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Published: 01 October 2011
Fig. 14.26 Effect of solution-treatment temperatures on microstructures of quenched and aged α alloy Ti-8Al-1Mo-1V. All specimens were solution annealed at indicated temperatures for 1 h, quenched in oil, stabilized at 580 °C (1075 °F) for 8 h and air cooled. (a) Fine α-β structure after β
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Published: 01 October 2011
Image
Published: 01 October 2011
Fig. 14.28 Effect of solution treatment on tensile properties of Ti-6Al-4V. (a) Tensile properties after solution treatment. (b) Tensile properties after solution treatment and aging. Source: Ref 14.10
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Image
Published: 01 March 2002
Fig. 12.7 Influence of solution heat treatment temperature on rupture life of Nimonic 80A nickel-base superalloy at 234 MPa (34 ksi) and 750 °C (1380 °F), showing effect of 1000 °C (1832 °F) intermediate heat treatment before aging. Open datapoints are SHT for 4 h. Cool to IHT and IHT for 16 h
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Published: 01 March 2002
Fig. 12.11 Effect of solution heat treatment and aging on X-40 (HA-31) cobalt-base superalloy showing increase in strength resulting from carbide precipitation
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in Heat Treatment of Aluminum Castings
> Aluminum Alloy Castings: Properties, Processes, and Applications
Published: 01 December 2004
Fig. 7.5 Characteristic residual stress distribution after solution heat treatment and quench. t , thickness
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Image
Published: 30 June 2023
Fig. 5.16 Solution heat treatment. (a) Batch vertical SHT furnace. (b) Load about to enter quench tank
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Image
Published: 01 December 2000
Fig. 6.11 Comparison of smooth axial fatigue behavior of Ti-6Al-4V investment castings subjected to various heat treatments (see Table 6.1 ). BUS, broken-up structure; HTH, high-temperature hydrogenation; BST, beta solution treatment; ABST, alpha-beta solution treatment; CST, constitutional
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Image
Published: 01 October 2012
Fig. 5.16 Schematic diagram of a conventional forging and subsequent heat treatment sequence for producing an α-β structure. Typical temperatures during processing would be 955 °C (1750 °F) for the forging and solution treatment, 730 °C (1350 °F) for annealing, and 540 °C (1000 °F) for aging
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Image
Published: 01 June 2008
Fig. 28.11 Typical thermomechanical processing sequence for alpha-beta titanium forgings. Typical temperatures during processing would be 955 °C (1750 °F) for the forging and solution treatment, 730 °C (1350 °F) for annealing, and 540 °C (1000 °F) for aging. Typical times during processing
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in Comparing the Microstructure of Components Prepared by Various Powder Metallurgy and Casting Methods
> Powder Metallurgy and Additive Manufacturing: Fundamentals and Advancements
Published: 30 September 2024
Fig. 7.13 Microstructures of Ti-5Fe alloy after (a) sintering, (b) extrusion at 900 °C (1650 °F), (c) extrusion at 850 °C (1560 °F), (d) extrusion at 800 °C (1470 °F), (e) after solution treatment and aging at 550 °C (1020 °F) for 4 h, and (f) after solution treatment and aging at 650 °C (1200
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Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 March 2002
DOI: 10.31399/asm.tb.stg2.t61280135
EISBN: 978-1-62708-267-9
... such changes are required. It describes several types of treatments, including stress relieving, in-process annealing, full annealing, solution annealing, coating diffusion, and precipitation hardening. It discusses the temperatures, holding times, and heating and cooling rates necessary to achieve the desired...
Abstract
All superalloys, whether precipitation hardened or not, are heated at some point in their production for a subsequent processing step or, as needed, to alter their microstructure. This chapter discusses the changes that occur in superalloys during heat treatment and the many reasons such changes are required. It describes several types of treatments, including stress relieving, in-process annealing, full annealing, solution annealing, coating diffusion, and precipitation hardening. It discusses the temperatures, holding times, and heating and cooling rates necessary to achieve the desired objectives of quenching, annealing, and aging along with the associated risks of surface damage caused by oxidation, carbon pickup, alloy depletion, intergranular attack, and environmental contaminants. It also discusses heat treatment atmospheres, furnace and fixturing requirements, and practical considerations, including heating and cooling rates for wrought and cast superalloys and combined treatments such as solution annealing and vacuum brazing.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2000
DOI: 10.31399/asm.tb.ttg2.t61120039
EISBN: 978-1-62708-269-3
.... However, because HIP itself is a heat treatment and, in turn, is usually followed by a high-temperature solution treatment at or above the HIP temperature, stress relief may not have any significant effect on final mechanical properties of hot isostatically pressed titanium castings. Heat treatment after...
