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2219-T62

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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
... NaCl plus 3 g H 2 O 2 per liter T31, T37, T351 tempers, −0.64 V T62, T81, T87, T851 tempers, −0.80 V Typical tensile properties of alloy 2219 Table 4 Typical tensile properties of alloy 2219 Temper Tensile strength, Yield strength, Elongation, % MPa ksi MPa ksi O 172...
Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.a0002408
EISBN: 978-1-62708-193-1
... fatigue life. Typical endurance limit values of wrought aluminum alloys Table 1 Typical endurance limit values of wrought aluminum alloys Alloyand temper Fatigue endurance limit, MPa (a) 2014-T6 124.11 2219-T62 103.43 2219-T81 103.43 5052-H32 117.22 5052-H34 124.11...
Series: ASM Desk Editions
Publisher: ASM International
Published: 01 December 1998
DOI: 10.31399/asm.hb.mhde2.a0003126
EISBN: 978-1-62708-199-3
... … … … … … … 73 10.6 2219-T31, T351 360 52 250 36 17 … … … … … … 73 10.6 2219-T37 395 57 315 46 11 … … … … … … 73 10.6 2219-T62 415 60 290 42 10 … … … … 105 15 73 10.6 2219-T81, T851 455 66 350 51 10 … … … … 105 15 73 10.6 2219-T87 475 69 395...
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
... 36 T62 Plate 535 995 T31 (a) 175 350 18 T81 (a) T37 (a) 175 350 18 T87 (a) T351 (b) 175 350 18 T851 (b) T42 190 375 36 T62 Rolled or cold-finished wire, rod, and bar 535 995 T351 (b) 190 375 18 T851 (b) 2219 (f) Extruded rod, bar, shapes...
Series: ASM Handbook
Volume: 4E
Publisher: ASM International
Published: 01 June 2016
DOI: 10.31399/asm.hb.v04e.a0006289
EISBN: 978-1-62708-169-6
... 2218-T72 40.00 2219-O 44.00 2219-T31, T37, and T351 28.00 2219-T62, T81, T87, and T851 30.00 2319-O 44.00 2618-T61 37.00 3003-O 44.70–49.80 3003-O 50.00 3003-H14 and H12 37.80–51.50 3003-H12 42.01 3003-H14 41.00 3003-H18 40.00 3003-H24 and H28 37.80...
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
... in underaging conditions to improve formability 2018 Forgings and forging stock T62 Solution heat treated in a furnace from annealed or F temper and artificially aged to demonstrate response to heat treatment All All T63, T64, T65 Solution heat treated and artificially aged to specified mechanical...
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
... T62 Plate 535 995 T31 (a) 175 350 18 T81 (a) T37 (a) 175 350 18 T87 (a) T351 (b) 175 350 18 T851 (b) T42 190 375 36 T62 Rolled and cold-finished wire, rod, and bar 535 995 T351 (b) 190 375 18 T851 (b) 2219 (f) Extruded rod, bar, shapes, and tube...
Series: ASM Handbook
Volume: 2A
Publisher: ASM International
Published: 30 November 2018
DOI: 10.31399/asm.hb.v02a.a0006482
EISBN: 978-1-62708-207-5
... response to heat treatment or when heat treatment is performed by user Temper Description (a) T42 Solution heat treated from annealed or F temper and naturally aged to a substantially stable condition T62 Solution heat treated from annealed or F temper and artificially aged T7 x 2...
Series: ASM Handbook
Volume: 2A
Publisher: ASM International
Published: 30 November 2018
DOI: 10.31399/asm.hb.v02a.a0006531
EISBN: 978-1-62708-207-5
... Cooled from elevated-temperature shaping process and artificially aged. When a second digit is present, it is material dependent and has no general interpretation. T6 Solution heat treated and artificially aged T62 Solution heat treated from the O or F temper to demonstrate response to heat...
Series: ASM Handbook
Volume: 4E
Publisher: ASM International
Published: 01 June 2016
DOI: 10.31399/asm.hb.v04e.a0006251
EISBN: 978-1-62708-169-6
... … … … … 10.6 2219-T42 52 27 20 … … … … 10.6 2219-T31, T351 52 36 17 … … … … 10.6 2219-T37 57 46 11 … … … … 10.6 2219-T62 60 42 10 … … … 15 10.6 2219-T81, T851 66 51 10 … … … 15 10.6 2219-T87 69 57 10 … … … 15 10.6 2618-T61 64 54 … 10 115...
Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006544
EISBN: 978-1-62708-210-5
... as it is for steels. Typical hardness values for wrought aluminum alloys Table 3 Typical hardness values for wrought aluminum alloys Alloy and temper Product form (a) Hardness HRB HRE HRH HRIST 2014-T3, -T4, -T42 All 65–70 87–95 … … 2014-T6, -T62, -T65 Sheet (b) 80–90 103–110...
Series: ASM Desk Editions
Publisher: ASM International
Published: 01 December 1998
DOI: 10.31399/asm.hb.mhde2.a0003204
EISBN: 978-1-62708-199-3
...) T42 190 375 36 T62 Plate 535 995 T31 (d) 175 350 18 T81 (d) T37 (d) 175 350 18 T87 (d) T351 (e) 175 350 18 T851 (e) T42 190 375 36 T62 Rolled or cold-finished wire, rod, and bar 535 995 T351 (e) 190 375 18 T851 (e) 2219 (f) Extruded rod, bar...
Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006543
EISBN: 978-1-62708-210-5
... and has no general interpretation. T6 Solution heat treated and artificially aged T62 Solution heat treated from the O or F temper to demonstrate response to heat treatment and artificially aged T651 Solution heat treated, stress relieved by stretching a controlled amount (permanent set 1.5–3...
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
... Military supersonic aircraft 2218 T61 D C … … … … C … C Jet engine impellers and rings  T72 D C … B D C B D C 2219 O … … … … D A B D Structural uses at high temperatures (to 315 °C, or 600 °F) high-strength weldments  T31, T351, T3510, T3511 D (c) C C B...
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 7475-T6 and T7-type sheet and plate. Recognized conventional high-strength alloys that are not produced to minimum toughness specifications include 2014, 2024, 2219, 7075, 7079, and 7178. Table 1 is a summary of plane-strain fracture toughness values for a wide variety of aluminum alloys, including...
Series: ASM Desk Editions
Publisher: ASM International
Published: 01 December 1998
DOI: 10.31399/asm.hb.mhde2.a0003130
EISBN: 978-1-62708-199-3
... C B Permanent mold castings 242.0 T571, T61 D C 308.0 F C B 319.0 F C B T6 C C 332.0 T5 C B 336.0 T551, T65 C B 354.0 T61, T62 C A 355.0 All C A C355.0 T61 C A 356.0 All B A A356.0 T61 B A F356.0 All B A A357.0 T61 B...
Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006626
EISBN: 978-1-62708-210-5
... 58 0.288 (a) 2199 T8 0.095 2.62 13.1 1040–1200 610 18 58 58 0.288 (a) 2219 O 0.103 2.84 12.4 1010–1190 1190 44 138 24 0.215 … T31, T37 0.103 2.84 12.4 1010–1190 780 28 88 37 0.215 … T62 0.103 2.84 12.4 1010–1190 840 30 94 35 0.215 … T81...
Series: ASM Handbook
Volume: 2
Publisher: ASM International
Published: 01 January 1990
DOI: 10.31399/asm.hb.v02.a0001060
EISBN: 978-1-62708-162-7
...–1.000 in. thick 400 58 … … 235 34 14 Sheet, T6, T62  0.020–0.039 in. thick 440 64 … … 395 57 6  0.040–0.0249 in. thick 455 66 … … 400 58… 7 Plate, T62, T651  0.250–2.000 in. thick 460 67 … … 405 59 7–4  2.001–2.500 in. thick 450 65 … … 400...
Series: ASM Handbook
Volume: 2
Publisher: ASM International
Published: 01 January 1990
DOI: 10.31399/asm.hb.v02.a0001061
EISBN: 978-1-62708-162-7
...–625 970–1160 33 0.31 22.1 (12.3) 23.6 (13.1) 224.0 T62(S) 2.81 2824 0.102 550–645 1020–1190 30 0.28 … … 238.0 F(P) 2.95 1938 0.107 510–600 950–1110 25 0.25 21.4 (11.9) 22.9 (12.7) 240.0 F(S) 2.78 2768 0.100 515–605 960–1120 23 0.23 22.1 (12.3) 24.3 (13.5...
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
...-Al99.5 … Al99.3 1370 E-Al99.7 2011 AlCu6BiPb 2014 AlCu4SiMg 2014A AlCu4SiMg(A) 2017 AlCu4MgSi 2017A AlCu4MgSi(A) 2024 AlCu4Mg1 2030 AlCu4PbMg 2117 AlCu2.5Mg 2219 AlCu6Mn 3003 AlMn1Cu 3004 AlMn1Mg1 3005 AlMn1Mg0.5 3103 AlMn1 3105 AlMn0.5Mg0.5...