2S118 Stockist, 2S118 Equivalent Steel

2S118
2025-08-15 14:20:00   Origin:   Remark:0 Click:

Aircraft high quality structural alloy steel 2S118 flat bar, round bar steelmaking, Electroslag melting, Blooming, heat treatment, straightened, cold worked
TECHNICAL DATA SHEET - 2S118

OFFICIAL TEST CERTIFICATE: issued by TUV - SGS -  BV
MATERIAL CATEGORY: Aircraft "S" series alloy structural steel
TYPE OF STEEL: Ni Cr Mo alloy 
steel
MELTING PROCESS - Consumable electrode remelted steel
H S CODE For Customs - 7228 4000 / 7228 5000 / 7228 6000
TYPICAL CHEMICAL COMPOSITIONS (mass fraction %)
Carbon, C (%): 0.35 ~ 0.45
Silicon, Si (%): 0.10 ~ 0.35
Manganese, Mn (%): 0.40 ~ 0.80
Phosphorus, P (%) ≤: 0.035
Sulfur, S (%) ≤: 0.030
Chromium, Cr (%): 0.90 ~ 1.40
Nickel, Ni (%): 1.20 ~ 1.60
Molybdenum, Mo (%): 0.10 ~ 0.20
TYPICAL MECHANICAL PROPERTIES
Condition: Heat treatment
Tensile strength, Rm ≥ MPa: 980
Yield strength, Rp0.2 ≥ MPa: 835
Elongation, A5 ≥ (%): 10.0
Impact strength, AKv ≥ J: 78
Hardness HB: 269 Min.
DIMENSIONS & AVAILABLE FORMS
Round bar (diameter): 5.5 to 600mm
Wire rod (diameter): 3.0 to 16mm
Square bar / flat bar: 8 to 600mm
Length: Fixed length or random length or based on the customer's special requirement.
Heavy/middle plate via hot rolled: T60 - 400 X W50 - 1000 X L1000 - 5000mm
Sheet steel via cold rolled: T0.5 - 6 X W100 - 1000 X L1000 - 2000mm
Steel strip via cold rolled: T0.5 - 3 X W5 - 200 X L (or in coil form)
Forging piece: stepped shafts, other different shapes based on OEM. 
TECHNICAL SALES ASSISTANCE
If you meet further on any technical inquiry, pleased to EMAIL our resident team of qualified production engineers. E-mail: 
sales@ccsteels.com
.
 

Hot search:2S118

Previous page:2S117
Last page:Incoloy 926

Share to: