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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 More
Image
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 More
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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 More
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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 More
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Published: 01 August 1999
Fig. 2 Pitting corrosion of an aluminum alloy 2014T6 sheet. Pitting occurred during the manufacturing cycle. Note the intergranular nature of the pit. 150× More
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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 More
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 More
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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 More
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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 More
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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 More
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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 More
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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 More
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...
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...
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...
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...
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...
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...
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...
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...