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Inconel Alloys

Alloy 718 is a high strength nickel base superalloy used for cryogenic temperatures up to long term service at 1200°F. The alloy is readily fabricated and may be welded in either the annealed or precipitation (age) hardened condition. Anneal 1700 -1850°F, air cool or faster. Age 1325°F 8 hours, furnace cool to hold at 1150°F, for a total aging time of 18 hours, air cool. Alloy 718 will show a contraction of 0.0008 inch/inch after precipitation hardening

Specifications :
UNS N07718, Werkstoff 2.4668, EN 2.4668
ASTM: B 637, B 670
ASME: SFA-5.14,ASME Case 2222-1
AMS 5596,AMS 5662, AMS 5663, AMS 5832
GE B50TF14, GE B50TF15

718 Alloy Inventor :
Plate, Sheet, Coil,Bar & Welding Products

Common Trade Names :
Alloy 718, Inconel 718, Nickel 718

Chemical Composition, %

  Ni+Co Cr Cb+Tap Mo Ti Al Co C Mn Si P S B Cu Fe
MIN 50.0 17.00 4.75 2.80 0.65 0.20 - - - - - - - - -
MAX 55.0 21.00 5.50 3.30 1.15 080 1.00 0.08 .035 0.35 0.015 0.015 0.006 0.30 Balance

Features :

  • Good mechanical properties: tensile, fatigue and creep-rupture
  • Excellent welding characteristics, resistant to postweld age cracking
  • Oxidation resistant throughout its useful temperature range

Applications :

  • Gas turbine engine parts
  • Liquid fuel rocket motor components
  • Springs, fasteners
  • Cryogenic tanks

Physical Properties :

Density: 0.296 lb/in3 annealed, 0.274 lb/in3 aged
Melting Point: 2410 - 2540°F

Temperature, °F -320 70 200 400 600 1000 1200 1400
Coefficient* of Thermal Expansion, in/in°F x 10-6   5.9 - 7.3 7.5 7.7 8.1 8.4 8.9
Thermal Conductivity
Btu • ft/ft2 • hr • °F
- 6.4 7.2 8.2 9.3 11.3 12.3 13.3
Modulus of Elasticity, Dynamic psi x 106 - 29 28 27 26 25 24 22

Mechanical Properties :
Typical Room Temperature Properties, 1800°F Annealed Condition

Ultimate tensile strength, ksi  135
0.2% yield strength, ksi  70
Elongation, %  45
Hardness, Rockwell C  100

Average Tensile Properties, ½" Bar Annealed 1800°F, Aged 1325/1150°F

Temperature, °F 70 400 800 1000 1200 1400
Ultimate Tensile Strength, ksi 210 198 191 185 168 111
0.2% Yield Strength, ksi 175 163 156 155 149 110
Elongation, % 22 20 19 18 19 27
Hardness, Rockwell C 42 - 44 - - 40 - 41 40 - 41 33 - 34

Typical Stress Rupture, Bar, Annealed 1800°F, Aged 1325/1150°F

Temperature, °F 1100 1200 1300 1400
100 Hours, ksi 170 110 75 44
1,000 Hours, ksi 130 85 55 25

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Inconel 750

Alloy X-750 is a nickel chromium alloy similar to Alloy 600 but made precipitation hardenable by additions of aluminum and titanium. It has goodresistance to corrosion and oxidation along with high tensile and creep-rupture properties at temperatures to 1300°F. Its excellent relaxation resistance is useful for high temperature springs and bolts. Used in gas turbines, rocket engines, nuclear reactors, pressure vessels, tooling, and aircraft structures.

Common Trade Names :
Inconel 625, Alloy 625, Nickel 625

Inventory :
X-750 Sheet

Specifications :
UNS: N07750 W. Nr./EN: 2.4669 ASTM: B 637 NACE: MR0175 ISO: 15156-3

Chemical Composition, %

Ni Cr C Mn Cu Si S Fe
MIN 70.00 14.00 -- -- -- -- -- 5.00
MAX -- 17.00 0.08 1.00 0.50 0.50 0.01 9.00

Features :

  • Good mechanical properties at high temperatures
  • Good formability
  • Good oxidation resistance

Applications :

  • Oil and gas production
  • Gas turbine engines
  • Nuclear engineering

Physical Properties :

Density: 0.299 lb/in3
Melting Point: 2540- 2600°F
Poisson's Ratio: 0.30
Electrical Resistivity: 731 Ohm-circ mil/ft

Temperature, °F 68 392 752 800 1000 1112
Coefficient* of Thermal Expansion, in/in°F x 10-6 - 7.1 7.7 9.2 10.1 8.3
Thermal Conductivity
Btu • ft/ft2 • hr • °F
6.8 -- -- -- -- --
Modulus of Elasticity, Dynamic psi x 106 32.1 30.5 28.6 23.9 20.3 26.2

* 70°F to indicated temperature.

