Hastelloy C-276 / N10276
2017-12-12 08:44:26 Origin： Remark：0 Click：
Technical specifications of American high temperature alloys Hastelloy C-276 / N10276 datasheet, Hastelloy C-276 Chemical compositions, Hastelloy C-276 mechanical properties from Steelmaking, ESR & VAR technique, Blooming, N10276 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 - Hastelloy Alloy C-276 & N10276
OFFICIAL TEST CERTIFICATE: issued by TUV - SGS - BV
MATERIAL CATEGORY: Cr - Ni - Mo - W alloy
CHEMICAL COMPOSITION (WEIGHT %)
C (％): ≤ 0.020
Si (％): ≤ 0.08
Mn (％): ≤ 1.00
P (％)≤: 0.025
C (％): ≤ 0.020
Si (％): ≤ 0.08
Mn (％): ≤ 1.00
P (％)≤: 0.025
S (％)≤: 0.010
Cr (％): 14.0 ~ 16.5
Cr (％): 14.0 ~ 16.5
Ni (％): Remainder
Mo (％): 15.0 ~ 17.0
Co (%): ≤ 2.50
Co (%): ≤ 2.50
W (%): 3.00 ~ 4.50
Al (%): -
Al (%): -
Cu (%): -
Ti (%): -
Ti (%): -
Fe (%): 1.00 ~ 4.70
V (%): ≤ 0.35
MECHANICAL PROPERTIES UNDER ROOM TEMP.
Tensile strength, σb/≥ MPa: 785
Yield strength, σ0.2/≥ MPa: 369
Elongation, δ ≥(％): 59.0
Reduction of area, ф ≥ (％): -
Hardness via annealing | HBW: -
Reduction of area, ф ≥ (％): -
Hardness via annealing | 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.
FORMS AND SHAPES
Round bar (Diameter): 5.50 ~ 550mm
Square bar / Flat bar: 3 ~ 450mm
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 ~ 550mm
Square bar / Flat bar: 3 ~ 450mm
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.
TECHNICAL SALES ASSISTANCE
If you meet further on any technical enquiry, pleased to EMAIL our qualified production engineers.
If you meet further on any technical enquiry, pleased to EMAIL our qualified production engineers.
- Email: lh.steel@hotmail.com
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