ASTM A538 / AMS 6514
2014-11-13 13:14:09 Origin： Remark：0 Click：
Specification 18% Nickel & 8.7% Cobalt High tensile steel AMS 6514 Round bar, Sheet, AISI A538 ESR Remelted, hot forging, hot rolling, heat treatment
MATERIAL SPECIFICATIONS - Grade ASTM A538 & AMS 6514
MATERIAL CATEGORY- 18% Nickel and Cobalt straightened steel
PRODUCT DESCRIPTION
The alloy is usually produced by VIM followed by VAR.
Bars and, where applicable, forgings are subjected to ultrasonic examination based on the different levels according to the buyers' requirements.
Bars are usually supplied black/bright in the annealed condition.
Final heat treatment - solution treatment + Ageing.
The alloy is usually produced by VIM followed by VAR.
Bars and, where applicable, forgings are subjected to ultrasonic examination based on the different levels according to the buyers' requirements.
Bars are usually supplied black/bright in the annealed condition.
Final heat treatment - solution treatment + Ageing.
ASTM A538 steels are iron-nickel alloys with absence of carbon and have metals such as molybdenum, cobalt, titanium and aluminum. The alloys have ultra-high strength, superior toughness characteristics and weldability. Typically, these alloys are used in aerospace applications, machinery and tooling and ordnance components and fasteners.
MATERIAL SPECIFICATIONS - AMS 6514, ASTM A538, UNS K93120, W-Nr 1.6358
CHEMICAL COMPOSITION (mass weight %)
Carbon, C (％): ≤ 0.030
Silicon, Si (％): ≤ 0.10
Manganese, Mn (％): ≤ 0.10
Phosphorus, P (％)≤: 0.010
Sulfur, S (％)≤: 0.010
Chromium, Cr (％): ≤ 0.50
Nickel, Ni (％): 18.0 ~ 19.0
Molybdenum, Mo (％): 4.60 ~ 5.20
Others (％): Al 0.05 ~ 0.15, Co 8.00 ~ 9.50. Ti 0.50 ~ 0.80, Cu ≤0.50
Silicon, Si (％): ≤ 0.10
Manganese, Mn (％): ≤ 0.10
Phosphorus, P (％)≤: 0.010
Sulfur, S (％)≤: 0.010
Chromium, Cr (％): ≤ 0.50
Nickel, Ni (％): 18.0 ~ 19.0
Molybdenum, Mo (％): 4.60 ~ 5.20
Others (％): Al 0.05 ~ 0.15, Co 8.00 ~ 9.50. Ti 0.50 ~ 0.80, Cu ≤0.50
MECHANICAL PROPERTIES UNDER ROOM TEMP.
Condition: heat treatment
Tensile strength, σb/MPa: 1930 Min.
Yield strenght, σ0.2≥/MPa: 1862
Elongation, δ5≥(％): 5.0
Yield strenght, σ0.2≥/MPa: 1862
Elongation, δ5≥(％): 5.0
Reduction of area, ψ≥(％): -
Hardness≥: 52HRC
Hardness≥: 52HRC
TYPICAL APPLICATIONS
Driveshafts, Gears, Fasteners, Landing and takeoff gear, Missile and ejector systems, Torsion springs.
TECHNICAL SALES ASSISTANCE
If you meet further on any technical enquiry, pleased to EMAIL our resident team of qualified production engineers, Email: sales@ccsteels.com.
If you meet further on any technical enquiry, pleased to EMAIL our resident team of qualified production engineers, Email: sales@ccsteels.com.
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Monthly rank
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