Inconel 617 / Alloy 617
2019-08-15 09:21:46 Origin： Remark：0 Click：
Technical specifications of American high temperature alloys Inconel 617 datasheet, Inconel 617 Chemical compositions, Inconel 617 mechanical properties from Steelmaking, Inconel 617 ESR & VAR technique, 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 - Inconel 617
OFFICIAL TEST CERTIFICATE: issued by TUV - SGS - BV
MATERIAL CATEGORY: Ni-Cr-Co-Mo-Al Superalloy
CHEMICAL COMPOSITION (WEIGHT %)
C (％): 0.05 ~ 0.15
C (％): 0.05 ~ 0.15
Si (％): ≤ 1.00
Mn (％): ≤ 1.00
P (％)≤: 0.025
P (％)≤: 0.025
S (％)≤: 0.015
Cr (％): 20.0 ~ 24.0
Cr (％): 20.0 ~ 24.0
Ni (％): 44.5 min.
Mo (％): 8.00 ~ 10.0
Co (%): 10.0 ~ 15.0
Co (%): 10.0 ~ 15.0
B (%): ≤ 0.006
Al (%): 0.80 ` 1.50
Al (%): 0.80 ` 1.50
Cu (%): ≤ 0.50
Ti (%): ≤ 0.60
Nb (%): -
Fe (% ): ≤ 3.00
TYPICAL MECHANICAL PROPERTIES UNDER SOLUTION ANNEALED
Tensile strength, σb/≥ MPa: 769
Yield strength, σ0.2/MPa: 315
Elongation, δ ≥(％): 50.0
Reduction of area, ф ≥ (％): 50.0
Hardness via heat treatment /HBW: 181
Reduction of area, ф ≥ (％): 50.0
Hardness via heat treatment /HBW: 181
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.
AVAILABLE FORMS AND SHAPES
Round bar (Diameter): 5.50 ~ 450mm
Square bar / Flat bar: 3 ~ 350mm
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.
AVAILABLE FORMS AND SHAPES
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.
Other sizes can be supplied to meet specific requirements.
TECHNICAL SALES ASSISTANCE
If you meet further on any technical enquiry, pleased to EMAIL our qualified production engineers.
If you meet further on any technical enquiry, pleased to EMAIL our qualified production engineers.
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