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Published: 15 January 2021
Fig. 3 Aluminum alloy 2219-T8 in (a) as-received condition and (b) after isothermal exposure to 300 °C (570 °F) for 2.8 h. Note the increase in quantity of smaller precipitates in the aged sample. Courtesy of K. Anderson Wedge More
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Published: 01 January 2000
Fig. 2 S / N data and best-fit curves for aluminum alloy 2219-T851 at five different stress ratios. Stresses are based on net section. 1.0 ksi = 6.8948 MPa More
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Published: 01 January 1996
Fig. 6 Best-fit S / N curves for notched, K t = 2.0, 2219-T851 aluminum alloy plate, longitudinal direction. This is a typical S - N diagram from MIL-HDBK-5D showing the fitted curve as the actual data that support the diagram. This is the currently required approach for representing More
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Published: 01 December 2004
Fig. 14 2219 aluminum alloy, gas metal arc weld (parameters unknown). Fusion-zone microstructure in which the cellular solidification structure is revealed by the distribution of the divorced eutectic microconstituent between the cells. Etchant: Kroll's reagent. Magnification: 200× More
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Published: 01 November 2010
Fig. 1 Solidification paths of a 2219 aluminum alloy, temperature versus solid fraction, from two models and the lever rule. L, liquid; fcc, face-centered cubic More
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Published: 01 January 2003
Fig. 26 Effect of water vapor on the fracture surface appearance of aluminum alloy 2219-T851 fatigue tested (a) in 0.101 MPa (1 atm) dry argon and (b) in 27 Pa (0.2 torr) water vapor. Testing conditions were the same except for frequency, which was 20 Hz in (a) and 5 Hz in (b More
Book Chapter

Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006608
EISBN: 978-1-62708-210-5
... Abstract This datasheet provides information on key alloy metallurgy and processing effects on mechanical properties of Al-Li plate alloy 2195. A figure provides a performance comparison of 2195-T84 and 2219-T87 alloys. aluminum alloy 2195 aluminum alloy 2195-T84 aluminum alloy 2219-T87...
Book Chapter

Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006614
EISBN: 978-1-62708-210-5
.... It retains good mechanical properties up to 250 °C, or 480 °F ( Ref 1 , 2 ) and higher. Due to its high tensile strength and good ductility at cryogenic temperatures, excellent weldability, and good resistance to stress corrosion cracking, alloy 2219 aluminum alloy is an attractive material for construction...
Book Chapter

Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006611
EISBN: 978-1-62708-210-5
..., and applications of this 2xxx series alloy. Alclad 2219 aluminum alloy 2219 elevated temperature applications fabrication characteristics physical properties post-weld heat treatment tensile properties welded structures Alloy 2219 ( Table 1 ) has good machinability and good mechanical properties...
Book Chapter

Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006594
EISBN: 978-1-62708-210-5
... 2050-T852 High-strength, intermediate-thickness products 7065-T7651 7065-T7451 7099-T7651 7099-T7451 7160-T7651 Weldability … 2219 2219 2219 Cryogenic properties … 2519 2519 2519 Fig. 3 Advances in aluminum alloys with higher toughness. Source: Ref 2 References...
Book Chapter

Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006602
EISBN: 978-1-62708-210-5
... composition aluminum alloy 2040 forging alloys high-temperature strength alloys mechanical properties Alloy 2040 ( Table 1 ) is a forging alloy with a significant improvement in elevated temperature properties over alloys 2014 and 2219. It was developed by Alcoa (now Arconic) as a replacement...
Book Chapter

By Eugene M. Langworthy
Book: Machining
Series: ASM Handbook
Volume: 16
Publisher: ASM International
Published: 01 January 1989
DOI: 10.31399/asm.hb.v16.a0002170
EISBN: 978-1-62708-188-7
.... Although chemical sizing can add significantly to the normal chemical milling costs, it is frequently justified by the resulting weight savings. Example 4: Chemical Sizing of Engine Cowl Inlet Duct Skins Engine inlet cowl skins, shown in Fig. 12 , are produced from aluminum alloy 2219...
Book Chapter

Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006623
EISBN: 978-1-62708-210-5
... Abstract This article provides a comprehensive matrix for selecting an aluminum filler alloy for the gas tungsten arc and gas metal arc welding processes, based on the various requirements or service conditions. A table lists the nominal strengths of aluminum filler metals. aluminum...
Book Chapter

Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006622
EISBN: 978-1-62708-210-5
... Abstract This article lists temper designations and their definitions for aluminum alloys along with their product forms used in the United States (ANSI H35.1), Europe (EN 515), and internationally (ISO 2107). aluminum alloys temper designations Temper designations and definitions...
Book Chapter

By Richard S. James
Series: ASM Handbook
Volume: 2
Publisher: ASM International
Published: 01 January 1990
DOI: 10.31399/asm.hb.v02.a0001063
EISBN: 978-1-62708-162-7
... orientation (crack plane and growth direction parallel to the extrusion direction) are on the average much higher than those for aluminum alloys 2219 and 2124. In contrast, the growth rates for Al-Li 8090 in the L-T orientation (crack plane and growth direction parallel to the extrusion direction) are much...
Book Chapter

Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006691
EISBN: 978-1-62708-210-5
... Table 4 Filler alloys for welding selected aluminum alloys used for sustained elevated-temperature service Aluminum alloys Acceptable filler alloys Wrought Cast 1 xxx series … Base alloy, 1100, 1188, 4043, 4047 2014, 2219 222.0, 295.0, 319.0, 333.0 2319, 4043, 4145 3003, 5005...
Image
Published: 01 January 1993
Fig. 3 Effect of welding heat on microstructure, hardness, and corrosion potential of three aluminum alloy welded assemblies. (a) Alloy 5456-H321 base metal with alloy 5556 filler. (b) Alloy 2219-T87 base metal with alloy 2319 filler. (c) Alloy 7039-T651 base metal with alloy 5183 filler More
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Published: 15 June 2019
Fig. 1 Yield strength/fracture toughness combination as a function of temperature for alloy 2219-T87 and 2090-T81 alloy. The shaded region represents the range of strength/toughness combinations for typical aerospace aluminum alloys. Source: Ref 1 More
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Published: 01 January 1990
Fig. 13 Yield strength/fracture toughness (combination as a function of temperature for 2090-T81 alloy. The shaded region represents the range of strength/toughness combinations for typical aerospace aluminum alloys. Data for alloy 2219-T87 as a function of temperature are shown for comparison More
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Published: 01 June 2016
Fig. 1 Partial equilibrium diagram for aluminum-copper alloys, with temperature ranges for precipitation-hardening operations. The vertical lines (a) and (b) show two alloys with 4.5% Cu and 6.3% Cu, respectively. The solubility relationships and heat treating behavior of these compositions More