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high-strength structural alloy 7050

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Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006733
EISBN: 978-1-62708-210-5
... information on key alloy metallurgy, processing effects on physical and mechanical properties, fabrication characteristics, and applications of high-strength structural alloy 7050. Reference Reference 1. Alcoa Aluminum Alloy 7050 : Heat Treatable Aluminum Alloy , Alloy Digest: Data on Worldwide...
Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006606
EISBN: 978-1-62708-210-5
... fuselage structures, lower wing stringers, and stiffness dominated designs. Detailed performance data and technical details are available in the Aerospace Structural Materials Handbook. Alloy 2099-T83 has high strength and excellent corrosion resistance with moderate fracture toughness. Alloy 2099-T81...
Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006726
EISBN: 978-1-62708-210-5
... aging and can recover 100% of the strength if artificially aged after welding. Consequently, the alloys are often used for welded structures. At relatively high Zn/Mg ratios, they are resistant to SCC in thin sections. Yield strengths can be as much as twice that of the commonly welded alloys of the 5...
Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006739
EISBN: 978-1-62708-210-5
... in the solution heat treated and final aged conditions. Production facility thermal practices are proprietary. The combination of high strength and fracture toughness properties and corrosion resistance in thick sections makes 7085 suitable as a replacement for 7050 and other thick product alloys for use...
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
... for parts and structures requiring high strength-to-weight ratios, and they are commonly used to make truck and aircraft wheels, truck suspension parts, aircraft fuselage and wing skins, structural parts, and parts requiring good strength at temperatures up to 150 °C (300 °F). The 2 xxx alloys are usually...
Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.a0002406
EISBN: 978-1-62708-193-1
... and weldability at medium strengths, see wide use in conventional structural applications. The 2XXX and 7XXX alloys generally are used in applications involving highly stressed parts. Certain alloys and tempers within these classes are promoted for their high toughness at high strength. Stress-corrosion cracking...
Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006457
EISBN: 978-1-62708-210-5
... and plate; 2419-T6 and T8-type sheet, plate, extrusion, and forgings; 7050-T7-type plate, forgings, and extrusions; 7149-T7-type forgings; 7175-T6 and T7-type extrusions and forgings; and 7475-T6 and T7-type sheet and plate. Recognized conventional high-strength alloys that are not produced to minimum...
Series: ASM Handbook
Volume: 4E
Publisher: ASM International
Published: 01 June 2016
DOI: 10.31399/asm.hb.v04e.a0006288
EISBN: 978-1-62708-169-6
... Effects in Aluminum Alloys, Age Hardening of Metals , American Society for Metals, 1940, p 8–30 Zinc, when coupled with a smaller percentage of magnesium, results in heat treatable alloys of moderate to very high strength ( Fig. 6 ). Usually other elements, such as copper and chromium, are also...
Series: ASM Handbook
Volume: 13A
Publisher: ASM International
Published: 01 January 2003
DOI: 10.31399/asm.hb.v13a.a0003618
EISBN: 978-1-62708-182-5
... be generally divided into two categories. The first category consists of the copper-containing, high- strength alloys (e.g., 7075, 7050, 7055). These alloys are available in various forms (sheet, plate, extrusion) and are used extensively in the aerospace industry. The second category is low- copper alloys...
Series: ASM Handbook
Volume: 4E
Publisher: ASM International
Published: 01 June 2016
DOI: 10.31399/asm.hb.v04e.a0006252
EISBN: 978-1-62708-169-6
.... Jeanmart P. and Bouvaist J. , Finite Element Calculation and Measurement of Thermal Stresses in Quenched Plates of High-Strength 7075 Aluminum Alloy , Mater. Sci. Technol. , Vol 1 , 1985 , p 765 – 769 10.1179/mst.1985.1.10.765 11. Aksel B. , Arthur W.R. , and Mukherjee...
Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006549
EISBN: 978-1-62708-210-5
... and fatigue resistance at high endurances than naturally aged T3 and T4 tempers. However, artificial aging of 2 xxx alloys is accompanied by loss in toughness with resultant decrease in FCG resistance. Fig. 17 Comparison of axial-stress fatigue strengths of 0.812 mm (0.032 in.) aluminum alloy sheet...
Book Chapter

Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006603
EISBN: 978-1-62708-210-5
...) phases detrimental to thermal stability. Cu content was adjusted to be sufficiently high to achieve the required strength level, and sufficiently far from the solubility limit to maximize the strength/toughness balance. For this composition, the main hardening phase is T 1 (Al 2 CuLi). Mn and Zr help...
Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006741
EISBN: 978-1-62708-210-5
... ultimate strength and up to 15% higher yield strength than alloy 7050-T7451. Fracture toughness properties are typical. aluminum alloy 7099 floor beams fuselage frames high-strength aluminum-magnesium-zinc-copper alloys Kaiser aluminum alloys mechanical properties quench-sensitive alloys wing...
Series: ASM Handbook
Volume: 2A
Publisher: ASM International
Published: 30 November 2018
DOI: 10.31399/asm.hb.v02a.a0006520
EISBN: 978-1-62708-207-5
... Alloys Zinc, in amounts of 1 to 8%, is the major alloying element in 7 xxx - and 7 xx.x series alloys and, when coupled with a smaller percentage of magnesium, results in heat treatable alloys of moderate to very high strength with strengthening from MgZn 2 . In wrought alloys (7 xxx series), Zn...
Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006746
EISBN: 978-1-62708-210-5
... Solution Heat Treated, Stress Relieved, and Overaged,” and MMPDS. In upper-wing structures, alloy 7449-T79511 extrusions are used to stiffen long panels machined from very high strength 7 xxx alloy plates. Alloy 7449 in the form of extruded bars is best suited for use in applications such as forged...
Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006545
EISBN: 978-1-62708-210-5
... cracking of various aluminum alloys. Corrodent: 3% sodium chloride plus 0.3% hydrogen peroxide. Source: Ref 29 Fig. 10 Crack propagation rates in stress-corrosion tests using precracked specimens of high-strength 2 xxx -series aluminum alloys, 25 mm (1 in.) thick, double-cantilever beam...
Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.a0002351
EISBN: 978-1-62708-193-1
... these data it is apparent that the basic alloy chemistry affects the relationship between strength and toughness. From Table 1 it is also evident that transformed microstructures may greatly enhance toughness while only slightly reducing strength. Typical fracture toughness of high-strength titanium...
Series: ASM Handbook
Volume: 2
Publisher: ASM International
Published: 01 January 1990
DOI: 10.31399/asm.hb.v02.a0001059
EISBN: 978-1-62708-162-7
... vessels, marine service  H32 A A B D C A A D  H34 A A B C C A A D NA  H111 A A B D C A A D 5456 O A (d) B (d) B D C A B D High-strength welded structures, storage tanks, pressure vessels, marine applications  H111 A (d) B (d) C D C A A D...
Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006735
EISBN: 978-1-62708-210-5
... resistance (ASTM G47) in the S-T direction is 172 MPa (25 ksi) for the T7651 temper, and 241 MPa (35 ksi) for the T7451 temper. The combination of high strength and fracture toughness properties ( Tables 2 and 3 ) and corrosion resistance makes 7065 suitable as a replacement for 7010, 7050, 7075, 7475...
Series: ASM Desk Editions
Publisher: ASM International
Published: 01 December 1998
DOI: 10.31399/asm.hb.mhde2.a0003125
EISBN: 978-1-62708-199-3
..., rectangles or odd-shape blanks. Plate of certain alloys—notably the high-strength 2 xxx and 7 xxx series alloys—also is available in clad form. The most commonly used plate alloys are 2024, 2124, 2219, 7050, 7178, and 7475 for aircraft structures; 5083, 5086, and 5456 for marine, cryogenic and pressure...