| Categories | Inconel Alloy |
|---|---|
| Brand Name: | HUONA |
| Model Number: | Inconel 718 |
| Certification: | ISO9001 |
| Place of Origin: | CHINA |
| MOQ: | 5 |
| Price: | Bargain |
| Payment Terms: | T/T,Western Union,MoneyGram,L/C |
| Supply Ability: | 500 Tons Per Month |
| Delivery Time: | 5-21DAYS |
| Packaging Details: | Spool Package With Carton Box, Coil Package With Polybag |
| Material:: | Ni Cr Fe |
| Magnetic Permeability:: | 1.0011 |
| Density:: | 8.19 |
| Condition:: | Hard / Soft |
| Delivery Time:: | 7-50 Days |
| Melting Point:: | 1260 - 1336℃ |
| Curie Temperature:: | -112 °C |
| Sureface:: | Bright,Oxided |
| Tensile Strength:: | 760-1600MPA |
| Specific Heat Capacity:: | 0.435 J/g-°C |

Inconel Alloy 718 is a precipitation hardenable nickel-based alloy designed to display exceptionally high yield, tensile and creep-rupture properties at temperatures up to 1300°F. The sluggish age-hardening response of alloy 718 permits annealing and welding without spontaneous hardening during heating and cooling. This alloy has excellent weldability when compared to the nickel-base superalloys hardened by aluminum and titanium. This alloy has been used for jet engine and high-speed airframe parts such as wheels, buckets, spacers, and high temperature bolts and fasteners.
| Element | Limiting Chemical Composition (%) |
| Nickel (plus Cobalt) | 50%-55% |
| Chromium | 17%-21% |
| Niobium (plus Tantalum) | 4.75%-5.50% |
| Molybdenum | 2.80%-3.30% |
| Titanium | 0.65%-1.15% |
| Aluminum | 0.20%-0.80% |
| Cobalt | 1% max |
| Carbon | 0.08% max |
| Manganese | 0.35% max |
| Silicon | 0.35% max |
| Phosphorus | 0.015% max |
| Sulfur | 0.015% max |
| Boron | 0.006% max |
| Copper | 0.30% max |
| Iron | Balance* |
The applications of Inconel 718 round bars include:
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