Hastelloy N / N10003
2018-05-17 13:37:54 Origin： Remark：0 Click：
Technical specifications of American high temperature alloys Hastelloy N datasheet, Hastelloy N & N10003 Chemical compositions, Hastelloy N & N10003 mechanical properties
TECHNICAL DATA SHEET - Hastelloy Alloy N & N10003
OFFICIAL TEST CERTIFICATE: issued by TUV - SGS - BV
MATERIAL CATEGORY: Ni - Mo - Cr base Superalloy
CHEMICAL COMPOSITION (mass weight - %)
Carbon, C (％): ≤ 0.10
Silicon, Si (％): ≤ 1.00
Manganese, Mn (％): ≤ 0.80
Phosphorus, P (％) ≤: 0.040
Carbon, C (％): ≤ 0.10
Silicon, Si (％): ≤ 1.00
Manganese, Mn (％): ≤ 0.80
Phosphorus, P (％) ≤: 0.040
Sulfur, S (％) ≤: 0.030
Chromium, Cr (％): 6.00 ~ 8.00
Chromium, Cr (％): 6.00 ~ 8.00
Nickel, Ni (％): 71.0 remainder
Molybdenum, Mo (％): 14.5 ~ 18.0
Cobalt, Co (%): ≤ 0.60
Cobalt, Co (%): ≤ 0.60
Tungstren, W (%): ≤ 0.50
Aluminum, Al (%): -
Aluminum, Al (%): -
Copper, Cu (%): ≤ 0.35
Titanium, Ti (%): -
Titanium, Ti (%): -
Vanadium, V (%): ≤ 0.02
Ferrum, Fe (%): ≤ 4.00
MECHANICAL PROPERTIES UNDER ROOM TEMP.
Tensile strength, Rm ≥ MPa: 795
Yield strength, Rp0.2 / MPa: 340
Elongation, A5 ≥ (％): 45.0
Reduction of area, Z ≥ (％): -
Hardness via heat treatment /HBW: -
Reduction of area, Z ≥ (％): -
Hardness via heat treatment /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.
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 DIMENSIONS
Round bar (Diameter): 5.50 ~ 450mm
Square bar / Flat bar: 3 ~ 350mm
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.
TECHNICAL SALES ASSISTANCE
If you meet further on any technical enquiry, pleased to EMAIL (sales@ccsteels.com.) our qualified production engineers.
If you meet further on any technical enquiry, pleased to EMAIL (sales@ccsteels.com.) our qualified production engineers.
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