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2014-T6
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Published: 01 November 2012
Fig. 30 Comparison of fatigue strength bands for 2014-T6, 2024-T4, and 7075-T6 aluminum alloys for rotating beam tests. Source: Ref 16
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Image
Published: 01 August 1999
Fig. 2 Pitting corrosion of an aluminum alloy 2014–T6 sheet. Pitting occurred during the manufacturing cycle. Note the intergranular nature of the pit. 150×
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Image
Published: 01 August 1999
Fig. 29 Aluminum alloy 2014-T6 aircraft nose wheel (a) that failed at the flange. (b) Close-up of tube well on wheel 31. (c) Appearance of flange failure on wheel 67. The topography is typical of other flange failures. (d) Close-up of wheel 31; note indentation (arrow). (e) Close-up of wheel
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Image
Published: 01 August 2005
Fig. 3.22 Forged aluminum alloy 2014-T6 aircraft component that failed by fatigue. Characteristic beach marks are evident. See also Fig. 3.23
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Image
Published: 01 August 2005
Fig. 3.40 Comparison of smooth-rotating/pure-bending fatigue test data for 2014-T6 aluminum in dripping commercial synthetic solution and in room-temperature air. A flow of liquid around the center section of the specimen was supplied by capillary action during the test. Source: Ref 3.37
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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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Image
Published: 01 November 2012
Fig. 29 Variation in rotating beam fatigue for (a) 2024-T4, (b) 7075-T6, (c) 2014-T6, and (d) 7079-T6 alloys. Notches (60°) were very sharp ( K t > 12), with a radius of approximately 0.005 mm (0.0002 in.). Results are from over a thousand rotating beam tests performed in the 1940s
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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: 01 March 2006
Q ≈ 1.1 P ≈ 0.03 (c) 2014-T6 aluminum ( Ref 4.17 ) σ u = 70 ksi Q ≈ 0.63 P ≈ 0.07 (d) 9Cr-4Co-0.45C steel ( Ref 4.18 ) σ u = 283 ksi Q ≈ 3.8 P ≈ 0.15
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Image
Published: 30 June 2023
Fig. 9.8 Effect of holding time at elevated temperature on residual room temperature strength of 2014-T6. Source: Ref 9.5
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Image
Published: 01 March 2006
Fig. 10.15 Ultrasonic technique for detecting early fatigue cracks. (a) Test configuration and specimen. (b) S-N curves for notched 2014-T6 0.60 in. sheet. Source: Ref 10.18
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Image
Published: 01 August 2005
Fig. 3.38 Fracture surface of a corrosion fatigue crack in a rotating bending specimen of 2014-T6 aluminum alloy. (a) Optical photograph showing the origin and beach marks typical of fatigue fracture. (b) Microphotograph of a section through the fatigue origin (arrow). The fracture surface
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Series: ASM Technical Books
Publisher: ASM International
Published: 01 August 2005
DOI: 10.31399/asm.tb.mmfi.t69540397
EISBN: 978-1-62708-309-6
... da/dN curves for 15 aluminum alloys, R = 0 to 0.1. Source: Ref A7.8 Tensile and fracture toughness data for the new 7033-T6 high-strength automotive alloy are presented in Table A7.3 , which also compares these properties with the conventional 2014-T6 and 6061-T6 alloys. S-N curves...
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
... 2014-T6 644 25.4 77 3.0 50 2.0 1.7 2024-T3 1022 40.2 76 3.0 67 2.6 2.0 2024-T81 725 28.5 97 3.8 76 3.0 6.0 2024-T86 806 31.7 77 3.0 58 2.3 6.2 6061-T4 378 14.9 57 2.2 38 1.5 0.4 6061-T6 422 16.6 98 3.9 42 1.7 0.7 7075-T6 688 27.1 119 4.7...
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: 30 June 2023
DOI: 10.31399/asm.tb.atia.t59340165
EISBN: 978-1-62708-427-7
... combinations of strength and corrosion resistance for forged automotive suspension components. The alloy 2014 has a special place in the forging business. Higher silicon in combination with magnesium and copper allow 2014-T6 forgings to be competitive in aerospace applications. Unlike 2024, it can reach...
