Inconel 617 / Alloy 617
2025-05-06 10:43:00 Origin： Remark：0 Click：
Technical specifications Inconel 617 Round bar, flat bar, Steelmaking, Inconel 617 ESR & VAR technique, Blooming, Hot forging, Hot rolling, Heat treatment
TECHNICAL DATA SHEET - Inconel 617
OFFICIAL TEST CERTIFICATE: issued by TUV - SGS - BV
MATERIAL CATEGORY: Ni-Cr-Co-Mo-Al Superalloy
CHEMICAL COMPOSITIONS (mass weight %)
Carbon, C (％): 0.05 ~ 0.15
Carbon, C (％): 0.05 ~ 0.15
Silicon, Si (％): ≤ 1.00
Manganese, Mn (％): ≤ 1.00
Phosphorus, P (％) ≤: 0.025
Phosphorus, P (％) ≤: 0.025
Sulfur, S (％) ≤: 0.015
Chromium, Cr (％): 20.0 ~ 24.0
Chromium, Cr (％): 20.0 ~ 24.0
Nickel, Ni (％): 44.5 min.
Molybdenum, Mo (％): 8.00 ~ 10.0
Cobalt, Co (%): 10.0 ~ 15.0
Cobalt, Co (%): 10.0 ~ 15.0
Boron, B (%): ≤ 0.006
Alunimum, Al (%): 0.80 ` 1.50
Alunimum, Al (%): 0.80 ` 1.50
Copper, Cu (%): ≤ 0.50
Titanium, Ti (%): ≤ 0.60
Niobium, Nb (%): -
Ferrum, Fe (% ): ≤ 3.00
TYPICAL MECHANICAL PROPERTIES UNDER SOLUTION ANNEALED
Tensile strength, σb ≥ MPa: 769
Yield strength, σ0.2 / MPa: 315
Elongation, δ5 ≥ (％): 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.
FORMS AND DIMENSIONS
Rod / round bar / disc (diameter): 5.50 ~ 850mm
Square bar / flat bar: 8 ~ 600mm
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.
FORMS AND DIMENSIONS
Rod / round bar / disc (diameter): 5.50 ~ 850mm
Square bar / flat bar: 8 ~ 600mm
Wire rod (diameter): 1.0 ~ 13mm
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.
Hot search：Inconel 617 / Alloy 617
Previous page：K11789
Last page：N06617 / Alloy 617
Total list
Monthly rank
- 14X6CrNiMo17-13
- 14X20CrMoWV12-1
- 13N07750 type 2
- 12Alloy 255/SD40
- 12CD4MCu
- 11ASTM B805 N07773
- 11X8CrNiMoNb16-16
- 11CE8MN
- 111.4910
- 11Nitronic 32