MP35N
2016-01-29 11:52:41 Origin： Remark：0 Click：
Specifications MP35N Round bar, Peeled bright bar MP35N, AMS 5844 ESR melted, forgings, Hot rolling, Heat treatment, Cold working or machined.
TECHNICAL DATA SHEET - Alloy MP35N
MATERIAL STANDARDS - AMS 5844
OFFICIAL TEST CERTIFICATE: issued by TUV - SGS - BV
MAIN FEATURES: MP35N is an age hardenable Nickel-Cobalt base alloy that has a unique combination of properties - ultra high strength, toughness, ductility and outstanding corrosion resistance. MP35N resists corrosion in hydrogen sulphide, salt water and other chloride solutions. It also has excellent resistance to crevice and stress corrosion cracking in sea water and other hostile environments.
CHEMICAL COMPOSITION (mass weight - %)
Carbon, C (％): ≤ 0.030
Silicon, Si (％): ≤ 0.15
Manganese, Mn (％): ≤ 0.15
Phosphorus, P (％)≤: 0.015
Sulfur, S (％)≤: 0.010
Chromium, Cr (％): 19.0 ~ 21.0
Nickel, Ni (％): 33.0 ~ 37.0
Molybdenum, Mo (％): 9.00 ~ 11.0
Silicon, Si (％): ≤ 0.15
Manganese, Mn (％): ≤ 0.15
Phosphorus, P (％)≤: 0.015
Sulfur, S (％)≤: 0.010
Chromium, Cr (％): 19.0 ~ 21.0
Nickel, Ni (％): 33.0 ~ 37.0
Molybdenum, Mo (％): 9.00 ~ 11.0
Cobalt, Co (%): 34.20 ~ 36.0
Titanium, Ti (%): ≤ 1.00
Other (％): Fe ≤ 1.00
Other (％): Fe ≤ 1.00
Similar material grade: R30035
MECHANICAL PROPERTIES UNDER ROOM TEMP.
Annealed condition:
Tensile strngth, σb/≥ MPa: 800~1000
Yeild strngth, σ0.2/≥ MPa: -
Elongation, δ ≥(％): -
Elongation, δ ≥(％): -
Reduction of area, ф ≥ (％): -
Hardness | HRB: -
DENSITY: 8.43 g/cm3
WORKING TEMPERATURE: 200～315°C
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.
Heat treating fixture, Furnace muffle, Nuclear reactor.
Turbine engine parts - mechanical gears, gear shaft, main axis, blade.
Mechanical parts - bolt and nut, fastener, Gas turbine, Turbine blade, Fuel nozzle.
Heat treatment furnace flask and components, especially in the carbonization.
These materials must stand up to high heat, extreme oxidation potential and recycling.
These materials must stand up to high heat, extreme oxidation potential and recycling.
PRODUCT DESCRIPTION
The alloy is usually produced by 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 annealed condition.
Final heat treatment - solution treatment
The alloy is usually produced by 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 annealed condition.
Final heat treatment - solution treatment
FORMS AND DIMENSIONS
Round bar via hot rolled / hot forged: Diameter 5.0 ~ 300mm
Steel strip via cold rolled: T0.1 - 3mm X W5 - 200mm X L (or in coil form)
Forging piece: stepped shafts, other different shapes based on OEM.
Forging piece: stepped shafts, other different shapes based on OEM.
TECHNICAL SALES ASSISTANCE
If you meet further on any technical enquiry, pleased to EMAIL our resident team of qualified production engineers, E-mail: sales@ccsteels.com
If you meet further on any technical enquiry, pleased to EMAIL our resident team of qualified production engineers, E-mail: sales@ccsteels.com
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