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aluminum-lithium alloys
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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
... Abstract Aluminum-lithium alloys have been developed primarily to reduce the weight of aircraft and aerospace structures. This article commences with a discussion on the physical metallurgy and development of aluminum-lithium alloys. It focuses on major commercial aluminum-lithium alloys...
Abstract
Aluminum-lithium alloys have been developed primarily to reduce the weight of aircraft and aerospace structures. This article commences with a discussion on the physical metallurgy and development of aluminum-lithium alloys. It focuses on major commercial aluminum-lithium alloys, including alloy 2090, alloy 2091, alloy 8090, alloy CP276, and Weldalite 049. The article also lists the chemical compositions, physical properties, fabrication characteristics, corrosion performance, and general applications of these alloys. A comparison of alloy properties is represented graphically.
Series: ASM Handbook
Volume: 6
Publisher: ASM International
Published: 01 January 1993
DOI: 10.31399/asm.hb.v06.a0001420
EISBN: 978-1-62708-173-3
... Abstract This article is a guide to the welding of commercially available aluminum-lithium alloys. It discusses the weldability issues created by weld porosity, hot cracking, and filler metal selection and presents the data revealed from weld characterization. aluminum-lithium alloys hot...
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in Aluminum-Lithium Alloys
> Properties and Selection: Nonferrous Alloys and Special-Purpose Materials
Published: 01 January 1990
Fig. 6 Use of aluminum-lithium alloys and superplastic-forming (SPF) aluminum-lithium alloys in a fighter aircraft
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in Aluminum-Lithium Alloys
> Properties and Selection: Nonferrous Alloys and Special-Purpose Materials
Published: 01 January 1990
Fig. 30 Pitting characteristics of selected aluminum and aluminum-lithium alloys exposed to an SO 2 salt fog for 32 days. (a) Pit density. (b) Pit depth
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in Aluminum-Lithium Alloys
> Properties and Selection: Nonferrous Alloys and Special-Purpose Materials
Published: 01 January 1990
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Published: 30 November 2018
Fig. 13 Comparison of corrosion resistance of aluminum-lithium alloys with 2000- and 7000-series alloys. Source: Ref 19
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Published: 01 January 1986
Fig. 72 Warm-worked and annealed aluminum-lithium alloy showing statically recovered subgrain structure. Thin foil TEM specimen
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Published: 01 January 2005
Fig. 29 Evolution of microstructure during hot rolling of an aluminum-lithium alloy undergoing dynamic recovery. (a) Optical micrograph showing heavily deformed, elongated initial grains. (b) TEM micrograph showing equiaxed subgrains. Courtesy of K.V. Jata, Air Force Research Laboratory
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Published: 01 January 2005
Fig. 1 Evolution of microstructure during hot-rolling of an aluminum lithium alloy undergoing dynamic recovery. (a) Optical micrograph showing heavily deformed elongated initial grains and (b) TEM micrograph showing equiaxed subgrains. Source: K.V. Jata, Air Force Research Laboratory
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Published: 31 October 2011
Fig. 3 Cross section of diffusion weld in aluminum-lithium alloy containing pure aluminum interlayer. Original magnification: 75×
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in Aluminum-Lithium Alloys
> Properties and Selection: Nonferrous Alloys and Special-Purpose Materials
Published: 01 January 1990
Fig. 2 Comparison of creep crack growth rates for aluminum-lithium alloy extrusions with those for other aluminum alloys. Alloy 8090 contains 2.5% Li, 1.5% Cu, 1.0% Mg, 0.12% Zr, and a balance of aluminum. T-L, crack plane and growth directions parallel to extrusion direction; L-T, crack plane
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in Aluminum-Lithium Alloys
> Properties and Selection: Nonferrous Alloys and Special-Purpose Materials
Published: 01 January 1990
Fig. 4 Average yield stress versus aging time for aluminum-lithium alloy 2090 (2.4% Li, 2.4% Cu, 0.18% Zr, balance aluminum) with various amounts of prior deformation
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in Aluminum-Lithium Alloys
> Properties and Selection: Nonferrous Alloys and Special-Purpose Materials
Published: 01 January 1990
Fig. 10 Longitudinal tensile strength versus temperature for aluminum-lithium alloy 2090-T84 and various other aluminum plate alloys
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in Aluminum-Lithium Alloys
> Properties and Selection: Nonferrous Alloys and Special-Purpose Materials
Published: 01 January 1990
Fig. 29 Average springback from 90° bend of aluminum-lithium alloy 8090 and two conventional alloys. All three alloys were tested in the as-received condition.
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in Procedure Development and Practice Considerations for Diffusion Welding[1]
> Welding, Brazing, and Soldering
Published: 01 January 1993
Fig. 3 Cross section of diffusion weld in aluminum-lithium alloy containing pure aluminum interlayer. 75×
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Published: 01 January 1993
Fig. 1 Schematic of ternary and quaternary aluminum-lithium alloy systems showing primary strengthening phases and corresponding commercial alloy designations
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Published: 30 November 2018
Fig. 11 Schematic of ternary and quaternary aluminum-lithium alloy systems showing primary strengthening phases and corresponding commercial alloy designations. Reprinted from Ref 17
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Published: 15 January 2021
Fig. 8 Fretting maps for an aluminum-lithium alloy. (a) Identification of the fretting regimes. (b) Corresponding material response. Adapted from Ref 22
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in Aluminum-Lithium Alloys
> Properties and Selection: Nonferrous Alloys and Special-Purpose Materials
Published: 01 January 1990
Fig. 7 Yield strengths of two aluminum-lithium candidate alloys for cryogenic tankage applications. Strain rate, 4 × 10 −4 /s with a 0.5-h hold at temperature
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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
... Abstract This article illustrates the relationships among commonly used 2xxx series alloys. It contains tables that list values for composition limits of aluminum-lithium alloys, and aerospace alloys and their temper conditions according to primary design requirements. 2xxx series...
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