Mechanical Properties :

Minimum Specified Properties, ASTM A 240

Ultimate Tensile Strength, ksi 120
0.2% Yield Strength, ksi 60
Elongation, % 30
Hardness MAX, Brinell --

Typical Tensile & Impact Properties, Bar ¾ equalized and precipitation treated hot-rolled, 1625°F 24 hours, AC + 1300°F for 20 hours, AC

Temperature,°F 600 800 1000 1100 1200 1350 1500
Ultimate Tensile Strength, ksi 169.0 166.0 163.5 159.0 143.0 107.0 65.4
0.2% Yield Strength, ksi 116.5 114.0 115.0 112.0 110.0 98.3 64.7

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Inconel 600

600 alloy is a nickel-base alloy with excellent carburization, and good oxidation resistance at elevated temperatures. The alloy has long been used in the heat treating industry for many of the same applications as RA330®. 600 alloy has useful resistance to dry Cl2 and HCl gases at moderately elevated temperatures. 600 alloy is not suggested for use at red heat when sulfur is present due to elevated nickel quantities.

Grades 200 and 201 nickel are normally preferred for handling concentrated, high temperature caustic. However, when sulfur compounds are present as well, or for ammonium hydroxide service, 600 alloy is suggested. 600 alloy is subject to stress corrosion cracking in hot, concentrated caustic alkalies. To avoid stress corrosion cracking, the 600 alloy fabrication should be fully stress relieved prior to use. A minimum treatment of 1650°F for 1 hour is suggested, but 1800-1850°F for 1 hour preferred.

Specifications :

UNS N06600, Werkstoff 2.4816, EN 2.4816
AMS 5540, AMS 5665
ASTM B 166, ASTM B 167
ASME SB-166, ASME SB-167, ASME SB-168

Inventory :

Alloy 600 Plate, Alloy 600 Sheet, Alloy 600 Coil, Alloy 600 Bar, Alloy 600 Welding Products

Common Trade Names :

Alloy 600, Inconel 600, Nickel 600

Chemical Composition, %

Ni Cr C Mn Cu Si S Fe
MIN 72.00 14.00 -- -- -- -- -- 6.00
MAX 17.00 0.15 1.00 0.50 0.50 0.015 10.00

Features :

  • Virtually immune to chloride ion stress corrosion cracking
  • Good caustic corrosion resistance
  • Resistant to dry Cl2 to about 1000°F
  • Oxidation resistance to 2000°F
  • Carburization resistance

Applications :

  • Heat treating muffles and retorts
  • Vacuum furnace fixtures
  • Chlorination equipment to 1000°F
  • Titanium dioxide plants

Physical Properties :

Density: 0.304 lb/in3
Melting Point: 2470- 2575°F
Poisson's Ratio: 0.29
Electrical Resistivity: 620 Ohm-circ mil/ft

Temperature, °F 70 1000 1200 1400 1600 2000
Coefficient* of Thermal Expansion, in/in°F x 10-6 - 8.4 8.6 8.7 9.1 9.3
Thermal Conductivity
Btu • ft/ft2 • hr • °F
8.6 13.2 14.3 13.0 16.7 -
Modulus of Elasticity, Dynamic psi x 106 30.0 25.6 24.5 23.6 22.2 20.4
* 70°F to indicated temperature.

