Inconel 625 Plate Disc To Astm B 443 Gr.Uns No. 6625 Gr 2, Size : 290 Mm X 40 Mm

Product Overview

Description

Inconel 718 is a nickel-chromium and age-hardenable alloy that brings in high strength against creep rupture when exposed to high temperatures close to 700^oC or 1300^oF. This alloy can also be fabricated into various complex components.

Its welding features, especially the resistance to cracking post welding, are deemed outstanding by the manufacturing community. When combined with fatigue, tensile, as well as rupture strength, this alloy has a wide-scale application. These alloy sheets are used for rings, fueled rockets, casings, as well as aircraft parts.

 

Common Names:

 

 

• UNS N07718


• Alloy 718


• DIN W. Nr. 2.4668

 

 

Executive Standards:

Plate, Sheet, and Coil

 

• ASME SB 670


• ASTM B 670


• B50TF14


• AMS 5596


• UNS N07718

 

Round Bar:

 

• AMS 5662


• B50809D


• UNS N07718


• B50TF15


• ASTM B 637


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Chemical Properties:

 

Chromium (%)	17.00 to 21.00
Nickel + Cobalt (%)	50.00 to 55.00
Columbium + Tantalum (%)	4.75 to 5.50
Molybdenum (%)	2.80 to 3.30
Aluminum (%)	0.20 to 0.80
Titanium (%)	0.65 to 1.15
Cobalt (%)	1.00 Maximum
Manganese (%)	0.35 Maximum
Carbon (%)	0.80 Maximum
Silicon (%)	0.35 Maximum
Sulfur (%)	0.015 Maximum
Phosphorus (%)	0.015 Maximum
Copper (%)	0.30 Maximum
Boron (%)	0.006 Maximum
Iron (%)	Balance

 

 

Mechanical Properties:

 

 

Yield Strength	Ksi	60 Minimum
	Mpa	414 Minimum
Tensile Strength	Ksi	120 Minimum
	Mpa	827 Minimum
Elongation	%	30

 Physical Properties:

Density	Lbs/in3	0.296
	g/cm3	8.19
Specific Heat	Btu/lb °F	0.104
	J/kg °C	435
Thermal Expansion (Mean Coefficient)	in/in/°	7.6 X 10
	mm/m/°C	13.0
Elasticity Modulus	Ksi	29.7 X 103
	Mpa	204.9 X 103
Magnetic Permeability	Oersteds	200
Annealed	–	1.013
Annealed + Aged	–	1.011
Melting Range	oF	2300 to 2437
	oC	1260 to 1336