Inconel 625
2019-08-20 09:07:01 Origin： Remark：0 Click：
Material standards Inconel 625 Round bar, Flat bar, Inconel 625 Plate, Forgings Steelmaking, ESR & VAR technique, Cold worked.
TECHNICAL DATA SHEET - Grade Inconel 625 & Alloy 625
OFFICIAL TEST CERTIFICATE: issued by TUV - SGS - BV
MATERIAL CATEGORY: Ni-Cr-Mo-Nb Superalloy
CHEMICAL COMPOSITION (mass weight - %)
Carbon, C (％): ≤ 0.10
Silicon, Si (％): ≤ 0.50
Manganese, Mn (％): ≤ 0.50
Phosphorus, P (％) ≤: 0.015
Sulfur, S (％) ≤: 0.015
Chromium, Cr (％): 20.0 ~ 23.0
Nickel, Ni (％): ≥ 58.0
Silicon, Si (％): ≤ 0.50
Manganese, Mn (％): ≤ 0.50
Phosphorus, P (％) ≤: 0.015
Sulfur, S (％) ≤: 0.015
Chromium, Cr (％): 20.0 ~ 23.0
Nickel, Ni (％): ≥ 58.0
Copper, Cu (％): -
Aluminum, Al (%): ≤ 0.40
Titanium, Ti (%): ≤ 0.40
Ferrum, Fe (%): ≤ 5.00
Molybdenum, Mo (%): 8.00 ~ 10.0
Niobium, Nb + Ta (%): 3.15 ~ 4.15
TYPICAL MECHANICAL PROPERTIES UNDER SOLUTION ANNEALED
Solution treated: ≥ 1090, rapid cooled
Annealed: ≥ 870, rapid cooled
Ageing treated: -
Condition: A
Tensile strength, σb/≥ MPa: 830
Yield strength, σ0.2/≥ MPa: 415
Elongation, δ ≥(％): 30
Hardness | HBW ≤: -
Yield strength, σ0.2/≥ MPa: 415
Elongation, δ ≥(％): 30
Hardness | HBW ≤: -
Suitable size /mm: 100
Tensile strength, σb/≥ MPa: 760
Yield strength, σ0.2/≥ MPa: 380
Elongation, δ ≥(％): 30
Hardness | HBW ≤: -
Yield strength, σ0.2/≥ MPa: 380
Elongation, δ ≥(％): 30
Hardness | HBW ≤: -
Suitable size /mm: 100 ~ 250
Condition: S
Tensile strength, σb/≥ MPa: 690
Yield strength, σ0.2/≥ MPa: 275
Elongation, δ ≥(％): 30
Hardness | HBW ≤: -
Yield strength, σ0.2/≥ MPa: 275
Elongation, δ ≥(％): 30
Hardness | HBW ≤: -
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.
AVAILABLE FORMS AND SHAPES
Round bar (diameter): 5.5 ~ 450mm
Square bar / Flat bar: 10 ~ 350mm
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.
AVAILABLE FORMS AND SHAPES
Round bar (diameter): 5.5 ~ 450mm
Square bar / Flat bar: 10 ~ 350mm
Wire rod (Diameter): 0.10 ~ 16mm
Steel strip via cold rolled: T0.1 - 3mm X W5 - 650mm X L (or in coil form)
Forging piece: Different shapes based on OEM.
Steel strip via cold rolled: T0.1 - 3mm X W5 - 650mm X L (or in coil form)
Forging piece: Different shapes based on OEM.
Other sizes can be supplied to meet specific requirements.
TECHNICAL SALES ASSISTANCE
If you meet further on any technical enquiry, pleased to EMAIL our qualified production engineers. Email: sales@ccsteels.com.
If you meet further on any technical enquiry, pleased to EMAIL our qualified production engineers. Email: sales@ccsteels.com.
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