Mechanical Properties
Representative Tensile Properties

Temperature,°F 70 1000 1200 1400 1600 1800
Ultimate Tensile Strength, ksi 93 84 65 27.5 15 7.5
0.2% Yield Strength, ksi 37 28.5 26.5 17 9.0 4.0
Charpy Impact V-notch, ft-lbs 45 47 39 46 80 118

Static Corrosion in Molten Caustic Soda :
Corrosion Rate, Mils Per Year

Temperature, °F 750 932 1076 1256
Alloy 201 0.9 1.3 2.5 37.8
Alloy 400 1.8 5.1 17.6 -
Alloy 600 1.1 2.4 5.1 66.4

Inconel 625

Alloy 625 is used both for its high strength and outstanding aqueous corrosion resistance. The strength of alloy 625 is primarily a solid solution effect from molybdenum and columbium. Alloy 625 has excellent weldability and is frequently used to weld AL-6XN® alloy. Matching filler metals are also used to join dissimilar metals.

Specifications :

UNS N06625, Werkstoff 2.4856, EN 2.4856ASTM B 443 Gr 1, ASTM B 446 Gr 1ASME SB-443 Gr 1, ASME SB-446 Gr 1, ASME SFA-5.14, ASME Sect. IX P No. 43NACE MR0175-3, ISO 15156-3AMS 5599, ASM 5666, ASM 5837

Inventory :

Alloy 625 Plate, Alloy 625 Sheet, Alloy 625 Coil, Alloy 625 Bar, Alloy 625 Welding Products

Common Trade Names :

Inconel 625, Alloy 625, Nickel 625

Chemical Composition, %

Cr Ni Mo Co Cb+Ta Al Ti C Fe Mn Si P S
MIN 20.0 - 8.0 - 3.15 - - - - - - - -
MAX 23.0 Balance 10.0 1.0 4.15 0.4 0.4 0.1 5.0 0.5 0.5 0.015 0.015

Features :

  • High creep-rupture strength
  • Oxidation resistant to 1800°F
  • Good fatigue resistance
  • Excellent weldability
  • Outstanding resistance to chloride pitting and crevice corrosion
  • Immune to chloride ion stress corrosion cracking
  • Resistant to seawater under both flowing and stagnant conditions and under fouling

Applications :

  • Aircraft ducting systems
  • Jet engine exhaust systems
  • Engine thrust-reverser systems
  • Bellows and expansion joints
  • Turbine shroud rings
  • Flare stacks
  • Seawater components
  • Chemical process equipment handling mixed acids both oxidizing and reducing.

Physical Properties :

Density: 0.305 lb/in3
Melting Point: 2350-2460°F

Temperature, °F 70 400 600 800 1000 1200 1400 1600
Coefficient* of Thermal Expansion, in/in°F x 10-6 - 7.3 7.4 7.6 7.8 8.2 8.5 8.8
Thermal Conductivity
Btu • ft/ft2 • hr • °F
5.7 7.2 8.2 9.1 10.1 11.0 12.0 13.2
Modulus of Elasticity, Dynamic psi x 106 30 28 28 27 26 24 23 -

* 70°F to indicated temperature.

Mechanical Properties

Representative Tensile Properties, Bar

Temperature,°F 70 400 600 800 1000 1200 1400 1600
Ultimate Tensile Strength, ksi 144 134 132 132 130 119 78 40
0.2% Yield Strength, ksi 84 66 63 61 61 60 59 39
Elongation, % 44 45 42.5 45 48 34 59 117

Typical Rupture Strength Bar, Stress to Rupture at Indicated Time

Temperature, °F 1200 1300 1400
100 Hours, ksi 59 34 18
1,000 Hours, ksi 43 23 12

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Inconel 825


These inconel 825, alloy 825 and incoloy 825 available in various forms like seamless , bar, wire, sheet, plate,, round bar, like inconel 825 etc.

Wide range of alloy 825 is round bar.

Chemical Analysis of ALLOY 825 (UNS N08825) :
Common Names : Incoloy 825®, Nickelvac® 825, Nicrofer® 4221

C MN P S Si Cr Ni Mo Cu Co Cb+Ta Ti Al Fe Other Other
.05 max 1.0 max .03 max .5 max 19.5 – 23.5 38.0 – 46.0 2.5 – 3.5 1.5 – 3.0 0.6 1.2 0.2 max 22.0 min

Specifications :

Inconel 825 Sheet / Plate Inconel 825 Round Bar Inconel 825 Pipe Inconel 825 Tube Inconel 825 Fittings Inconel 825 Forgings
ASME SB-424 ASME SB-425 ASME SB-423 ASME SB-829 ASME SB-705 ASME SB-775 ASME SB-163 ASME SB-704 ASME SB-751 ASME SB-366 ASME SB-564

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