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grain boundary precipitation
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in Mechanisms and Causes of Failures in Heat Treated Steel Parts
> Failure Analysis of Heat Treated Steel Components
Published: 01 September 2008
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Published: 01 August 1999
Fig. 8.14 (Part 1) Overheating: grain-boundary sulfide precipitation. 0.3% C, Ni-Cr-Mo alloy (0.32C-0.25Si-0.005S-0.006P-2.56Ni-0.84Cr-0.57Mo, wt%). Heated for 1 h at 1400 °C, cooled at 750 °C/h, austenitized at 850 °C, quenched in oil, tempered at 600 °C. 350 HV. (a) Scanning electron
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Published: 01 August 1999
Fig. 8.14 (Part 2) Overheating: grain-boundary sulfide precipitation. 0.3% C, Ni-Cr-Mo alloy (0.32C-0.25Si-0.005S-0.006P-2.56Ni-0.84Cr-0.57Mo, wt%). Heated for 1 h at 1400 °C, cooled at 750 °C/h, austenitized at 850 °C, quenched in oil, tempered at 600 °C. 350 HV. (a) Scanning electron
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Published: 01 August 1999
Fig. 8.15 Overheating: grain-boundary sulfide precipitation. 0.4% C, Ni-Cr-Mo alloy (0.40C-0.03Si-0.02P-1.8Ni-0.3Mo, wt%). (a) Heated for 1 h at 1325 °C, cooled at 750 °C/h, heated at 850 °C, oil quenched, tempered. Light macrograph of fracture surface. 5×. (b) Heated for 1 h at 1325 °C
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Published: 01 August 1999
Fig. 3 Schematic of grain boundary region in a 2 xxx alloy. Precipitation of the very high copper content precipitates on the boundary causes a copper-depleted zone on either side of the boundary. The difference in electrochemical potentials of the copper-depleted zone and the copper-rich
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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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Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 July 1997
DOI: 10.31399/asm.tb.wip.t65930329
EISBN: 978-1-62708-359-1
... alloys in terms of grain boundary precipitation, grain growth, and hot cracking in the heat-affected zone; fusion zone segregation and porosity; and postweld heat treatments. Next, the article analyzes the welding characteristics of dissimilar and clad materials. This is followed by sections summarizing...
Abstract
Nickel-base alloys are generally used in harsh environments that demand either corrosion resistance or high-temperature strength. This article first describes the general welding characteristics of nickel-base alloys. It then describes the weldability of solid-solution nickel-base alloys in terms of grain boundary precipitation, grain growth, and hot cracking in the heat-affected zone; fusion zone segregation and porosity; and postweld heat treatments. Next, the article analyzes the welding characteristics of dissimilar and clad materials. This is followed by sections summarizing the various types and general weldability of age-hardened nickel-base alloys. The article then discusses the composition, welding metallurgy, and properties of cast nickel-base superalloys. Finally, it provides information on the welding of dissimilar metals, filler metal selection for welding clad materials and for overlay cladding, service conditions during repair, and welding procedural idiosyncrasies of cobalt-base alloys.
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in Sintering and Corrosion Resistance
> Powder Metallurgy Stainless Steels: Processing, Microstructures, and Properties
Published: 01 June 2007
Fig. 5.46 Chromium nitride precipitates in 316L. (a) Sintered at 1150 °C (2100 °F) in dissociated ammonia; 4500 ppm N 2 ; Cr 2 N precipitates along grain boundaries (1) and within grains (2). (b) Sintered at 1120 °C (2050 °F) in dissociated ammonia and slowly cooled; 6500 ppm N 2 ; Cr 2 N
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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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Published: 01 June 2008
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Published: 01 November 2012
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Published: 01 December 2006
Fig. 2 Photomicrographs showing corrosion attack in alloy C-276 (UNS N10276) caused by grain boundary precipitation in the HAZ of the weld. The sample was taken from a pipe removed after 18 months of service in a hydrochloric acid vapor environment in a chemical plant. Sample was etched in HCl
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Published: 01 July 1997
Fig. 1 Photomicrographs showing corrosion attack in Hastelloy C-276 (UNS N10276) caused by grain boundary precipitation in the heat-affected zone of the weld. The sample was taken from a pipe removed after 18 months of service in a hydrochloric acid vapor environment in a chemical plant
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Published: 01 March 2002
Fig. 12.14 Micrographs of IN-718 nickel-base superalloy after receiving a high solution treatment at 1038 °C (1900 °F) for differing times. (a) 20 min at 1038 °C, showing presence of prior δ-phase grain boundary precipitates (arrows). 550×. (b) 1 h showing absence of prior δ phase particles
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Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 November 2010
DOI: 10.31399/asm.tb.sap.t53000017
EISBN: 978-1-62708-313-3
... of grain structure, as in columnar-grained alloys, or by the elimination of grain boundaries as with single-crystal superalloys. dispersion strengthening precipitation hardening solid-solution hardening superalloys SUPERALLOYS ARE STRENGTHENED through three principal mechanisms: solid...
