Nickel Alloy 706/ Inconel 706
Technical Data Sheet
Alloy 706 (UNS N09706) is a nickel-iron-chromium. As alloy 706 is a precipitation-hardenable alloy that provides high mechanical strength in combination with good fabricability. The properties of Alloy 706 are similar to Alloy 718 however alloy 706 is more readily fabricated. The main uses of Alloy 706 are for aerospace and land base gas turbine parts and components.
Chemical Composition Limits | ||||||||||||||
Weight % | Ni+Co | Cr | Fe | Nb+Ta | Ti | Al | C | Cu | Mn | Si | S | P | B | Co |
Alloy 706 | 39.0 - 44.0 | 14.5 - 17.5 | Bal | 2.5 - 3.3 | 1.5 -2.0 | 0.40 max | 0.06 max | 0.30 max | 0.35 max | 0.35 max | 0.015 max | 0.020 max | 0.006 max | 1 max |
Typical Mechanical Properties
Material | Condition | Tensile Strength Ksi | Yield Strength Ksi | Elongation (%) |
Alloy 706 Sheet | Solution Annealed | 109.8 | 55.5 | 47 |
Availability
Alloy 706 (UNS N09706) is available in Round Bar and Forging Stock. For all stock availability contact Sales.
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