AE961W
2024-12-19 03:33:00 Origin： Remark：0 Click：
AE961W (13Cr11Ni2W2MoV), a Martensitic type stainless steel, AE961W is used for the applications of expendable gas turbine engine development, Aviation
TECHNICAL DATA SHEET - AE961W & 13Cr11Ni2W2MoV
Material Category - Heat resisting steel for Turbine blade fabricating
Material Technical standards: GJB - 2294
Inventory & Stocklist - Round bar diameter 12 ~ 300mm. ESR ingot (0.5t, 1.0t, 1.5t, 2.0t, 3.0t )
Sheet & Plate: THK 0.5 ~ 6.0 X Width 200 ~ 1000 X L mm
MAIN CHEMICAL COMPOSITIONS (mass fraction - %)
Carbon, C (％): 0.10 ~ 0.16
Silicon, Si (％): ≤ 0.60
Manganese, Mn (％): ≤ 0.60
Phosphorus, P (％) ≤: 0.030
Sulfur, S (％) ≤: 0.010
Chromium, Cr (％): 10.5 ~ 12.0
Chromium, Cr (％): 10.5 ~ 12.0
Molybdenum, Mo (％): 0.35 ~ 0.50
Nickel, Ni (%): 1.40 ~ 1.80
Vanadium, V (%): 0.18 ~ 0.30
Tungsten, W (%): 1.50 ~ 2.00
Ferrum, Fe (%): balance
TYPICAL MECHANICAL PROPERTIES
Contion: QT1 (Tempering 660 ~ 710 Deg. C)
Tensile strength, Rm ≥ MPa: 885
Yield strength, Rp0.2 ≥ MPa: 738
Elongation, A5 ≥ (％): 15.0
Yield strength, Rp0.2 ≥ MPa: 738
Elongation, A5 ≥ (％): 15.0
Reduction of area, Z (%): 55.0
Impact, AKu/J ≥: 71
QT hardness, HB ≤: 269 ~ 311
Contion: QT2 (Tempering 540 ~ 590 Deg.C)
Tensile strength, Rm ≥ MPa: 1080
Yield strength, Rp0.2 ≥ MPa: 885
Elongation, A5 ≥ (％): 12.0
Yield strength, Rp0.2 ≥ MPa: 885
Elongation, A5 ≥ (％): 12.0
Reduction of area, Z (%): 50.0
Impact, AKv/J ≥: 55
QT hardness, HB ≤: 311 ~ 388
ADVANTAGE & SUPERIOR SERVICE
20+ years Focus On Special Steel Manufacturing and processing.
Stock over 60 grades with a competitive price, along with cutting service for specific requirement.
Customizing special material is welcome.
Stock over 60 grades with a competitive price, along with cutting service for specific requirement.
Customizing special material is welcome.
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