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Inconel 718 (UNS N07718) Nickel Alloy Plate
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Product Description
Inconel 718 comprises of nickel-chromium, along with niobium and molybdenum, offering heat treatment-derived high strength, exceptional corrosion resistance, formability and weldability, plus resistance to strain age cracking, up to 700ºC.
Inconel 718 (UNS N07718) Nickel Alloy Applications
- Chemical processing
- Aerospace
- Liquid fuel rocket motor components
- Pollution-control equipment
- Nuclear reactors
- Cryogenic storage tanks
- Valves, fasteners, springs, mandrels, tubing hangers
- Well head completion equipment and blow out preventers (BOP's)
- Gas turbine engine parts
Inconel 718 Nickel Alloy Standards
- UNS N07718
- ASTM B637, ASTM B670
- AMS 5596, AMS 5662, AMS 5663, AMS 5832
- ASME Case 2222-1, SFA 5.14
- NACE MR0175
- EN 2.4668, Werkstoff 2.4668
- GE B50TF14, B50TF15
- Other common names: Alloy 718, Haynes 718, Nicrofer 5219, Allvac 718, Altemp 718
Inconel 718 Nickel Alloy Chemical Composition %
Inconel 718 Nickel Alloy Mechanical Properties
Inconel 718 (UNS N07718) Nickel Alloy Characteristics
- Good mechanical properties - tensile, fatigue and creep-rupture
- Yield tensile strength, creep, and rupture strength properties are exceedingly high
- Highly resistant to chloride and sulfide stress corrosion cracking
- Resistant to aqueous corrosion and chloride ion stress corrosion cracking
- High temperature resistant
- Age-hardenable with a unique property of slow aging response that permits heating and cooling during annealing without the danger of cracking.
- Excellent welding characteristics, resistant to postweld age cracking
- Available Sizes And Specifications
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