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Solution annealing

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Published: 01 January 2017
Fig. 4.12 Effect of applied stress on the time to failure of solution-annealed and electropolished type 347 tested in a magnesium chloride solution boiling at 145 °C (293 °F). After Ref 4.42 More
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Published: 01 January 2017
Fig. 5.25 Effect of chromium content on the time to failure of solution-annealed Ni-Cr-Fe alloys tested in H 3 BO 3 + LiOH solutions containing hydrogen at 360 °C (680 °F). Source: Ref 5.103 More
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Published: 01 December 1984
Figure 3-40 Microstructure of solution-annealed Hadfield Mn austenitic steel. More
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Published: 01 December 1984
Figure 3-50 AISI 316 austenitic stainless steel (solution-annealed), 75×. More
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Published: 01 December 1984
Figure 3-62 Microstructure of nickel-based superalloys (solution-annealed and aged) Pyromet 31 (left) and Pyromet X-750 (right) revealed using Kalling’s no. 2 (top) and using Beraha’s tint etch (bottom), 60×. More
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Published: 01 December 1995
Fig. 20-24 Isocorrosion diagrams for solution-annealed and quenched ACI CN-7M in H 2 SO 4 , HNO 3 , NaOH, and H 3 PO 4 . (a), (b), (d), and (f) Tested at atmospheric pressure. (c) and (e) Tested at equilibrium pressure in a closed container. See Fig. 20-22 for legend. More
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Published: 01 July 1997
Fig. 9 Effect of heating rate on the cracking tendency of solution-annealed (before welding) René 41 during postweld heat treatment. Source: Ref 15 More
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...
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
... , 1972 , p 157 – 192 Fig. D.1 Laves phase (white islands) has precipitated at dendrites in the gamma matrix. Optical microscope, original magnification 250x. Condition: Solution treated and aged—solution annealed 1 h at 1095 °C (2000 °F), air cooled, reannealed 1 h at 980 °C (1800 °F), air...
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Published: 01 November 2010
Fig. 5.8 Secondary ion mass spectroscopy images showing boron (B) and carbon (C) concentration in boron-modified alloy 690. (a) Solution annealed. (b) Solution annealed + 700 °C (1290 °F)/1 h. (c) Solution annealed + 700 °C (1290 °F)/100 h. Source: Ref 42 More
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Published: 01 December 2006
Fig. 3 Solidification morphologies of fusion welded alloy 2205. (a) As-welded base metal. (b) As-welded composite region. (c) As-welded weld metal. (d) Postweld heat treated solution-annealed base metal. (e) Solution annealed composite region. (f) Solution annealed weld metal. Source: Ref 2 More
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Published: 01 December 1984
Figure 3-34 Microstructure of beryllium-copper alloy revealed by swabbing with aqueous 3% ammonium persulfate and 1% ammonium hydroxide. Left, solution-annealed, twins not attacked [70 HRB (Rockwell hardness on the B scale), 300×]; right, solution-annealed and aged [41 HRC (Rockwell hardness More
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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 More
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Published: 01 January 2017
Fig. 4.23 Relationship among applied potential, applied stress, and time to failure of solution-annealed type 304 in a 42% MgCl 2 solution at 144 °C (291 °F). After Ref 4.71 More
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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 More
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Published: 01 November 2010
Fig. D.16 Structure is precipitates of M6C and “Co2W” intermetallic in a face-centered cubic matrix. Optical microscope, original magnification 500×. Condition: Solution treated and aged—solution annealed at 1205 °C (2200 °F) and aged 3400 h at 870 °C (1600 °F). Source: Ref 1 , 2 More
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Published: 01 January 2015
Fig. 6.16 Typical S-N curves for annealed (Ann.) and solution-treated and aged (STA) Ti-6Al-4V bar. K t , theoretical stress-concentration factor More
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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 More
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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 More
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Published: 01 November 2010
Fig. D.5 Structure is delta phase (Ni3Nb) in a gamma matrix. Optical microscope, original magnification 1000×. 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 cooled in 10 h to 620 °C (1150 °F). Source More