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gamma prime
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Image
Published: 01 November 2010
Fig. D.13 Light, acicular sigma phase has formed in the gamma-gamma prime matrix; some sigma is also visible at boundaries of the platelets. Optical microscope, original magnification 500×. Condition: Heat treated—solution annealed 4 h at 1175 °C (2150 °F), aged 4 h at 1080 °C (1975 °F
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Image
Published: 01 November 2010
Fig. D.3 Details of delta phase crystals. Gamma prime precipitate is visible in the gamma matrix. Replica electron micrograph, original magnification 10,000× Condition: Solution treated and aged—solution annealed 1 h at 955 °C (1750 °F), air cooled, aged 8 h at 720 °C (1325 °F), and furnace
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Image
Published: 01 November 2010
Fig. D.8 Small, uniformly dispersed gamma prime precipitate and large, discontinuous M23C6 carbide at the grain boundary. Replica electron micrograph, original magnification 15,000×. Condition: Solution treated and aged—solution annealed 2 h at 1150 °C (2100 °F) and air cooled, then aged 24
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Image
Published: 01 November 2010
Fig. D.15 Precipitated carbide at grain boundaries and gamma prime within grains of the gamma solid-solution matrix. Replica electron micrograph, original magnification 4500×. Condition: Solution treated and aged—solution annealed 4 h at 1175 °C (2150 °F) and aged 24 h at 980 °C (1800 °F
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Image
Published: 01 October 2011
Fig. 14.18 Gamma prime (γ′) phase in superalloy forging (Astroloy) at three different magnifications. (a) 100×. (b) 1000×. (c) 10,000×. The forging was solution annealed at 1150 °C for 4 h, air cooled, aged at 1080 °C for 4 h, oil quenched, aged at 845 °C for 4 h, air cooled, aged at 760 °C
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Image
in Life-Assessment Techniques for Combustion Turbines
> Damage Mechanisms and Life Assessment of High-Temperature Components
Published: 01 December 1989
Fig. 9.40. Gamma-prime overaging and associated loss of creep strength in Udimet 710 tested at 845 °C and 350 MPa (1555 °F and 50 ksi) ( Ref 70 ; courtesy of P. Lowden, Liburdi Engineering, Ltd., Burlington, Canada). Top: New creep life, 140 h. Bottom: Service, 45,000 h; creep life, 10 h.
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Image
in Life-Assessment Techniques for Combustion Turbines
> Damage Mechanisms and Life Assessment of High-Temperature Components
Published: 01 December 1989
Fig. 9.41. Gamma-prime particle size as a function of t 1/3 (t is time of thermal exposure) for superalloys (based on Ref 7 , 8 , 64 , and 69 ).
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Image
in Process Modeling in Impression-Die Forging Using Finite-Element Analysis
> Cold and Hot Forging: Fundamentals and Applications
Published: 01 February 2005
Fig. 16.6 Prediction of the distribution of the size (μm) of gamma prime for a Rene 88 experimental forging
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Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 November 2010
DOI: 10.31399/asm.tb.sap.t53000139
EISBN: 978-1-62708-313-3
...: Heat treated (solution annealed 2 h at 1095 °C (2000 °F), air cooled, reannealed 1 h at 980 °C (1800 °F), air cooled, aged 16 h at 720 °C (1325 °F), air cooled) Source: Ref 1 , 2 Fig. D.3 Details of delta phase crystals. Gamma prime precipitate is visible in the gamma matrix. Replica...
Image
Published: 01 November 2010
Fig. D.6 The needlelike constituent is eta phase (Ni3Ti); the remainder of the structure is gamma prime in a gamma matrix. Negative-replica electron micrograph, original magnification 15,000×. Condition: Miscellaneous condition(s)—creep tested to rupture at 138 MPa (20 ksi) for 7380 h
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Image
Published: 01 November 2010
Fig. D.14 Structure is acicular sigma phase, M23C6 carbide at grain boundary, and gamma prime within the gamma matrix grains. Optical microscope, original magnification 4500×. Condition: Solution treated and aged—solution annealed 4 h at 1175 °C (2150 °F) and aged 1500 h at 815 °C (1500 °F
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Image
Published: 01 November 2010
Fig. D.7 The grain-boundary constituents (MC, M3B2, or both) contributed to low ductility. Note the grain-boundary depleted zone. The gamma matrix contains gamma prime precipitate. Replica electron micrograph, original magnification 10,000×. Condition: Heat treated—solution annealed 2 h
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Image
Published: 01 November 2010
Fig. D.9 Grain-boundary M23C6 carbide is stabilized, and precipitation of fine gamma prime particles has increased. Replica electron micrograph, original magnification 15,000×. Condition: Solution treated and aged—solution annealed 2 h at 1150 °C (2100 °F) and air cooled, then aged 24 h
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Series: ASM Technical Books
Publisher: ASM International
Published: 01 February 2005
DOI: 10.31399/asm.tb.chffa.t51040193
EISBN: 978-1-62708-300-3
.... The development and utilization of physical metallurgy-based microstructure models and the integration of the models with finite-element analysis has allowed for microstructure prediction by computer. Two important microstructural features of superalloy forgings are the grain size and the gamma-prime...
