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Superalloy
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Series: ASM Desk Editions
Publisher: ASM International
Published: 01 December 1998
DOI: 10.31399/asm.hb.mhde2.a0003120
EISBN: 978-1-62708-199-3
... Abstract Superalloys are nickel, iron-nickel, and cobalt-base alloys generally used for high-temperature applications. Superalloys are used in aircraft, industrial, marine gas turbines, nuclear reactors, spacecraft structures, petrochemical production, orthopedic and dental prostheses...
Abstract
Superalloys are nickel, iron-nickel, and cobalt-base alloys generally used for high-temperature applications. Superalloys are used in aircraft, industrial, marine gas turbines, nuclear reactors, spacecraft structures, petrochemical production, orthopedic and dental prostheses, and environmental protection applications. This article discusses the material characteristics, phases, structures, and systems of superalloys. It describes the processing of superalloys, including primary and secondary melting, deformation processing (conversion), powder processing, investment casting, and joining methods. The article also describes the properties, microstructure, and thermal exposure of superalloys. It further discusses the effects of environmental factors on superalloys, including oxidation and hot corrosion. Protective coatings are also discussed. The article provides information on the mechanical properties and chemical composition of nickel, iron, and cobalt-base superalloys in both the cast and wrought forms.
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Published: 01 January 1986
Fig. 27 AEM-EDS spectra collected from the iron-base superalloy Haynes Alloy 556. (a) Bright-field image of precipitates that decorate the grain boundaries. (b) and (c) show EDS spectra from the matrix and particles, respectively. Iron, chromium, nickel, cobalt, molybdenum, tungsten
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Published: 01 January 1986
Fig. 39 AEM analysis of an iron-base superalloy. (a) η-Ni 3 Ti platelets. (b) Electron diffraction pattern in nearby γ matrix at zero specimen tilt. Zone axis is close to [001] γ .
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Published: 01 August 2013
Fig. 1 Example of grains in a wrought superalloy material. Hastelloy X is shown with frequent twinning due to imparted strains.
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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 June 2016
Fig. 12 Gamma prime (γ′) phase in superalloy forging (Astroloy) at three different magnifications. (a) The forging was solution annealed at 1150 °C (2100 °F) for 4 h, air cooled, aged at 1080 °C (1975 °F) for 4 h, oil quenched, aged at 845 °C (1550 °F) for 4 h, air cooled, aged at 760 °C (1400
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Published: 01 January 1994
Fig. 3 Archetypical microstructures of aluminide coatings on a nickel superalloy. (a) Inward diffusion based on Ni 2 Al 3 (and aluminum-rich NiAl). (b) Same as (a) but heat treated at 1080 °C (1975 °F). (c) Outward diffusion of nickel in nickel-rich NiAl. (d) Inward diffusion of aluminum
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Published: 01 January 1994
Fig. 5 Chromium diffusion coatings on a nickel superalloy by (a) pack cementation and (b) out-of-contact gas-phase processing. Both at 500×. Source: Ref 37
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Published: 30 September 2015
Fig. 36 Average low-cycle fatigue life for a PM superalloy during 1980 through 1996
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Published: 30 September 2015
Fig. 7 Hot isostatic pressing densification maps for a nickel-base superalloy powder having a particle diameter of 50 µm (2 mils). (a) Density as a function of pressure (pressure expressed as the log of the ratio of applied hydrostatic pressure over flow stress) when processed at constant
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Published: 01 June 2016
Fig. 41 Example of quench cracking in a powder metallurgy superalloy disk rim
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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 June 2016
Fig. 6 As-cast structure of Co-Cr-W-Ta superalloy (MAR-M 509). (a) The structure consists of metal carbide (MC) particles in script form and M 23 C 6 particles in eutectic form (gray areas) and precipitate form in the dendritic alpha solid-solution matrix. (b) Higher magnification reveals
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Published: 01 June 2016
Fig. 7 As-cast microstructure of Co-Cr-W-Ta superalloy (MAR-M 302). (a) Structure at 100× reveals primary or eutectic M 6 C carbides (dark gray) and MC particles (small white crystals in solid-solution matrix). (b) At higher magnification (500×), the mottled gray islands are primary eutectic
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in Wrought and P/M Superalloys
> Properties and Selection: Irons, Steels, and High-Performance Alloys
Published: 01 January 1990
Fig. 15 Flow diagram of processes widely used to produce superalloy components. Source: Ref 22
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in Wrought and P/M Superalloys
> Properties and Selection: Irons, Steels, and High-Performance Alloys
Published: 01 January 1990
Fig. 17 Gas atomization system for superalloy powder production. (a) Atomization nozzle. (b) Typical system. Source: Ref 28
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in Wrought and P/M Superalloys
> Properties and Selection: Irons, Steels, and High-Performance Alloys
Published: 01 January 1990
Fig. 18 Soluble gas atomization system for producing superalloy powder. Source: Ref 28
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in Polycrystalline Cast Superalloys
> Properties and Selection: Irons, Steels, and High-Performance Alloys
Published: 01 January 1990
Fig. 3 The evolution of the processing of nickel-base superalloy turbine blades. (a) From left, equiaxed, directionally solidified, and single-crystal blades. (b) An exposed view of the internal cooling passages of an aircraft turbine blade. Source: Ref 5
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