Abstract
Titanium castings are used in a wide range of aerospace, chemical process, marine, biomedical, and automotive applications. This chapter provides an overview of titanium casting and associated processes and how they compare with other manufacturing methods. It also discusses the role heat treating and its effect on the tensile properties of different titanium alloys.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2000
DOI: 10.31399/asm.tb.ttg2.t61120055
EISBN: 978-1-62708-269-3
... (annealing) To increase strength by solution treatment and aging To optimize special properties, such as fracture toughness, fatigue strength, and high-temperature creep strength Various types of annealing treatments (e.g., single, duplex, mill, beta, and recrystallization) and solution treating...
Abstract
This chapter discusses the effect of heat treating on titanium alloys and the influence of time and temperature on critical properties and behaviors. It explains how heat treatments are used to make titanium stronger, tougher, more ductile, and easier to machine as well as more resistant to the effects of corrosion and thermal and mechanical fatigue. It describes accepted practices for stress relieving, aging, annealing, and post-treatment processing along with associated challenges and concerns.
Image
Published: 01 March 2006
Fig. 3 Part of the aluminum-copper phase diagram. The kappa phase, bounded by ABC, is a solid solution of copper in aluminum; CuAl 2 precipitates from this phase on slow cooling or on aging after solution treatment. Source: Ref 5
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Series: ASM Technical Books
Publisher: ASM International
Published: 01 January 2015
DOI: 10.31399/asm.tb.tpmpa.t54480075
EISBN: 978-1-62708-318-8
... (a) Quenched from above beta transus. (b) Beta phase is mechanically unstable and can transform to martensite with application of stress. Also, a thermal omega may be present. When referring to beta phase stability, note that if the solution treatment is carried out below the beta transus...
Abstract
Titanium alloys respond well to heat treatment be it to increase strength (age hardening), reduce residual stresses, or minimize tradeoffs in ductility, machinability, and dimensional and structural stability (annealing). This chapter describes the phase transformations associated with these processes, explaining how and why they occur and how they are typically controlled. It makes extensive use of phase diagrams and cooling curves to illustrate the effects of alloying and quenching on beta-to-alpha transformations and the conditions that produce metastable phases. It also examines several time-temperature-transformation diagrams, which account for the effect of cooling rate.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 October 2011
DOI: 10.31399/asm.tb.mnm2.t53060333
EISBN: 978-1-62708-261-7
... that can be hardened by heat treatment. Some of the common nonferrous alloys that can be hardened through heat treatment include: Solution-treated and aged aluminum alloys (e.g., aluminum-copper alloys) Solution-treated and aged cobalt alloys Solution-treated copper alloys (such as beryllium...
Abstract
Nonferrous alloys are heat treated for a variety of reasons. Heat treating can reduce internal stresses, redistribute alloying elements, promote grain formation and growth, produce new phases, and alter surface chemistry. This chapter describes heat treatment processes and how nonferrous alloys respond to them. It provides information on aluminum, cobalt, copper, magnesium, nickel, and titanium alloys and their composition, microstructure, properties, and processing characteristics.
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in Melting, Casting, and Powder Metallurgy[1]
> Titanium: Physical Metallurgy, Processing, and Applications
Published: 01 January 2015
Fig. 8.14 Cast Ti-6Al-4V broken-up structure, the result of a 1025 °C (1880 °F) solution treatment followed by an 815 °C (1500 °F) aging for 24 h. B, grain-boundary alpha
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Image
Published: 01 March 2006
Fig. 5 Beryllium-copper phase diagram. The alpha phase holds about 1.55% Be at 605 °C (1121 °F) and about 2.7% at 865 °C (1590 °F). Decreasing solubility of the beryllium causes precipitation of a hard beryllium-copper phase on slow cooling or on aging after solution treatment. Source: Ref 4
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Image
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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