CD4MCu
2017-07-28 11:12:44 Origin： Remark：0 Click：
Technical specifications of American high temperature alloys CD4MCu datasheet,CD4MCu Chemical compositions,CD4MCu mechanical properties from Steelmaking, ESR melted, Blooming,Gr.CD4MCu Forging, Hot rolling, Heat treatment, Straightening, Ultrasonic 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.
MATERIAL TECHNICAL DATA SHEET - Grade CD4MCu
OFFICIAL TEST CERTIFICATE: issued by TUV - SGS - BV
MATERIAL TYPE: Fe - Cr - Ni - Mo - Cu Duplex alloy
SPECIFICATIONS: ASTM A744
CHEMICAL COMPOSITION (WEIGHT %)
C (％): ≤ 0.40
Si (％): ≤ 1.00
Mn (％): ≤ 1.00
P (％)≤: 0.040
S (％)≤: 0.025
Cr (％): 24.5 ~ 26.5
C (％): ≤ 0.40
Si (％): ≤ 1.00
Mn (％): ≤ 1.00
P (％)≤: 0.040
S (％)≤: 0.025
Cr (％): 24.5 ~ 26.5
Ni (％): 4.75 ~ 6.00
Mo (％): 1.75 ~ 2.25
Co (%): -
Co (%): -
W (%): -
Al (%): -
Al (%): -
Cu (%): 2.75 ~ 3.25
Ti (%): -
Ti (%): -
Fe (%): Remainder
MECHANICAL PROPERTIES
Tensile strength, σb/≥ MPa: 724
Yield strength, σ0.2/≥ MPa: 552
Elongation, δ ≥(％): 22.0
Reduction of area, ф ≥ (％): 45.0
Hardness | HB: 224
Yield strength, σ0.2/≥ MPa: 552
Elongation, δ ≥(％): 22.0
Reduction of area, ф ≥ (％): 45.0
Hardness | HB: 224
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 treated + Aged
FORMS AND SHAPES
Round bar (Diameter): 0.50mm to 650mm
Square bar / Flat bar: 3mm to 450mm
Steel strip via cold rolled: T0.1 - 3mm X W5 - 200mm X L (or in coil form)
Forging piece: Different shapes based on OEM.
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 treated + Aged
FORMS AND SHAPES
Round bar (Diameter): 0.50mm to 650mm
Square bar / Flat bar: 3mm to 450mm
Steel strip via cold rolled: T0.1 - 3mm X W5 - 200mm 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 EMAIL our qualified production engineers. - Email: lh.steel@hotmail.com
You also can reach our sales dept via E-mail: sales@ccsteels.com
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