Astroloy
2017-06-16 11:49:20 Origin： Remark：0 Click：
Technical specifications of American high temperature alloys Astroloy datasheet, Astroloy Chemical compositions, Astroloy mechanical properties from Steelmaking, ESR melted, Blooming, Forging, Hot rolling, Heat treatment, Straightening, Ultrasonic 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.
MATERIAL TECHNICAL DATA SHEET - Grade Astroloy
OFFICIAL TEST CERTIFICATE: issued by TUV - SGS - BV
MATERIAL CATEGORY: American high temperature alloy and other special alloys
CHEMICAL COMPOSITION (mass weight %)
C (％): 0.02 ~ 0.06
Si (％): ≤ 0.40
Mn (％): ≤ 0.50
P (％)≤: 0.030
S (％)≤: 0.015
Cr (％): 14.0 ~ 15.5
Ni (％): Remainder
Mo (％): 4.80 ~ 5.50
Co (%): 14.0 ~ 16.0
Mo (％): 4.80 ~ 5.50
Co (%): 14.0 ~ 16.0
W (%): -
Al (%): ≤ 4.40
Cu (%): -
Ti (%): ≤ 3.50
Al (%): ≤ 4.40
Cu (%): -
Ti (%): ≤ 3.50
Fe (%): -
MECHANICAL PROPERTIES UNDER ROOM TEMP.
Tensile strength, σb/≥ MPa: 1241
Yield strength, σ0.2/≥ MPa: 862
Elonghation, δ ≥(％): 12.0
Reduction of area, ф ≥ (％): 11.0
Hardness | HB: HBW 369
Yield strength, σ0.2/≥ MPa: 862
Elonghation, δ ≥(％): 12.0
Reduction of area, ф ≥ (％): 11.0
Hardness | HB: HBW 369
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 treated + 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 treated + Aged
SHAPES AND DIMENSIONS
Round bar (Diameter): 5.5 to 800mm
Square bar / Flat bar: 10 to 500mm
Steel strip via cold rolled: T0.1 - 3mm X W5 - 200mm 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. -via E-mail: sales@ccsteels.com
If you meet further on any technical enquiry, pleased to EMAIL our qualified production engineers. -via E-mail: sales@ccsteels.com
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