Abstract
This chapter discusses the use of finite-element modeling in forging design. It describes key modeling parameters and inputs, mesh generation and computation time, and process modeling outputs such as metal flow, strain rate, loading profiles, and microstructure. It also includes a variety of application examples.
Series: ASM Technical Books
Publisher: ASM International
Published: 01 July 2009
DOI: 10.31399/asm.tb.bcp.t52230179
EISBN: 978-1-62708-298-3
... at.% or 3 wt%. There are two congruent melting phases: The beta phase, with a cesium chloride-ordered cubic structure, melts at 1420 °C (2590 °F), and the gamma phase melts at 1400 °C (2550 °F). Gamma and gamma prime are closely related, with gamma being a disordered version of gamma prime. There are two...
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 March 2002
DOI: 10.31399/asm.tb.stg2.t61280025
EISBN: 978-1-62708-267-9
... prime gamma prime microstructure superalloys Groups, Crystal Structures, and Phases Superalloy Groups As noted earlier, there are three groups of superalloys (iron-nickel-, nickel-, and cobalt-base), which are further subdivided into cast and wrought (where wrought includes powder...
Abstract
This chapter describes the metallurgy of superalloys and the extent to which it can be controlled. It discusses the alloying elements, crystal structures, and processing sequences associated with more than a dozen phases that largely determine the characteristics of superalloys, including their properties, behaviors, and microstructure. It examines the role of more than 20 alloying elements, including phosphorus (promotes carbide precipitation), boron (improves creep properties), lanthanum (increases hot corrosion resistance), and carbon and tungsten which serve as matrix stabilizers. It explains how precipitates provide strength by impeding deformation under load. It also discusses the factors that influence grain size, shape, and orientation and how they can be controlled to optimize mechanical and physical properties.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2003
DOI: 10.31399/asm.tb.pnfn.t65900065
EISBN: 978-1-62708-350-8
... surface etches out white in appearance above the nitrided case. The zone is called “compound” due to the presence of more than one phase ( Fig. 1 ). Two phases generally are present in the compound zone: the epsilon (ε) phase, which has a chemical formula of Fe 2-3 N, and the gamma prime (γ′) phase, which...
Abstract
The compound zone that forms on the surface of nitrided steels is often called the white layer. When the nitrided sample is sectioned through the case, and then polished and etched with a standard solution of nital (2 to 5% nitric acid and alcohol), the immediate surface etches out as white in appearance above the nitrided case. This chapter focuses on the methods to control the compound zone, or white layer. It first provides information on a test to determine the presence of the white layer, and discusses the processes involved in the reduction of the compound zone by the two-stage process. Next, it describes other methods for controlling compound zone formation, and, finally, reviews the factors related to the determination of case depth in nitriding.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2008
DOI: 10.31399/asm.tb.ssde.t52310001
EISBN: 978-1-62708-286-0
... 6 fcc a = 10.57–10.68 Cr 16 Fe 5 Mo 2 C (e.g.) M 23 (C,B) 6 fcc a = 10.57–10.68 Cr 23 (C,B) 6 M 6 C Diamond cubic a = 10.62–11.28 (FeCr) 21 Mo 3 C; Fe 3 Nb 3 C; M 5 SiC M 2 N Hexagonal a = 2.8 c = 4.4 Cr 2 N MN Cubic a = 4.13–4.18 CrN Gamma prime fcc...
Abstract
Metallurgy, as discussed in this chapter, focuses on phases normally encountered in stainless steels and their characteristics. This chapter describes the thermodynamics and the three basic phases of stainless steels: ferrite, austenite, and martensite. Formation of the principal intermetallic phases is also covered. In addition, the chapter provides information on carbides, nitrides, precipitation hardening, and inclusions.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2003
DOI: 10.31399/asm.tb.pnfn.t65900193
EISBN: 978-1-62708-350-8
... surface. This is accomplished by changing the nature of the surface compound layer, which is also known as the white layer. The completed compound layer will form with both epsilon (ε) and gamma prime (γ′) phases. The dominant ε-phase resists abrasive wear. Ferritic nitrocarburizing improves...
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 October 2012
DOI: 10.31399/asm.tb.lmub.t53550299
EISBN: 978-1-62708-307-2
...-two + gamma) or three-phase (alpha-two + gamma + beta) near-gamma titanium aluminide alloys during ingot breakdown and/or rolling suggests that these materials may be prime candidates for superplastic forming. Materials were tested over a wide range of temperatures and strain rates. For most...
Abstract
Titanium aluminides are lightweight materials that have relatively high melting points and good high-temperature strength. They also tend to be stronger and lighter than conventional titanium alloys, but considerably less ductile. This chapter begins with a review of the titanium-aluminum phase diagram, focusing on the properties, compositions, and microstructures of alpha-2 Ti3Al alloys. It then describes the properties, microstructures, and compositions of orthorhombic, gamma, and near-gamma alloys as well as the processing methods and procedures normally used in their production.