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Series: ASM Handbook
Volume: 4A
Publisher: ASM International
Published: 01 August 2013
DOI: 10.31399/asm.hb.v04a.a0005782
EISBN: 978-1-62708-165-8
... Abstract Stress-relief heat treating of steel is the uniform heating of a structure to a suitable temperature below the transformation range, holding at this temperature for a predetermined period of time, followed by uniform cooling. This article provides information on the sources of residual...
Series: ASM Handbook
Volume: 22B
Publisher: ASM International
Published: 01 November 2010
DOI: 10.31399/asm.hb.v22b.a0005506
EISBN: 978-1-62708-197-9
... and trivial loading and boundary conditions. The article discusses approximate and advanced solution techniques that can be employed in practice for simulation of residual stress relief: finite-difference method and finite-element method. It also describes advanced techniques applicable to transient creep...
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Published: 01 August 2013
Fig. 3 Residual stress as a function of stress-relief annealing temperature and time for HY-100 steel. Source: Ref 16 More
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Published: 01 October 2014
Fig. 5 Effect of stress-relieving time and temperature on degree of stress relief obtained in low-alloy gray irons. Table shows compositions and negligible effect of maximum stress-relieving conditions on hardness. Iron Composition, % Hardness, HRB C Si P S Mn Ni Cr Mo Cu More
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Published: 31 August 2017
Fig. 5 Effect of stress-relieving time and temperature on degree of stress relief obtained in low-alloy gray irons. Table shows compositions and negligible effect of maximum stress-relieving conditions on hardness. More
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Published: 01 August 2013
Fig. 4 Stress-relief data of a steel plotted versus the Larson-Miller equation ( Eq 1 ). Source: Ref 16 More
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Published: 01 August 2013
Fig. 7 Effect of temperature on 1 h stress relief of 2 mm (0.080 in.) diameter spring wire. (a) Hard-drawn carbon wire. (b) Music wire. Source: Ref 21 More
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Published: 01 August 2013
Fig. 8 Effect of stress-relief time at two temperatures for 2 mm (0.080 in.) diameter hard-drawn carbon wire. At these temperatures, the bulk of stress relief occurs after 20–30 min. ce: Ref 21 More
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Published: 01 January 1990
Fig. 19 Stress relief of gray iron at various temperatures. Source: Ref 17 More
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Published: 01 August 2013
Fig. 37 Plot of stress relief versus tempering temperatures held for 1 h for two surface carbon concentration levels in austenite. Source: Ref 68 More
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Published: 01 January 2006
Fig. 3 Temperature and concentrations of caustic soda that require stress relief to prevent SCC of carbon steel. Source: Ref 22 More
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Published: 01 December 2008
Fig. 23 Stress relief of gray iron at various temperatures. Source: Ref 30 More
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Published: 01 January 1996
Fig. 9 Effect of stress relief on fatigue strength of 5456-H3221 longitudinal butt welds. Source: Ref 23 More
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Published: 01 June 2016
Fig. 18 Residual stresses. Stress-relief behavior strongly depends on alloy composition, as evident from the curves for unalloyed titanium and two alloys. The effect of stress-relief time and temperature on the percent of remaining original residual stresses is illustrated. More
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Published: 01 June 2016
Fig. 10 Relationship between time and stress relief at various temperatures for Ti-6Al-4V. Source: Ref 1 More
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Published: 31 October 2011
Fig. 14 Effect of temperature and time on stress relief. Time and temperature, 4 h More
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Published: 01 October 2014
Fig. 7 Stress relief obtained in type 347 stainless steel, as a function of temperature, initial stress, and time at temperature More
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Published: 01 October 2014
Fig. 25 Stress relief obtained in ductile iron held at three temperatures for 1 2 to 8 h. Initial hardness was 102 to 103 HRB. Hardness after holding at 540, 595, and 650 °C (1000, 1100, and 1200 °F) for 8 h was 102 to 104, 101 to 103, and 90 to 93 HRB. More
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Published: 01 January 1987
Fig. 108 Stress-relief crack in plate steel Lehigh restraint sample. The crack is intergranular, but the high restraint level suppresses crack branching. The square marks in the weld HAZ in (a) are hardness impressions. (a) 9×. (b) Etched with 2% nital. 74× More
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Published: 01 January 2002
Fig. 28 Large welded tube that cracked upon postweld stress-relief heat treatment ( example 12 ) More