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.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 August 1999
DOI: 10.31399/asm.tb.caaa.t67870099
EISBN: 978-1-62708-299-0
..., % Stressed (b) , % 2014-T6 3½% NaCl 84 0 42 55 Seacoast 365 0 18 28 Inland industrial 365 0 7 7 2219-T81 3½% NaCl 84 0 21 26 Seacoast 365 0 6 8 Inland industrial 300 0 … … 2024-T3 3½% NaCl 84 0 33 40 Seacoast 365 0 16 20 Inland industrial 365...
Abstract
Environmentally assisted cracking is a generic term that includes various cracking phenomena such as stress-corrosion cracking (SCC), corrosion fatigue cracking, and liquid-metal embrittlement. This chapter describes these cracking mechanisms beginning with SCC and the factors that influence its formation. It covers alloy selection and mitigation techniques and includes examples of SCC in aircraft components. The chapter also addresses corrosion fatigue, explaining how different environments and operating conditions affect crack propagation, fatigue strength, and fatigue life. It includes information on liquid-metal embrittlement as well.
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
... Tensile, % in 50.8 mm (2 in.) Free bend, % 2014-T6 4043 234 34 193 28 4 9 345 50 … … 2 5 2014-T6 2319 241 35 193 28 5 … 414 60 317 46 5 … 2219-T81, T87 2319 241 35 179 26 3 15 379 55 262 38 7 5 2219-T31, T37 2319 241 35 179 26 3 15 276 (b) 40...
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.t59340179
EISBN: 978-1-62708-427-7
..., losing their strengthening ability. Figure 9.8 illustrates effect of time at temperature for alloy 2014-T6. Heat-treated alloys are normally aged to a T temper at 120–150 °C (7075-T6 and T7) or 180 °C (6061-T6, 2014-T6). When service temperatures reach 200 °C, the T tempers are unstable; alloys overage...
Abstract
This chapter describes the attributes of aluminum products that are critical for key structural applications. It covers the selection criteria and evaluations performed by the aluminum supplier or customer: physical attributes, mechanical properties (tensile, fracture, and fatigue), and corrosion.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 August 1999
DOI: 10.31399/asm.tb.caaa.t67870025
EISBN: 978-1-62708-299-0
... of heat-treatable commercial wrought aluminum alloys Alloy Temper Potential (a) , V 2014 T4 −0.69 (b) T6 −0.78 2219 T3 −0.64 (b) T4 −0.64 (b) T6 −0.80 T8 −0.82 2024 T3 −0.69 (b) T4 −0.69 (b) T6 −0.81 T8 −0.82 2036 T4 −0.72 2090 T8E41 −0.83...
Abstract
Aluminum generally has excellent resistance to corrosion and gives years of maintenance-free service in natural atmospheres, fresh waters, seawater, many soils and chemicals, and most foods. This chapter explains why aluminum and aluminum alloys are naturally resistant to corrosion and describes the conditions and circumstances under which their natural defenses break down. It discusses the causes and forms of corrosion observed in aluminum alloys and the effect of composition, microstructure, processing history, and environmental variables such as impurities, fluid flow, surface area, pressure, and temperature.
Series: ASM Technical Books
Publisher: ASM International
Published: 01 January 2017
DOI: 10.31399/asm.tb.sccmpe2.t55090241
EISBN: 978-1-62708-266-2
... cracking of wrought aluminum alloys Alloy Temper Resistance to corrosion General (a) SCC (b) 1060 All A A 1100 All A A 1350 All A A 2011 T3, T4, T451 D (c) D T8 D B 2014 O … … T3, T4, T451 D (c) C T6, T651, D C T6510, T6511 2017 T4...
Abstract
Aluminum is protected by a barrier oxide film that, if damaged, reforms immediately in most environments. Despite this inherent corrosion resistance, there are conditions where aluminum alloys, like many materials, are subject to the effects of stress-corrosion cracking (SCC). This chapter describes those conditions, focusing initially on the effects of alloying elements and temper on solution potential and how it compares to other metals. It then addresses the issue of intergranular corrosion and its role in SCC. It explains how factors such as stress loads, grain structure, and environment determine whether or not stress-corrosion cracking develops in a susceptible alloy. It also provides stress-corrosion ratings for many alloys, tempers, and product forms and includes information on hydrogen-induced cracking.
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