Inconel 686
2019-11-20 13:49:10 Origin： Remark：0 Click：
Technical specifications of American high temperature alloys Inconel 686 datasheet, Inconel 686 Chemical compositions, Inconel 686 Mechanical properties from Steelmaking, Inconel 686 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 - Grade Inconel 686
OFFICIAL TEST CERTIFICATE: issued by TUV - SGS - BV
MATERIAL CATEGORY: Nickel - Cr base Superalloy
CHEMICAL COMPOSITION (WEIGHT %)
C (％): ≤ 0.010
Si (％): ≤ 0.08
Mn (％): ≤ 0.75
P (％) ≤: 0.035
S (％) ≤: 0.015
Cr (％): 19.0 ~ 23.0
Ni (％): Balance
Si (％): ≤ 0.08
Mn (％): ≤ 0.75
P (％) ≤: 0.035
S (％) ≤: 0.015
Cr (％): 19.0 ~ 23.0
Ni (％): Balance
Mo (%): 15.0 ~ 17.0
Co (％): -
W (%): 3.00 ~ 4.40
Al (%): -
Ti (%): 0.02 ~ 0.25
Fe (%): ≤ 2.00
TYPICAL MECHANICAL PROPERTIES UNDER SOLUTION ANNEALED
Tensile strength, σb/≥ MPa: 810
Yield strength, σ0.2/MPa: 359
Elongation, δ ≥(％): 50.0
Reduction of area, ф ≥ (％): -
Hardness via heat treatment /HBW: -
Reduction of area, ф ≥ (％): -
Hardness via heat treatment /HBW: -
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 ( lh.steel@hotmail.com ) our qualified production engineers.
If you meet further on any technical enquiry, pleased to EMAIL ( lh.steel@hotmail.com ) our qualified production engineers.
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