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Copper alloy no. 647

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Journal Articles
Alloy Digest (1971) 20 (4): Cu-230.
Published: 01 April 1971
... COPPER ALLOY No. 647 is an age-hardenable copper-nickel-silicon alloy which can be age hardened to strength levels equivalent to those of many alloy steels. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also...
Journal Articles
Alloy Digest (1966) 15 (6): Cu-164.
Published: 01 June 1966
... CUNISIL-647 is a copper-nickel-silicon precipitation-hardening alloy having high strength, hardness, wear and corrosion resistance. Typical applications include electrical hardware and fasteners. This datasheet provides information on composition, physical properties, hardness, elasticity...
Journal Articles
Alloy Digest (2000) 49 (2): Cu-647.
Published: 01 February 2000
... in Table 1. Filing Code: Cu-647 Copper February 2000 OLIN C654 Table 1 Mechanical Properties Tensile strength Yield strength Temper MPa ksi MPa ksi Elongation in 2 in., % Approximate hardness, HRB 1 4 hard 517 621 75 90 414 60 33 81 1 2 hard 593 696 86 101 545 79 23 92 3 4 hard 669 772 97 112 634 92 13 95...
Journal Articles
Alloy Digest (2007) 56 (6): Al-404.
Published: 01 June 2007
... 2007 ASM International Alcan 2056 clad alloy corrosion-resistant alloys fatigue properties heat treatability tensile properties workability Chemical Composition, wt (Typical) Core, 2056 Cladding, 1050 Silicon 0.10 max · · · Silicon + Iron · · · 0.7 max Iron 0.12 max · · · Copper 3.3-4.3...
Journal Articles
Alloy Digest (2008) 57 (10): Al-418.
Published: 01 October 2008
... alloy in T7651 temper. The alloy possesses an improved strength-toughness balance over incumbent alloys and is used in aerospace structures. Chemical Composition, wt (Typical) Silicon 0.10 max Iron 0.13 max Copper 1.5 2.3 Magnesium 1.7 2.4 Zinc 5.7 6.7 Titanium 0.06 max Zirconium 0.05 0.12 Aluminum bal...
Journal Articles
Alloy Digest (2007) 56 (11): Al-407.
Published: 01 November 2007
... aerospace applications Alcan 7449 T7951 chemical composition compressive strength corrosion-resistant alloys fracture toughness heat treatability tensile properties workability Chemical Composition, wt (Typical) Silicon 0.12 max Iron 0.15 max Copper 1.40-2.1 Manganese 0.20 max Magnesium 1.8-2.7...
Journal Articles
Alloy Digest (2007) 56 (5): Al-403.
Published: 01 May 2007
... workability Chemical Composition, wt (Typical) Silicon 0.12 max Iron 0.15 max Copper 1.4 2.1 Manganese 0.20 max Magnesium 1.8 2.7 Chromium 0.005 max Zinc 7.5 8.7 Titanium + Zirconium 0.25 max Aluminum bal Physical Properties: Density, 7449, T79511 12 50 mm 2850 (0.103) (0.5 2 in.) thick extrusion, T6511...
Journal Articles
Alloy Digest (1991) 40 (5): Ni-66.
Published: 01 May 1991
... Alloy) NIMONIC ALLOY 105 is a wrought nickel-cobalt-chromium-base alloy strengthened by additions of molybdenum, aluminum and titanium. It has been developed for service up to 950 C (1742°F). Composition*: Carbon 0.12 Silicon 1.0 Copper 0.2 Iron 1.0 Manganese 1.0 Chromium 14.0-15.7 Titanium 0.9-1.5...
Journal Articles
Alloy Digest (1996) 45 (11): Ni-518.
Published: 01 November 1996
.... and nitriding; good resistance to stress-corro- sion cracking; and good resistance to dry chlorine and hydrogen chloride. Nicrofer is a registered trademark of KRUPP-VDM GmbH. Composition, wt Carbon Mangane= Silicon Nickel Chromium copper Aluminum litanium Phosphorus sulfur iron Boron Physical Properties...
Journal Articles
Alloy Digest (2001) 50 (6): Ni-568.
Published: 01 June 2001
... (Nickel Alloy) Filing Code: Ni-568 Nickel June 2001 NICROFER® 7216LC Chemical Composition, wt Carbon 0.025 max Manganese 1.0 max Silicon 0.05 max Nickel 72.0 min Chromium 14.0 17.0 Copper 0.5 max Phosphorus 0.3 max Sulfur 0.010 max Iron 6.0 10.0 Aluminum 0.3 max Boron 0.006 max Physical Properties...
Journal Articles
Alloy Digest (2023) 72 (9): CS-259.
Published: 01 September 2023
...: 0.10% maximum, 0.07 to 0.15%, 0.10 to 0.20%, 0.15 to 0.35%, 0.15 to 0.40%, 0.20 to 0.40%, or 0.30 to 0.60%. (d) When copper is required, 0.20% minimum is generally specified. Source: Ref 7 9 httpsdoi.org/10.31399/asm.ad.cs0259 ISSN: 002-614X Hot Forming Heat to 1050 °C (1920 °F). Wait for equalization...
Journal Articles
Alloy Digest (2022) 71 (7): CS-226.
Published: 01 July 2022
... rates of non-alloy steel specimens which were exposed for two years at various locations in the United States and Canada are given in Table 7. Source: Ref 17 18 Liquid-Metal Corrosion. Non-alloy steels can be embrittled by contact with liquid brass, aluminum bronze, copper, zinc, lead-tin solders...
Journal Articles
Alloy Digest (2022) 71 (6): CS-224.
Published: 01 June 2022
... Corrosion. Non-alloy steels can be embrittled by contact with liquid brass, aluminum bronze, copper, zinc, lead-tin solders, lithium, cadmium, and indium. The degree of embrittlement is greater for steels that have been heat treated to produce higher strength. Source: Ref 23 Corrosion in Fresh Water...
Journal Articles
Alloy Digest (2022) 71 (6): CS-225.
Published: 01 June 2022
... are given in Table 8. Source: Ref 21 22 Liquid-Metal Corrosion. Non-alloy steels can be embrittled by contact with liquid brass, aluminum bronze, copper, zinc, lead-tin solders, lithium, cadmium, and indium. The degree of embrittlement is greater for steels that have been heat treated to produce higher...
Journal Articles
Alloy Digest (2022) 71 (7): CS-227.
Published: 01 July 2022
... with liquid brass, aluminum bronze, copper, zinc, lead-tin solders, lithium, cadmium, and indium. The degree of embrittlement is greater for steels that have been heat treated to produce higher strength. Source: Ref 25 Table 1 Physical properties Property Liquidus temperature Density Coefficient of linear...