NiCr20Co18Ti
2014-09-11 09:49:24 Origin： Remark：0 Click：
Description NiCr20Co18Ti datasheet, NiCr20Co18Ti Chemical, NiCr20Co18Ti Property steelmaking, 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 - DIN NiCr20Co18Ti
High temperature high strength steel and superalloy
MATERIAL SPECIFICATIONS
DIN 17742, 17460, 17480 (2002/1992), DIN EN 103021, 10296, 10095 (2002/1999)
AVAILABLE SHAPES
Round bar / Flat bar / Square bar
Bright - peeled + polishing, centerless grinding
Forged - ring, tube, pipe casing, discs, shaft
CHEMICAL COMPOSITION (WEIGHT %)
C (％): ≤ 0.13
Si (％): ≤ 1.00
Mn (％): ≤ 1.00
P (％)≤: 0.030
S (％)≤: 0.015
Cr (％): 18.0 ~ 21.0
Ni (％): Balance
Mo (％): -
Co (％): 15.0 ~ 21.0
Al (%): 1.00 ~ 2.00
Ti (%): 2.00 ~ 3.00
Others (%): Zr ≤0.15, B ≤0.020, Fe ≤1.50, Cu ≤0.20
MECHANICAL PROPERTIES - HOT WORKING, HEAT TREATMENT AND HARDNESS
Hot forming temperature /℃: 1150～1050
Heat treatment temperature /℃ | annealing: —
Heat treatment temperature /℃ | quenching or solution: 1065 ~ 1095 air cooling
Heat treatment temperature /℃ | tempering: 685~715
Heat treatment temperature /℃ | ageing: —
Condition: precipitation hardening
Mechanical property under room temperature |σb/MPa: ≥1200
Mechanical property under room temperature |σs≥/MPa: 685
Mechanical property under room temperature |δ5≥(％): 16.5
Mechanical property under room temperature |Akv(DVM): 55
Heat stability temperature/℃: 850
Non-scale temperature in air /℃: 950
MECHANICAL PROPERTY UNDER HIGH TEMPERATURE
echanical property above 200℃ σ0.2/MPa，at following temperature /℃|200: 745
Mechanical property above 200℃ σ0.2/MPa，at following temperature /℃|300: 735
Mechanical property above 200℃ σ0.2/MPa，at following temperature /℃|400: 726
Mechanical property above 200℃ σ0.2/MPa，at following temperature /℃|500: 726
Mechanical property above 200℃ σ0.2/MPa，at following temperature /℃|600: 726
Mechanical property above 200℃ σ0.2/MPa，at following temperature /℃|700: 686
Mechanical property above 200℃ σ0.2/MPa，at following temperature /℃|800: 441
Creep rupture strength /MPa，at following time/h and temperature /℃|1000h|600: —
Creep rupture strength /MPa，at following time/h and temperature /℃|1000h|700: 373
Creep rupture strength /MPa，at following time/h and temperature /℃|1000h|800: 117
Creep rupture strength /MPa，at following time/h and temperature /℃|1000h|900: 39
Creep rupture strength /MPa，at following time/h and temperature /℃|10000h|600: —
Creep rupture strength /MPa，at following time/h and temperature /℃|10000h|700: 294
Creep rupture strength /MPa，at following time/h and temperature /℃|10000h|800: 98
Creep rupture strength /MPa，at following time/h and temperature /℃|10000h|900: —
Creep rupture strength /MPa，at following time/h and temperature /℃|100000h|600: —
Creep rupture strength /MPa，at following time/h and temperature /℃|100000h|700: 206
Creep rupture strength /MPa，at following time/h and temperature /℃|100000h|800: 49
Creep rupture strength /MPa，at following time/h and temperature /℃|100000h|900: —
High temperature high strength steel and superalloy
MATERIAL SPECIFICATIONS
DIN 17742, 17460, 17480 (2002/1992), DIN EN 103021, 10296, 10095 (2002/1999)
AVAILABLE SHAPES
Round bar / Flat bar / Square bar
Bright - peeled + polishing, centerless grinding
Forged - ring, tube, pipe casing, discs, shaft
CHEMICAL COMPOSITION (WEIGHT %)
C (％): ≤ 0.13
Si (％): ≤ 1.00
Mn (％): ≤ 1.00
P (％)≤: 0.030
S (％)≤: 0.015
Cr (％): 18.0 ~ 21.0
Ni (％): Balance
Mo (％): -
Co (％): 15.0 ~ 21.0
Al (%): 1.00 ~ 2.00
Ti (%): 2.00 ~ 3.00
Others (%): Zr ≤0.15, B ≤0.020, Fe ≤1.50, Cu ≤0.20
MECHANICAL PROPERTIES - HOT WORKING, HEAT TREATMENT AND HARDNESS
Hot forming temperature /℃: 1150～1050
Heat treatment temperature /℃ | annealing: —
Heat treatment temperature /℃ | quenching or solution: 1065 ~ 1095 air cooling
Heat treatment temperature /℃ | tempering: 685~715
Heat treatment temperature /℃ | ageing: —
Condition: precipitation hardening
Mechanical property under room temperature |σb/MPa: ≥1200
Mechanical property under room temperature |σs≥/MPa: 685
Mechanical property under room temperature |δ5≥(％): 16.5
Mechanical property under room temperature |Akv(DVM): 55
Heat stability temperature/℃: 850
Non-scale temperature in air /℃: 950
MECHANICAL PROPERTY UNDER HIGH TEMPERATURE
