1.4922
2025-06-04 13:47:00 Origin： Remark：0 Click：
1.4922 is a Martensitic Chromium-Molybdenum-Vanadium base high tensile Creep-resisting steel X20CrMoV12-1 Round bar, flat bar, ESR ingot, forging piece
TECHNICAL DATA SHEET - W-Nr.1.4922 & X20CrMoV11-1
PRODUCT DESCRIPTION
The alloy is usually produced by AOD / EAF followed by electroslag refining (ESR or VAR) if necessary for special purpose. Bars and, where applicable, forgings are subjected to ultrasonic examination based on the different level according to the buyers' requirements.
Bars are usually supplied bright in the solution annealing condition.
Final heat treatment - heat treatment / Q+T.
MATERIAL SPECIFICATIONS - DIN 17742, 17460, 17480, DIN EN 103021, 10296, 10095
PROFILE AND DIMENSIONS
Round bar / disc (diameter): 5.5mm to 800mm
Square bar / flat bar: 10mm to 800mm
Plate / Sheet steel / Steel strip: 0.5mm to 1200mm
Length: random length or based on the customer's special requirement.
Forged steel shape: stepped shafts, and other different shapes based on OEM.
CHEMICAL COMPOSITIONS (mass weight %)
Carbon, C (％): 0.17 ~ 0.23
Silicon, Si (％): ≤ 0.50
Manganese, Mn (％): ≤ 1.00
Phosphorus, P (％) ≤: 0.030
Sulfur, S (％) ≤: 0.030
Chromium, Cr (％): 10.0 ~ 12.5
Nickel, Ni (％): 0.30 ~ 0.80
Molybdenum, Mo (％): 0.80 ~ 1.20
Vanadium, V (％): 0.25 ~ 0.35
MECHANICAL PROPERTIES - HOT WORKING, HEAT TREATMENT AND HARDNESS
Silicon, Si (％): ≤ 0.50
Manganese, Mn (％): ≤ 1.00
Phosphorus, P (％) ≤: 0.030
Sulfur, S (％) ≤: 0.030
Chromium, Cr (％): 10.0 ~ 12.5
Nickel, Ni (％): 0.30 ~ 0.80
Molybdenum, Mo (％): 0.80 ~ 1.20
Vanadium, V (％): 0.25 ~ 0.35
MECHANICAL PROPERTIES - HOT WORKING, HEAT TREATMENT AND HARDNESS
Hot forming temperature /℃: 1100～850
Heat treatment temperature /℃ | annealing: 750~780
Heat treatment temperature /℃ | quenching or solution: 1030 ~ 1070 air / oil
Heat treatment temperature /℃ | tempering: 720~770
Heat treatment temperature /℃ | ageing: -
Condition: heat treatment
Mechanical property under room temperature | σb / MPa: 700~ 850
Mechanical property under room temperature | σs ≥ MPa: 500
Mechanical property under room temperature | δ5 ≥ (％): 16
Mechanical property under room temperature | Akv (DVM): 41
Heat stability temperature/℃: 580
Non-scale temperature in air /℃: 700
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.
Gas turbine, Turbine blade, Fuel nozzle, Heat treating fixture, Furnace muffle, Nuclear reactor.
Turbine engine parts - mechanical gears, gear shaft, main axis, blade.
Mechanical parts - bolt and nut, fastener.
Heat treatment furnace flask and components, especially in the carbonization.
These materials must stand up to high heat, extreme oxidation potential and recycling.
These materials must stand up to high heat, extreme oxidation potential and recycling.
TECHNICAL SALES ASSISTANCE
If you meet further on any technical enquiry. pleased to Email (sales@ccsteels.com) or call our resident team of qualified production engineers.
Hot search：1.4922
Previous page：X20CrMoV12-1
Last page：X22CrMoV12-1
