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residual stresses
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Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 30 November 2013
DOI: 10.31399/asm.tb.uhcf3.t53630035
EISBN: 978-1-62708-270-9
... Abstract Residual, or locked-in internal, stresses are regions of misfit within a metal part or assembly that can cause distortion and fracture just as can the more obvious applied, or service, stresses. This chapter describes the fundamental facts about residual stresses and discusses...
Abstract
Residual, or locked-in internal, stresses are regions of misfit within a metal part or assembly that can cause distortion and fracture just as can the more obvious applied, or service, stresses. This chapter describes the fundamental facts about residual stresses and discusses the basic mechanisms of residual stress formation: thermal, transformational, mechanical, and chemical.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 January 2015
DOI: 10.31399/asm.tb.spsp2.t54410487
EISBN: 978-1-62708-265-5
... Temperature and deformation gradients developed in the course of manufacturing can have undesired effects on the microstructures along their path; the two most common being residual stress and distortion. This chapter discusses these manufacturing-related problems and how they can be minimized...
Abstract
Temperature and deformation gradients developed in the course of manufacturing can have undesired effects on the microstructures along their path; the two most common being residual stress and distortion. This chapter discusses these manufacturing-related problems and how they can be minimized by heat treatments. It also provides information on residual stress evaluation and prediction techniques.
Series: ASM Technical Books
Publisher: ASM International
Published: 01 June 2022
DOI: 10.31399/asm.tb.tstap.t56040084
EISBN: 978-1-62708-428-4
... Abstract This article, prepared under the auspices of the ASM Thermal Spray Society Committees on Accepted Practices, describes a procedure for evaluating residual stresses in thermal spray coatings, which is an extension of the well-known layer removal method to include the Young’s modulus...
Abstract
This article, prepared under the auspices of the ASM Thermal Spray Society Committees on Accepted Practices, describes a procedure for evaluating residual stresses in thermal spray coatings, which is an extension of the well-known layer removal method to include the Young’s modulus and Poisson’s ratio properties of the thermal spray coating material and the substrate. It presents questions and answers that were selected to introduce residual stresses in thermal spray coatings. The article describes equipment and the laboratory procedure for the modified layer removal method and provides the description of the residual stress specimen. It also describes the procedures for applying or installing bonded resistance strain gages, the dimensions of the test specimen, the procedure for removing layers, and the method for interpreting the data to evaluate residual stresses. The spreadsheet program, “ MLRM for Residual Stresses ,” is available as a supplement to this document.
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Published: 01 December 2006
Fig. 10 Peak axial residual stresses on the inside surface of welded type 304 stainless steel pipes. Source: Ref 19
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Published: 01 December 2006
Fig. 11 Through-wall distribution of weld residual stresses in a 660 mm (26 in.) diam type 304 stainless steel pipe. Source: Ref 22
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Published: 01 December 2006
Fig. 6 SCC test specimen containing residual stresses from welding. (a) Sandwich specimen simulating rigid structure. Note SCC in edges of center plate. Source Ref 23 . (b) Cracked ring-welded specimen. Source: Ref 24
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Published: 01 December 1999
Fig. 6.36 Effect of fatigue stressing on the tangential residual stresses in 18 mm diam case-hardened fatigue test pieces. Source: Ref 40
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Published: 01 December 1999
Fig. 7.11 Residual stresses (tangential) in cyanide-hardened 40Kh rings before and after tempering (for 1.5 h). Ring dimensions: 80 mm outside diam × 66 mm inside diam × 15 mm high. Case depth 0.22 mm (on outside diam only). Source: Ref 22
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Published: 01 December 1999
Fig. 7.32 Residual stresses in the carbonitrided case of EX55 (a) without subzero treatment and (b) with subzero treatment. Source: Ref 50
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Published: 01 December 1999
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Published: 01 December 1999
Fig. 7.34 Residual stresses in the carburized case of SAE 9310 before and after subzero treatments. Source: Ref 52
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Published: 01 December 1999
Fig. 8.9(a) Residual stresses in SAE 4340 steel (quenched and tempered, 50 HRC) after grinding with CBN and diamond. Source: Ref 14 Conventional grind Diamond RVG-W Borazon II Wheel speed, ft/min 6000 6000 Down feed, in./pass 0.001 0.001 Grinding fluid Soluble oil
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Published: 01 December 1999
Fig. 8.9(b) Residual stresses in SAE 4340 steel (quenched and tempered, 50 HRC) after grinding with alumina. Source: Ref 14 Gentle Conventional Abusive Wheel A46HV A46KV A46MV Wheel speed, ft/min 2000 6000 6000 Down feed, in./pass Low-stress grinding 0.001 0.002
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Published: 01 December 1999
Fig. 8.33 Influence of shot peening on (a) residual stresses within austenite and martensite of a case-hardened surface and (b) fatigue strength. Table shows influence of shot peening on impact fracture stress. Source: Ref 38 Steel Condition Surface hardness (a) , HRC Core hardness
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Published: 01 December 1999
Fig. 8.37 Residual stresses in (a) CBN ground and (b) ground and shot peened surfaces for 9310 steel, 10 in. dp. Source: Ref 8
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Published: 01 August 2015
Fig. 5.24 Complex pattern of residual stresses forms in a carbon steel cylinder after induction heating and spray quenching. One of the goals of tempering is to relieve the subsurface tensile stresses that can cause cracking in service. Surface compressive stresses are beneficial. Stresses
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Published: 01 December 1999
Fig. 1.19 Residual stresses at the base of the teeth in carburized and carbonitrided gears. Source: Ref 28
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Published: 01 December 1999
Fig. 2.15 Effect of decarburization on the residual stresses developed in carburized and hardened plates. The carbon content at 0.002 mm was estimated to be 1% (curve 1), 0.64% (curve 2), and 0.35% (curve 3). Source: Ref 9
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Published: 01 December 1999
Fig. 3.26 The loss of surface compressive residual stresses due to the presence of a highly developed carbide zone in 20KhNV4MF steel. Source: Ref 41
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Published: 01 September 2005
Fig. 22 Ranges and patterns of residual stresses as a function of depth for 70 carburized steels. Source: Ref 49
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