echanical property above 200℃ σ0.2/MPa，at following temperature /℃|200: 745
Mechanical property above 200℃ σ0.2/MPa，at following temperature /℃|300: 735
Mechanical property above 200℃ σ0.2/MPa，at following temperature /℃|400: 726
Mechanical property above 200℃ σ0.2/MPa，at following temperature /℃|500: 726
Mechanical property above 200℃ σ0.2/MPa，at following temperature /℃|600: 726
Mechanical property above 200℃ σ0.2/MPa，at following temperature /℃|700: 686
Mechanical property above 200℃ σ0.2/MPa，at following temperature /℃|800: 441
Creep rupture strength /MPa，at following time/h and temperature /℃|1000h|600: —
Creep rupture strength /MPa，at following time/h and temperature /℃|1000h|700: 373
Creep rupture strength /MPa，at following time/h and temperature /℃|1000h|800: 117
Creep rupture strength /MPa，at following time/h and temperature /℃|1000h|900: 39
Creep rupture strength /MPa，at following time/h and temperature /℃|10000h|600: —
Creep rupture strength /MPa，at following time/h and temperature /℃|10000h|700: 294
Creep rupture strength /MPa，at following time/h and temperature /℃|10000h|800: 98
Creep rupture strength /MPa，at following time/h and temperature /℃|10000h|900: —
Creep rupture strength /MPa，at following time/h and temperature /℃|100000h|600: —
Creep rupture strength /MPa，at following time/h and temperature /℃|100000h|700: 206
Creep rupture strength /MPa，at following time/h and temperature /℃|100000h|800: 49
Creep rupture strength /MPa，at following time/h and temperature /℃|100000h|900: —
PRODUCT DESCRIPTION
The alloy is usually produced by AOD/VIM/VOD followed by electroslag refining (ESR) if necessary for special purpose.
Bars and, where applicable, forgings are subjected to ultrasonic examination based on the different level according to the buyers' requirements.
Bars are usually supplied bright in the solution annealing condition.
Final heat treatment - heat treatment / QT / solution treatment.
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.
Gas turbine
Turbine blade
Fuel nozzle
Heat treating fixture
Furnace muffle
Nuclear reactor
Turbine engine parts - mechanical gears, gear shaft, main axis, blade
Mechanical parts - bolt and nut, fastener
Heat treatment furnace flask and components, especially in the carbonization.
These materials must stand up to high heat, extreme oxidation potential and recycling.
PRODUCT PROFILE & FORMS
Round bar / Wire rod (Diameter): 5.5mm to 600mm
Square bar / Flat bar: 3mm to 1000mm
Plate / Sheet steel / Steel strip: 0.5mm to 1000mm
Width: 8mm to 1200mm
Length: random length or based on the customer's special requirement.
Forged steel shape: stepped shafts with flanks / discs /tubes /slugs /donuts /cubes /other different shapes based on OEM.
TECHNICAL SALES ASSISTANCE
If you meet further on any technical enquiry. pleased to email or call our resident team of qualified production engineers, E-mail: sales@ccsteels.com
The alloy is usually produced by AOD/VIM/VOD followed by electroslag refining (ESR) if necessary for special purpose.
Bars and, where applicable, forgings are subjected to ultrasonic examination based on the different level according to the buyers' requirements.
Bars are usually supplied bright in the solution annealing condition.
Final heat treatment - heat treatment / QT / solution treatment.
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.
Gas turbine
Turbine blade
Fuel nozzle
Heat treating fixture
Furnace muffle
Nuclear reactor
Turbine engine parts - mechanical gears, gear shaft, main axis, blade
Mechanical parts - bolt and nut, fastener
Heat treatment furnace flask and components, especially in the carbonization.
These materials must stand up to high heat, extreme oxidation potential and recycling.
PRODUCT PROFILE & FORMS
Round bar / Wire rod (Diameter): 5.5mm to 600mm
Square bar / Flat bar: 3mm to 1000mm
Plate / Sheet steel / Steel strip: 0.5mm to 1000mm
Width: 8mm to 1200mm
Length: random length or based on the customer's special requirement.
Forged steel shape: stepped shafts with flanks / discs /tubes /slugs /donuts /cubes /other different shapes based on OEM.
TECHNICAL SALES ASSISTANCE
If you meet further on any technical enquiry. pleased to email or call our resident team of qualified production engineers, E-mail: sales@ccsteels.com
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