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 Cold Rolled |
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.
Specifications
UNS N09706
AMS 5701
AMS 5702
AMS 5703
Inconel 706 (tradename)
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Disclaimer
Every effort is made to ensure that technical specifications are accurate. However, technical specifications included herein should be used as a guideline only. All specifications are subject to change without notice.
