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aluminum alloy
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Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 July 1997
DOI: 10.31399/asm.tb.wip.t65930283
EISBN: 978-1-62708-359-1
... Abstract This article reviews weldability of aluminum alloys and factors that affect weld performance. It first addresses hot tears, which can form during the welding of various aluminum alloys. It then presents comparison data from different weldability tests and discusses the specific...
Abstract
This article reviews weldability of aluminum alloys and factors that affect weld performance. It first addresses hot tears, which can form during the welding of various aluminum alloys. It then presents comparison data from different weldability tests and discusses the specific properties that affect welding, namely oxide characteristics; the solubility of hydrogen in molten aluminum; and its thermal, electrical, and nonmagnetic characteristics. The article addresses the primary factors commonly considered when selecting a welding filler alloy, namely ease of welding or freedom from cracking, tensile or shear strength of the weld, weld ductility, service temperature, corrosion resistance, and color match between the weld and base alloy after anodizing. A number of factors, both global and local, that influence the fatigue performance of welded aluminum joints are also covered.
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2004
DOI: 10.31399/asm.tb.aacppa.9781627083355
EISBN: 978-1-62708-335-5
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Published: 01 October 2012
Fig. 1.5 Aluminum alloy cast products. (a) Aluminum alloy 380.0 gearbox casting for passenger car. (b) Aluminum alloy 380.0 rear axle casting. Source: Ref 1.1
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Published: 01 December 2006
Fig. 2.10 Large section in the aluminum alloy AlMgSi0.7 for aluminum carriages for the San Francisco Metro using large section welded technology on the runout table of the 98,000 kN direct extrusion press at Alusuisse Singen. Source: Alusuisse
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in Corrosion of Welded, Brazed, Soldered, and Adhesive-Bonded Joints
> Corrosion of Aluminum and Aluminum Alloys
Published: 01 August 1999
Fig. 2 Welded assemblies of aluminum alloy 7005 with alloy 5356 filler metal after a one-year exposure to seawater. (a) As-welded assembly shows severe localized corrosion in the HAZ. (b) Specimen showing the beneficial effects of postweld aging. Corrosion potentials of different areas
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Published: 01 December 2006
Fig. 2 Welded assemblies of aluminum alloy 7005 with alloy 5356 filler metal after a one-year exposure to seawater. (a) As-welded assembly shows severe localized corrosion in the HAZ. (b) Specimen showing the beneficial effects of postweld aging. Corrosion potentials of different areas
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Published: 01 October 2012
Fig. 12.8 Applications for aluminum alloy castings. (a) Alloy 319 automotive cylinder head. (b) Alloy 380 automotive transmission case. Source: Ref 12.16
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Published: 01 December 2015
Fig. 3 Welded assemblies of aluminum alloy 7005 with alloy 5356 filler metal after a 1 year exposure to seawater. (a) As-welded assembly shows severe localized corrosion in the HAZ. (b) Specimen showing the beneficial effects of postweld aging. Corrosion potentials of different areas
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in The Art of Revealing Microstructure
> Metallographer’s Guide: Practices and Procedures for Irons and Steels
Published: 01 March 2002
Fig. 8.50 The dendritic structure of a zinc-aluminum alloy spangle (Galvalume) on a steel wire. Specimen etched by suspending over fuming nitric acid. 200×
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Published: 30 November 2013
Fig. 9 Fatigue fracture in aluminum alloy 2024-T3 tested first in vacuum (region A) and then in air (region B) (7500×). The arrow at the lower right indicates the direction of crack propagation. Note the flat, featureless fracture surface formed while testing in vacuum (region
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Published: 01 September 2008
Fig. 14 Fatigue striations in (a) interstitial-free steel and (b) aluminum alloy AA2024-T42. (c) Fatigue fracture surface of a cast aluminum alloy where a fatigue crack was nucleated from a casting defect, presenting solidification dendrites on the surface. Arrow at top right indicates fatigue
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in Evaluation of Stress-Corrosion Cracking[1]
> Stress-Corrosion Cracking: Materials Performance and Evaluation
Published: 01 January 2017
Fig. 17.16 Effect of temper on SCC performance of aluminum alloy 7075 subjected to alternate immersion in 3.5% NaCl solution at a stress of 207 MPa (30 ksi). Mean flaw depth was calculated from the average breaking strength of five specimens subjected to identical conditions. Source: Ref
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in Evaluation of Stress-Corrosion Cracking[1]
> Stress-Corrosion Cracking: Materials Performance and Evaluation
Published: 01 January 2017
Fig. 17.42 Anodic polarization curves for aluminum alloy 7075-T651 in deaerated 3.5% NaCl solution showing the domains of behavior predicted from the curve. Source: Ref 17.73
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in Evaluation of Stress-Corrosion Cracking[1]
> Stress-Corrosion Cracking: Materials Performance and Evaluation
Published: 01 January 2017
Fig. 17.54 Stress-corrosion cracking propagation rates for various aluminum alloy 7050 products. Double-beam specimens (S-L; see Fig. 17.29 ) bolt-loaded to pop-in and wetted three times daily with 3.5% NaCl. Plateau velocity averaged over 15 days. The right-hand end of the band for each
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in Failure Analysis of Stress-Corrosion Cracking[1]
> Stress-Corrosion Cracking: Materials Performance and Evaluation
Published: 01 January 2017
Fig. 18.23 Aluminum alloy 2014-T6 hinge bracket that failed by SCC in service. (a) Hinge bracket. Arrow indicates crack. (b) Micrograph showing secondary cracking adjacent and parallel to the fracture surface. Keller’s reagent. Original magnification: 250×. Source: Ref 18.21
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Published: 01 October 2011
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in Cold Spray Applications in the Automotive Industry
> High Pressure Cold Spray: Principles and Applications
Published: 01 June 2016
Fig. 8.12 Sequence of wear-resistant coating on aluminum alloy engine block. Reproduced by permission of Oerlikon Metco. Source: Ref 8.49
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in Cold Spray Applications in Repair and Refurbishment for the Aerospace, Oil and Gas, and Power-Generation Industries
> High Pressure Cold Spray: Principles and Applications
Published: 01 June 2016
Fig. 11.10 (a) Crack in electron-beam-welded aluminum alloy Al-6061 (right: weld metal; left: parent metal). (b) Crack-free electron beam weld in Al-6082 alloy made with cold-sprayed buttering layer using Al-4041 alloy. Source: Ref 11.15 . Courtesy of TWI Ltd.
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Published: 01 August 2005
Fig. 20 Fracture surfaces of an aluminum alloy lug. Fractures originated by SCC on the surface of a diametrical hole, at A and B. The crack was then propagated by fatigue, as evidenced by the presence of beach marks at C
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Published: 01 January 2000