X22CrMoV12-1
2018-05-17 16:53:12 Origin： Remark：0 Click：
Alloys X22CrMoV12-1 datasheet, X22CrMoV12-1 Ex-stock, X22CrMoV12-1 Mechanical property from Steelmaking, ESR & VAR technique, Blooming, Hot forging, Hot rolling, Heat treatment, Straightening, 100% Ultrasonic flaw detection test, Cold working or Machined. All of these materials conform to Military standard, nuclear power. 100% Ultrasonic test ASTM E2375 /SAE AMS 2154 /SEP 1923 /GB/T 4162 /EN 10228-3.
TECHNICAL DATA SHEET - Grade X22CrMoV12-1
DIN 17442,17744 (2002/1985), DIN EN 10302, 10269
TYPICAL APPLICATIONS
Superalloy is widely used to produce the high temperature components for gas turbine in the field of aviation, naval vessels and industry, such as turbine blade, guide blade, turbine disc, high pressure compressor disc, combustor, and also production of energy conversion devices, such as aerospace craft, rocket motor, nuclear reactor, petrochemical equipments, coaly transforming and so on. The alloy is usually produced by AOD / VOD /VIM followed by electroslag refining (ESR) / VAR if necessary for special purpose.
Bars and, where applicable, forgings are subjected to ultrasonic examination based on the different levels according to the buyers' requirements.
Bars are usually supplied bright surface in the solution annealed condition.
Final heat treatment - solution + Aged or Double aged.
FORMS AND SHAPES
Round bar (Diameter): 5.50 ~ 650mm
Square bar / Flat bar: 10 ~ 700mm
CHEMICAL COMPOSITION (WEIGHT %)
Carbon, C (％): 0.18 ~ 0.24
Silicon, Si (％): ≤ 0.50
Manganese, Mn (％): 0.40 ~ 0.90
Phosphorus, P (％)≤: 0.025
Sulfur, S (％)≤: 0.015
Silicon, Si (％): ≤ 0.50
Manganese, Mn (％): 0.40 ~ 0.90
Phosphorus, P (％)≤: 0.025
Sulfur, S (％)≤: 0.015
Chromium, Cr (％): 11.0 ~ 12.5
Nickel, Ni (％): 0.30 ~ 0.80
Molybdenum, Mo (％): 0.80 ~ 1.20
Nickel, Ni (％): 0.30 ~ 0.80
Molybdenum, Mo (％): 0.80 ~ 1.20
Nitrogen, N (%): -
Aluminum, Al (%): -
Niobium, Nb (%): -
Vanadium, V (％): 0.20 ~ 0.35
Vanadium, V (％): 0.20 ~ 0.35
MECHANICAL PROPERTIES UNDER ROOM TEMP.
Condition: solution treatment
Tensile strength, σb/MPa: 700 ~ 850
Tensile strength, σb/MPa: 700 ~ 850
Yield strength, σs≥/MPa: 600
Elongation, δ5≥(％): 14.0
Elongation, δ5≥(％): 14.0
Non-scale temperature in Air: 600℃
Superalloy is widely used to produce the high temperature components for gas turbine in the field of aviation, naval vessels and industry, such as turbine blade, guide blade, turbine disc, high pressure compressor disc, combustor, and also production of energy conversion devices, such as aerospace craft, rocket motor, nuclear reactor, petrochemical equipments, coaly transforming and so on. The alloy is usually produced by AOD / VOD /VIM followed by electroslag refining (ESR) / VAR if necessary for special purpose.
Bars and, where applicable, forgings are subjected to ultrasonic examination based on the different levels according to the buyers' requirements.
Bars are usually supplied bright surface in the solution annealed condition.
Final heat treatment - solution + Aged or Double aged.
FORMS AND SHAPES
Round bar (Diameter): 5.50 ~ 650mm
Square bar / Flat bar: 10 ~ 700mm
Wire rod (Diameter): 0.50 ~ 16mm
Steel strip via cold rolled: T0.5 - 3mm X W10 - 650mm X L (or in coil form)
Forging piece: Different shapes based on OEM.
Steel strip via cold rolled: T0.5 - 3mm X W10 - 650mm X L (or in coil form)
Forging piece: Different shapes based on OEM.
TECHNICAL SALES ASSISTANCE
If you meet further on any technical enquiry, pleased to E-MAIL (sales@ccsteels.com) our qualified production engineers.
If you meet further on any technical enquiry, pleased to E-MAIL (sales@ccsteels.com) our qualified production engineers.
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