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6061-T6
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Image
Published: 01 August 1999
Image
Published: 01 August 1999
Fig. 6 Corrosion (a) of aluminum alloy 6061-T6 aircraft fuel line (arrow). (b) Close-up of corrosion on fuel line. Note pitting and corrosion products. (c) Intergranular corrosion of the fuel line at area A from (a)
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Image
in Erosion, Cavitation, Impingement, and Fretting Corrosion
> Corrosion of Aluminum and Aluminum Alloys
Published: 01 August 1999
Fig. 4 Aluminum alloy 6061-T6 combustion chamber damaged by cavitation erosion. The chamber rotated in water at moderate speed. (a) Overall view of the chamber. (b) and (c) Micrographs of cross sections of the chamber wall showing typical cavitation damage. 100 and 500×, respectively
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Image
Published: 30 June 2023
Image
Published: 30 June 2023
Image
Published: 01 July 1997
Fig. 10 Hardness profiles of the HAZ for 6061-T4 and T6 starting materials in the as-welded (AW) and postweld (PWA) conditions. Source: Ref 15
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Published: 01 August 1999
Fig. 6 Average weight losses for seven aluminum alloys exposed at each of five test sites. Alloys combined were 1199-H14, 2024-T3, 5154-H34, 5357-H34, 6061-T6, Alclad 3003-H14, and Alclad 6061-T6. Source: Ref 8
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in Mechanical Properties Data for Selected Aluminum Alloys
> Mechanics and Mechanisms of Fracture: An Introduction
Published: 01 August 2005
Fig. A7.8 S-N curves for three aluminum alloys, R = 0.1. Curves A and B: 7033-T6; curves C and D: 2014-T6; curves E and F: 6061-T6. Source: Ref A7.10
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Image
Published: 30 June 2023
Fig. 8.6 Hollow cores forgings (a) as-forged and (b) after machining and assembly of 6061-T6 electrical power grid test load cells. Courtesy of Scot Forge
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Image
Published: 30 June 2023
Fig. 10.16 Anodizing. (a) Growth of aluminum oxide surface layer due to anodizing process. (b) SEM photomicrograph of anodized surface layer on 6061-T6 aluminum sheet. Source: Alcoa
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Image
Published: 01 June 2016
Fig. 3.8 Initial configuration (left) and the simulation results (a–f) showing the impact morphology and the evolution of the oxide film on an Al 6061-T6 particle during impact onto a substrate of the same material at a velocity of 700 m/s (2300 ft/s). Source: Ref 3.37
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Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 August 1999
DOI: 10.31399/asm.tb.caaa.t67870135
EISBN: 978-1-62708-299-0
...-H14, 2024-T3, 5154-H34, 5357-H34, 6061-T6, Alclad 3003-H14, and Alclad 6061-T6. Source: Ref 8 Fig. 7 Comparison of the loss in tensile strength calculated from weight loss with that of actual determinations of tensile strength for several aluminum alloys exposed 20 years to the atmospheres...
Abstract
Aluminum products are used extensively in natural atmospheres and in and around water. They are also widely used in building materials and as containers for chemicals and food and beverage products. This chapter discusses the corrosion mechanisms associated with these environments and the influence of various factors and prevention methods. It also includes an extensive amount of data of corrosion rates, corrosion resistance, and changes in mechanical properties.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 August 1999
DOI: 10.31399/asm.tb.caaa.t67870063
EISBN: 978-1-62708-299-0
... environments as described in the following example. Example 1: Aircraft Fuel Line IGC Inspections revealed fuel line corrosion beneath ferrules ( Fig. 6 ). The cause of the corrosion was traced to the fuel line marking process, which involved electrolytic labeling of ferruled aluminum alloy 6061-T6...
Abstract
This chapter describes the mechanisms, characteristics, and prevention of intergranular and exfoliation corrosion in various aluminum alloys. It discusses susceptible alloys and recommended tempers and presents several examples of exfoliation in aircraft components. It also explains how the two forms of corrosion are related to stress-corrosion cracking.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 30 June 2023
DOI: 10.31399/asm.tb.atia.t59340165
EISBN: 978-1-62708-427-7
... with the circumference of the part ( Ref 8.5 ). Fig. 8.6 Hollow cores forgings (a) as-forged and (b) after machining and assembly of 6061-T6 electrical power grid test load cells. Courtesy of Scot Forge Forging Equipment Hammers are a relatively low-cost method for production of closed- or open-die...
Abstract
Forged aluminum products vary widely in their production methods and applications. The forging process allows for control of microstructure and directional properties, and their fatigue and fracture resistance are superior to shape castings. This chapter presents the types, equipment, process steps, alloys, and products of aluminum forging.
Series: ASM Technical Books
Publisher: ASM International
Published: 01 August 2005
DOI: 10.31399/asm.tb.mmfi.t69540397
EISBN: 978-1-62708-309-6
...) 6061–T651 289 41.9 Bend T-L 29.1 26.5 41.6 37.9 … … … … 7039–T6 381 55.3 Bend T-L 32.3 29.4 33.5 30.5 … … … … 7075–T651 536 77.7 Bend T-L 22.5 20.5 27.6 25.1 … … … … 7075–T7351 403 58.5 Bend T-L 35.9 32.7 32.1 29.2 … … … … 7075–T7351 392...
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
... (b) 228 (b) 33 (b) 2 (b) 12 (b) 6009-T4 4043 221 32 138 20 9 … 303 (b) 44 (b) … … … … 6061-T6 4043 186 27 124 18 8 16 303 (c) 44 (c) 276 (c) 40 (c) 5 (c) 11 (c) 6061-T6 5356 207 30 131 19 11 25 … … … … … 6061-T4 4043 186 27 124...
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.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 30 June 2023
DOI: 10.31399/asm.tb.atia.t59340303
EISBN: 978-1-62708-427-7
... of the truck. Floors and side rails of U.S. dry vans are typically 6061-T6 or 6005A-T6 extrusions, while in Europe, alloy 6082-T6 is preferred for similar parts. Sheets are attached to an extruded frame with vertical and longitudinal members to support the side panels. Special fasteners often are used...
Image
Published: 01 October 2012
) Young’s modulus as a function of SiC w and SiC p volume fraction. (d) Thermal conductivity for 2009/SiC/ xx -T6. (e) Electrical conductivity for 2009/SiC/ xx p-T6 and 6061/SiC/ xx p-T6. (f) Coefficient of thermal expansion (CTE) for 6061/SiC/ xx p-T6. Source: Ref 9.5
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Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 30 June 2023
DOI: 10.31399/asm.tb.atia.t59340143
EISBN: 978-1-62708-427-7
... higher strength compared to 6061 and 6262 ( Ref 7.8 ). It contains higher copper to increase the strengthening potential and a zinc addition to improve corrosion resistance. The alloy is produced as T6 and T8 rod and bar for automotive and small engine parts and sports products such as fly reels. One...
Abstract
Aluminum shapes, rod, bar, tubes, and wire may be produced directly as extrusions or by subsequent processing of continuous cast stock. This chapter describes the key aspects of aluminum extrusion and wire production focusing on the more common hot extrusion process and presenting the general types of aluminum extrusion alloys. An overview of free-machining alloys and products, and weldable 6xxx and 7xxx high-strength structural alloys is also provided.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2004
DOI: 10.31399/asm.tb.aacppa.t51140069
EISBN: 978-1-62708-335-5
...) F 0.096 2.70 2.70 12.8 22.6 970–1160 520–630 1155 168 54 177 31 103 19 0.032 0.210 879 0.33 201.0 (d) T6 0.101 2.80 2.80 10.7 19.3 1060–1200 570–650 840 121 30 99 17 57 35 0.057 0.220 922 0.33 T7 0.101 2.80 2.80 10.7 19.3 1060–1200 570–650 840 121...
Abstract
This chapter reviews and provides data tables for the wide range of properties and performance characteristics that are possible with specific aluminum casting alloys and tempers. Properties and performance attributes addressed include casting and finishing characteristics; typical physical properties; typical and minimum (design) mechanical properties; fatigue strength; fracture resistance, including subcritical crack growth; and resistance to general corrosion and to stress-corrosion cracking. The chapter concludes with information on the properties of cast aluminum matrix composites.
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