Abstract
This chapter discusses the metallurgical changes that occur and the improvements that can be achieved in superalloys through solid-solution hardening, precipitation hardening, and dispersion strengthening. It also explains how further improvements can be achieved through the control of grain structure, as in columnar-grained alloys, or by the elimination of grain boundaries as with single-crystal superalloys.
Book Chapter
Book: Corrosion of Weldments
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2006
DOI: 10.31399/asm.tb.cw.t51820125
EISBN: 978-1-62708-339-3
... can occur during reheating, as in weld heat-affected zones (HAZs), typically as grain-boundary precipitates. Modern wrought alloys, with their very low carbon and silicon contents, are quite stable and can be used in the as-welded condition with only a low risk of intergranular attack. Older cast...
Abstract
Nickel-base alloys used for low-temperature aqueous corrosion are commonly referred to as corrosion-resistant alloys (CRAs), and nickel alloys used for high-temperature applications are known as heat-resistant alloys, high-temperature alloys, or superalloys. The emphasis in this chapter is on the CRAs and in particular nickel-chromium-molybdenum alloys. The chapter provides a basic understanding of general welding considerations and describes the welding metallurgy of molybdenum-containing CRAs and of nickel-copper, nickel-chromium, and nickel-chromium-iron CRAs. It discusses the corrosion behavior of nickel-molybdenum alloys and nickel-chromium-molybdenum alloys. Information on the phase stability and corrosion behavior of nickel-base alloys is also included.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 August 1999
DOI: 10.31399/asm.tb.lmcs.t66560185
EISBN: 978-1-62708-291-4
...- and fine-grained steels. The chapter also discusses grain-refinement processes and some of the effects of overheating, including sulfide spheroidization, grain-boundary sulfide precipitation, and grain-boundary liquation. austenitization carbon steel grain boundary grain growth grain size We...
Abstract
This chapter examines the structural changes that occur in high-carbon steels during austenitization. It describes the effect of heating time and temperature on the production of austenite and the associated transformation of ferrite and cementite in eutectoid, hypoeutectoid, and hypereutectoid steels. It discusses the factors that influence the kinetics of the process, including carbon diffusion and the morphology of the original structure. It describes the nucleation and growth of austenite grains, the effect of grain size on mechanical properties, and the difference between coarse- and fine-grained steels. The chapter also discusses grain-refinement processes and some of the effects of overheating, including sulfide spheroidization, grain-boundary sulfide precipitation, and grain-boundary liquation.
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2015
DOI: 10.31399/asm.tb.cpi2.t55030070
EISBN: 978-1-62708-282-2
... treated temper (T3 or T4). If quenched too slowly, the alloy can be highly susceptible to IG corrosion. When poorly quenched, large Al-Cu(-Mg) precipitates form along the grain boundary. This produces a copper-depleted-zone along the boundaries, and a galvanic couple is then established. The copper...
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 August 1999
DOI: 10.31399/asm.tb.caaa.t67870063
EISBN: 978-1-62708-299-0
... and 7 xxx alloys) and is often related to copper depleted regions or to anodic precipitates at the grain boundary region. Because corrosion is limited to the immediate grain boundary region, IGC is difficult to detect without the aid of a microscope. Intergranular corrosion penetrates more quickly than...
Abstract
This chapter describes the mechanisms, characteristics, and prevention of intergranular and exfoliation corrosion in various aluminum alloys. It discusses susceptible alloys and recommended tempers and presents several examples of exfoliation in aircraft components. It also explains how the two forms of corrosion are related to stress-corrosion cracking.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 March 2002
DOI: 10.31399/asm.tb.stg2.t61280211
EISBN: 978-1-62708-267-9
... Abstract This chapter examines the effect of heat treating and other processes on the microstructure-property relationships that occur in superalloys. It discusses precipitation and grain-boundary hardening and how they influence the phases, structures, and properties of various alloys...
Abstract
This chapter examines the effect of heat treating and other processes on the microstructure-property relationships that occur in superalloys. It discusses precipitation and grain-boundary hardening and how they influence the phases, structures, and properties of various alloys. It explains how the delta phase, which is used to control grain size in IN-718, improves strength and prevents stress-rupture embrittlement. It describes heat treatments for different product forms, discusses the effect of tramp elements on grain-boundary ductility, and explains how section size and test location influence measured properties. It also provides information and data on the physical and mechanical properties of superalloys, particularly tensile strength, creep-rupture, fatigue, and fracture, and discusses related factors such as directionality, porosity, orientation, elongation, and the effect of coating and welding processes.
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