HR3C / S31042
2018-08-22 10:36:36 Origin： Remark：0 Click：
Technical specifications of American high temperature alloys HR3C & S31042 datasheet, HR3C & S31042 Chemical compositions, HR3C & S31042 mechanical properties 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 HR3C & S31042
OFFICIAL TEST CERTIFICATE: issued by TUV - SGS - BV
MATERIAL CATEGORY: Ni-Cr--Fe Superalloy
CHEMICAL COMPOSITION (WEIGHT %)
C (％): 0.04 ~ 0.10
C (％): 0.04 ~ 0.10
Si (％): ≤ 0.75
Mn (％): ≤ 2.00
P (％)≤: 0.030
Mn (％): ≤ 2.00
P (％)≤: 0.030
S (％)≤: 0.030
Cr (％): 24.0 ~ 26.0
Cr (％): 24.0 ~ 26.0
Ni (％): 17.0 ~ 23.0
Mo (％): -
Co (%): -
Co (%): -
W (%): -
Al (%): -
Al (%): -
Cu (%): -
Ti (%):
Fe (% ): Balance
N (%): 0.15 ~ 0.35
TYPICAL MECHANICAL PROPERTIES
Tensile strength, σb/≥ MPa: 580
Yield strength, σ0.2/MPa: 270
Elongation, δ ≥(％): 25.0
Reduction of area, ф ≥ (％): -
Hardness via heat treatment /HBW: 217
Reduction of area, ф ≥ (％): -
Hardness via heat treatment /HBW: 217
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 ~ 450mm
Square bar / Flat bar: 3 ~ 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.
FORMS AND SHAPES
Round bar (Diameter): 5.50 ~ 450mm
Square bar / Flat bar: 3 ~ 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.E-mail: lh.steel@hotmail.com
If you meet further on any technical enquiry, pleased to EMAIL our qualified production engineers.E-mail: lh.steel@hotmail.com
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