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7079-T6

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Published: 01 August 1999
Fig. 22 Stress-corrosion cracking (SCC) in an aluminum alloy 7079-T6 main landing gear H-link. (a) Overall view of H-link. (b) Pitting and intergranular corrosion that initiated SCC. Source: Ref 17 More
Image
Published: 01 August 1999
Fig. 23 SCC in aluminum alloy 7079-T6 spars of a vertical fin. (a) Cracks in the mating surface of the rear spar. (b) Fracture surface of a statically broken front spar. Source: Ref 17 More
Image
Published: 01 August 1999
Fig. 26 Aluminum alloy 7079-T6 aircraft wing spar (a) showing crack (arrow). (b) Fracture surfaces of opened spar crack. Note clamshell marks at termination of the crack (left). Suspected multiple initiation sites are located between arrows. 1.5 x . (c) Section of flange with surface at right 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
Series: ASM Technical Books
Publisher: ASM International
Published: 01 August 1999
DOI: 10.31399/asm.tb.caaa.t67870099
EISBN: 978-1-62708-299-0
... … … 7178-T76 L >360 >52 >380 >55 … … LT >360 >52 >360 >52 … … ST 170 25 170 25 … … 7079-T6 L >380 >55 >410 >60 >340 >50 LT 270 40 240 35 210 30 ST <55 <8 <55 <8 <55 <8 7049-T73 ST...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 August 1999
DOI: 10.31399/asm.tb.caaa.t67870063
EISBN: 978-1-62708-299-0
... 2024-T6 C Yes Yes 2011-T3 D Yes Yes 2024-T3, T4 D Yes Yes 2219-T3 D Yes Yes 7075-T6 D Yes Yes 7175-T66 D Yes Yes 7079-T6 D Yes Yes 7178-T6 D Yes Yes (a) Stress-corrosion cracking (SCC) ratings are based on service experience (excluding special...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 August 1999
DOI: 10.31399/asm.tb.caaa.t67870135
EISBN: 978-1-62708-299-0
... 71 2.8 1.7 7079-T6 635 25.0 65 2.6 37 1.5 0.5 Alclad alloys—heat treatable and non-heat-treatable 2014-T6 358 14.1 43 1.7 28 1.1 0 2024-T3 264 10.4 46 1.8 27 1.1 0 3003-H14 345 13.6 128 5.0 117 4.6 0 5155-H34 345 13.6 53 2.1 35 1.4 0 6061-T6...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 January 2017
DOI: 10.31399/asm.tb.sccmpe2.t55090241
EISBN: 978-1-62708-266-2
... L A (d) A (d) LT B (e) (d) B (e) (d) ST D (d) D (d) 7178-T76 L A (d) A (d) LT A (d) A (d) ST C (d) C (d) 7079-T6 L A (d) A A LT B (e) (d) B (e) B (e) ST D (d) D D (a) Ratings apply...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 August 1999
DOI: 10.31399/asm.tb.caaa.t67870025
EISBN: 978-1-62708-299-0
... … Al (99.999%) −0.76 −0.75 −0.73 7075-T7 , 8090-T7, 7049-T7, 7050-T7, 7475-T7 −0.77 −0.75 −0.73 7055-T77 … −0.75 −0.74 3004, 1060, 5050 … −0.75 … 5052, 5086, Alclad 2024, Alclad 2014 … −0.76 … 5154, 5454 , 5254, 5042 … −0.77 … 5056, 7079-T6, 5456, 5083 , 5182...
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.t67870191
EISBN: 978-1-62708-299-0
... No visible pitting 7039-T6 No visible pitting 7075-T6 Edge pitting only 7075-F, alclad Edge pitting only 7079-T6 Edge pitting only Extrusions 6351-T6 No visible pitting 6061-T6 No visible pitting 6063-T5 No visible pitting 6070-T6 No visible pitting 7039-T6 Scattered...
Series: ASM Technical Books
Publisher: ASM International
Published: 31 December 2020
DOI: 10.31399/asm.tb.phtbp.t59310351
EISBN: 978-1-62708-326-3
... the various alloy conditions. The temper designation is always presented immediately following the alloy designation, with a hyphen between the designation and the temper (e.g., 2014-T6). The first character of the temper designation is a capital letter indicating the general class of treatment...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 November 2012
DOI: 10.31399/asm.tb.ffub.t53610209
EISBN: 978-1-62708-303-4
... 7075-T6 to have a broader scatter for smooth specimens and a lower bound of performance for severely notched specimens that is below that for alloy 2024-T4 ( Fig. 29a ). Broader scatter is also evident for 7079 compared to 2014 ( Fig. 29c and d ). Fig. 29 Variation in rotating beam fatigue...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 March 2000
DOI: 10.31399/asm.tb.aet.t68260187
EISBN: 978-1-62708-336-2
... of various harder alloys Table 5 Typical heat treatment practices of various harder alloys Alloy Solution heat treatment Precipitation heat treatment Temperature Temper Temperature Time, h Temper °F °C °F °C 2014 935 500 T4 320 160 18 T6 2024 920 495 T3 375 190...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 March 2001
DOI: 10.31399/asm.tb.secwr.t68350095
EISBN: 978-1-62708-315-7
... pitting 2024-T3, alclad Edge pitting only 5456-H343 No visible pitting 5086-H34 No visible pitting 6061-T6 No visible pitting 7039-T6 No visible pitting 7075-T6 Edge pitting only 7075-F, alclad Edge pitting only 7079-T6 Edge pitting only Extrusions 6351-T6...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2001
DOI: 10.31399/asm.tb.aub.t61170351
EISBN: 978-1-62708-297-6
..., and corrosion resistance, with medium strength. Alloys in this heat-treatable group may be formed in the T4 temper (solution heat treated but not precipitation heat treated) and strengthened after forming to full T6 properties by precipitation heat treatment. Figure 3 shows the relationships between some...
Book Chapter

Series: ASM Technical Books
Publisher: ASM International
Published: 01 August 1999
DOI: 10.31399/asm.tb.caaa.t67870219
EISBN: 978-1-62708-299-0
Series: ASM Technical Books
Publisher: ASM International
Published: 01 January 2017
DOI: 10.31399/asm.tb.sccmpe2.t55090367
EISBN: 978-1-62708-266-2
.... 17.6 ). Fig. 17.6 Comparison of the SCC response under constant load with bending versus direct tension stressing for Al-5.3Zn-3.7Mg-0.3Mg-0.1Cr T6 temper alloy sheet. Tested to failure in 3% NaCl plus 0.1% H 2 O 2 . Source: Ref 17.9 Bending stress specimens experience other sources...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 August 2005
DOI: 10.31399/asm.tb.mmfi.t69540215
EISBN: 978-1-62708-309-6
... the analytical stable flaw shape with test data. The data sample consists of nine specimens made of 7075-T6 aluminum. These specimens were either 1.27 or 0.635 cm (0.5 or 0.25 in.) thick and 7.62 cm (3 in.) wide, with initial flaw depths approximately equal to 5 to 10% of the specimen thickness. The initial flaw...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2001
DOI: 10.31399/asm.tb.aub.9781627082976
EISBN: 978-1-62708-297-6