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TECHNICAL SPECIFICATION: ASTM B805 - 2006
OFFICIAL TEST CERTIFICATE: issued by TUV - SGS - BV
MATERIAL CATEGORY: precipitation hardening nickel alloy
CHEMICAL COMPOSITION (WEIGHT %)
C (％): ≤ 0.030
Si (％): ≤ 0.20
Mn (％): ≤ 0.20
P (％) ≤: 0.015
S (％) ≤: 0.010
Cr (％): 19.0 ~ 22.0
Ni (％): 59.0 ~ 63.0
Mo (％): 7.00 ~ 9.50
Nb (%): 2.75 ~ 4.00
Ti (%): 1.00 ~ 1.60
Al (%): ≤ 0.35
Fe (%): remainder
MECHANICAL PROPERTIES UNDER ROOM TEMPERATURE
Form: round bar and wire rod
Condition: Solution treated, 1025 Deg.
Tensile strength,σb/≥ MPa: 758
Yield strength, σ0.2/≥ MPa: 310
Elongation, δ ≥(％): 30.0
Reduction of area, ф ≥ (％): 40.0
Hardness | HRC: -
Condition: Solution + Ageing treated ( 732 Deg.for 8 hours followed by furnace cooling to 621 ~ 649 Deg. holding 8 hours, and air cooling.)
Tensile strength,σb/≥ MPa: 1137
Yield strength, σ0.2/≥ MPa: 827
Elongation, δ ≥(％): 20.0
Reduction of area, ф ≥ (％): 35.0
Hardness | HRC: -
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
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.
FORMS AND SHAPES
Round bar (Diameter): 0.20mm to 800mm
Square bar / Flat bar: 3mm to 500mm
Heavy/middle plate via hot rolled: T6 - 200mm X W1000- 2500mm X L1000-12000mm
Sheet steel via cold rolled: T0.5 - 6mm X W600- 1000mm X L1000 - 2000mm
Steel strip via cold rolled: T0.1 - 3mm X W5 - 200mm X L (or in coil form)
Forging piece: stepped shafts with flanks / discs /tubes /slugs /donuts /cubes /other different shapes based on OEM.
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