12 Wrought nickel-base superalloys showing spheroidal nature of early (low V f γ′) alloys (Waspaloy, left) and cuboidal nature of later (higher V f γ′) alloys (U 700, right). Note secondary (cooling) γ′ between primary cuboidal γ′ particles in U 700. Original magnification, 6800×
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Published: 01 December 2009
Fig. 5 Static crack growth rates for five nickel-base superalloys at 650 °C, showing that the differences in their behavior in air are dominated by environmental interaction. Source: Ref 7
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in Wrought and P/M Superalloys
> Properties and Selection: Irons, Steels, and High-Performance Alloys
Published: 01 January 1990
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in Strategic Materials Availability and Supply
> Properties and Selection: Irons, Steels, and High-Performance Alloys
Published: 01 January 1990
Fig. 2 Increased use of refractory metals in nickel-base superalloys. (a) Weight percent. (b) Atomic percent
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Published: 01 January 1996
Fig. 21 High-temperature fatigue crack growth of two nickel-base superalloys. (a) Hastelloy X at 760 °C (1400 °F) with R = 0.05. (b) NASA 11B-7 at 650 °C (1200 °F) with R = 0.05.
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Published: 01 January 2005
Fig. 11 Resistance of selected cast nickel-base superalloys to plastic deformation at elevated temperatures. H11 is included for comparison. Source: Ref 15
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Published: 01 January 2005
Fig. 12 Resistance of selected wrought nickel-base superalloys to plastic deformation at elevated temperatures. H11 is included for comparison. Source: Ref 15 , 16
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Published: 15 June 2020
Fig. 3 Tendency for cracking in nickel-base superalloys based on aluminum and titanium content as susceptible to strain-age cracking. LSHR, low solvus, high refractory
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in Polycrystalline Cast Superalloys
> Properties and Selection: Irons, Steels, and High-Performance Alloys
Published: 01 January 1990
Fig. 5 Stress-rupture curves for selected superalloys. (a) and (b) Nickel-base superalloys. 1000 h. (c) Cobalt-base superalloys. 1000 h. Source: Ref 3 . (d) Larson-Miller stress-rupture curves for selected nickel-base superalloys. Source: Ref 7 . (e) Larson-Miller stress-rupture curves
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Published: 01 June 2016
Fig. 7 Strength (hardness) versus particle diameter in a nickel-base superalloy. Cutting occurs at low particle diameters, bypassing at higher particle diameters. Note also that aging temperature affects strength in conjunction with particle size.
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Published: 01 June 2016
Fig. 12 Nitrogen content versus depth for Inconel nickel-base superalloy heated at 815 °C (1500 °F) in nitrogen
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Published: 01 August 2013
Fig. 5 Recrystallized grains on a nickel-base superalloy after surface deformations due to processes such as grinding. Original magnification: 100×
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Published: 01 December 1998
Fig. 13 Strength (hardness) versus particle diameter in a nickel-base superalloy. Cutting occurs at low particle sizes, bypassing at larger sizes. Note that aging temperature also affects strength in conjunction with particle size.
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Published: 01 December 1998
Fig. 20 Stress-rupture behavior of B-1900 nickel-base superalloy, showing break in slope believed to be caused by γ′ coarsening
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Published: 01 December 1998
Fig. 14 Auger composition-depth profile of argon-atomized nickel-base superalloy powder. Source: Ref 5
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