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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...
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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. More
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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× More
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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 More
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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 More
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Published: 01 January 1990
Fig. 36 Location and structure of tungsten fibers in fiber-reinforced superalloy composite turbine blades for rocket engine turbopumps. Courtesy NASA Lewis Research Center More
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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 More
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Published: 30 September 2015
Fig. 2 Isothermal superalloy forging More
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Published: 30 September 2015
Fig. 36 Average low-cycle fatigue life for a PM superalloy during 1980 through 1996 More
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Published: 01 December 2008
Fig. 10 (a) Freckles in a single-crystal nickel-base superalloy prototype blade. (b) Closeup of a single freckle. The freckles are approximately 2 mm (0.1 in.) in diameter. More
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Published: 01 January 1996
Fig. 21 Effect of grain size on fatigue crack growth of Waspaloy superalloy. Source: Ref 50 More
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Published: 27 April 2016
Source: L. Kaufman and H. Nesor, Calculation of Superalloy Phase Diagrams: Part IV, Metall. Trans. A , Vol 6, 1975, p 2123–2131 ( Ref 6 ) More
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Published: 27 April 2016
Source: L. Kaufman and H. Nesor, Calculation of Superalloy Phase Diagrams: Part IV, Metall. Trans. A , Vol 6, 1975, p 2123–2131 ( Ref 6 ) More
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Published: 27 April 2016
Source: L. Kaufman and H. Nesor, Calculation of Superalloy Phase Diagrams: Part IV, Metall. Trans. A , Vol 6, 1975, p 2123–2131 ( Ref 6 ) More
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Published: 27 April 2016
Source: L. Kaufman and H. Nesor, Calculation of Superalloy Phase Diagrams: Part I, Metall. Trans ., Vol 5, 1974, p 1617–1621 ( Ref 8 ) More
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Published: 27 April 2016
Source: L. Kaufman and H. Nesor, Calculation of Superalloy Phase Diagrams: Part I, Metall. Trans ., Vol 5, 1974, p 1617–1621 ( Ref 8 ) More
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Published: 27 April 2016
Source: L. Kaufman and H. Nesor, Calculation of Superalloy Phase Diagrams: Part I, Metall. Trans ., Vol 5, 1974, p 1617–1621 ( Ref 8 ) More
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Published: 27 April 2016
Source: L. Kaufman and H. Nesor, Calculation of Superalloy Phase Diagrams: Part IV, Metall. Trans. A , Vol 6, 1975, p 2123–2131 ( Ref 6 ) More
Image
Published: 27 April 2016
Source: L. Kaufman and H. Nesor, Calculation of Superalloy Phase Diagrams: Part IV, Metall. Trans. A , Vol 6, 1975, p 2123–2131 ( Ref 6 ) More
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Published: 27 April 2016
Source: L. Kaufman and H. Nesor, Calculation of Superalloy Phase Diagrams: Part IV, Metall. Trans. A , Vol 6, 1975, p 2123–2131 ( Ref 1 ) More