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aluminum alloy 7475

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Published: 01 January 2005
Fig. 9 Double-well pan superplastically formed using aluminum alloy 7475 More
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Published: 01 January 1996
Fig. 11 Crack resistance curves for aluminum alloy 7475 sheet More
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Published: 01 January 1996
Fig. 71 Effect of overaging on part through crack growth of aluminum alloy 7475 subject to 500 h block flight-by-flight fighter spectrum loading in sump tank water. Source: Ref 127 More
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Published: 15 June 2019
Fig. 22 Crack resistance curves for aluminum alloy 7475 sheet. T-L, transverse-longitudinal; L-T, longitudinal-transverse. Source: Ref 43 More
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Published: 01 January 2005
Fig. 27 Examples of cavitation. (a) In aluminum (Al-7475) alloy. Courtesy of A.K. Ghosh. (b) In titanium (Ti-6Al-4V) alloy. Source: Ref 37 More
Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006747
EISBN: 978-1-62708-210-5
... Abstract Alloy 7475 is a controlled-toughness alloy for sheet and plate product forms. This datasheet provides information on key alloy metallurgy, processing effects on physical and mechanical properties, and fabrication characteristics of this 7xxx series alloy. aluminum alloy 7475...
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Published: 01 January 2006
Fig. 14 (a) Stress versus strain and (b) corresponding strain-rate sensitivity m for superplastic aluminum alloy 7475 in three different grain sizes. Tests were performed at 516 °C (960 °F), the optimal forming temperature for alloy 7475. Source: Ref 21 More
Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006743
EISBN: 978-1-62708-210-5
... provides a fatigue life comparison of these alloys. aluminum alloy 7175 aluminum alloy 7475 ductility fatigue life physical properties Alloys 7175 and 7475 ( Table 1 ) are high-purity versions of 7075 to improve ductility in the transverse direction of thick products. The Zn/Mg ratio in 7175...
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Published: 01 January 2006
Fig. 13 Steps involved in thermal and mechanical processing to produce superplastic aluminum alloy 7475. Source: Ref 30 More
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Published: 01 January 1996
Fig. 7 Aluminum alloys 2124 and 7475 are tougher versions of alloys 2024 and 7075. High-purity metal (low iron and silicon) and special processing techniques are needed to optimize toughness in these materials. Source: Ref 14 More
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Published: 01 January 1996
Fig. 12 Fracture toughness comparisons of aluminum alloys 2024, 2124, 7075 and 7475. Source: Ref 15 More
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Published: 15 June 2019
Fig. 17 Fracture toughness comparisons of aluminum alloys 2024, 2124, 7075, and 7475. Aluminum alloys 2124 and 7475 are tougher versions of alloys 2024 and 7075. High-purity metal (low iron and silicon) and special processing techniques are needed to optimize toughness in these materials More
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
... copper, chromium, silicon, and iron from commercial alloys. Consequently, an often-used approach to improve the toughness of high-strength aluminum alloys has been the reduction of iron and silicon levels. The development of improved alloys such as 7475, 7050, and 2124 has hinged, in large part, upon...
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Published: 01 January 1996
Fig. 10 (a) The decrease in fracture strain with increase of volume percent of micron-size intermetallic particles for a super-purity aluminum matrix and an Al-4Mg matrix. (b) A comparison of high-purity 7050 aluminum sheet, 7475 sheet, and a 7 xxx -series aluminum alloy. Tear strength More
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Published: 01 January 1996
Fig. 10 Critical stress intensity factor, K c , vs. tensile yield strength for 1.0 to 4.7 mm (0.040 to 0.188 in.) aluminum alloy sheet. Improved alloy 7475 is compared to other commercial alloys. Source: Ref 10 More
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Published: 15 June 2019
Fig. 21 Critical stress-intensity factor, K c , vs. tensile yield strength for 1.0 to 4.7 mm (0.040 to 0.188 in.) aluminum alloy sheet. Improved alloy 7475 is compared to other commercial alloys. Source: Ref 43 More
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Published: 01 January 2006
Fig. 43 Effect of hydrostatic pressure on the suppression of cavitation in a 7475 aluminum alloy specimen superplastically deformed at 516 °C (961 °F) More
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 practices of alloys 7050, 7075, and 7475 vary with product form, size, equipment, loading procedures, and furnace-control capabilities. The optimum practice for a specific item can be ascertained only by actual trial treatment of the item under specific conditions. Aging of aluminum alloys 7050...
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
... of one high-toughness aluminum alloy (7475-T7351) are shown in Table 4 . Typical room-temperature yield strength and plane-strain fracture toughness values for several high-strength aluminum alloys Table 3 Typical room-temperature yield strength and plane-strain fracture toughness values...
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Published: 01 January 2006
Fig. 5 Stress-strain curves at various constant strain rates for (a) Ti-6Al-4V at 927 °C (1701 °F) and (b) 7475 aluminum alloy at 516 °C (961 °F). Initial grain size: approximately 10 to 14 μm (395 to 550 μin.) More