ATI 617™ Nickel-Based Alloy
UNS N06617
ATI 617™ alloy is a solid-solution strengthened, nickel-based superalloy with excellent creep-rupture strength and oxidation resistance at temperatures over 1800F (980C). The alloy is resistant to a variety of both reducing and oxidizing media. ATI 617™ alloy is primarily used to manufacture combustion cans, inner housings, ducting, and transition liners for both aerospace and land-based gas turbines. Alloy 617 is one of the few materials covered by the ASME Boiler and Pressure Vessel Code with design stresses up to 1800F.
Product Documents
Documents
Product Specifications By Form
Plate
Composition
| Element | Minimum (weight %) | Maximum (weight %) | Typical (weight %) |
|---|
| C | 0.05 | 0.15 | |
| Mn | | 0.50 | |
| Si | | 0.50 | |
| P | | 0.015 | |
| S | | 0.015 | |
| Cr | 20.00 | 24.00 | |
| Co | 10.00 | 15.00 | |
| Mo | 8.00 | 10.00 | |
| Al | 0.80 | 1.50 | |
| Ti | &nbps; | 0.60 | |
| B | | 0.006 | |
| Fe | | 3.00 | |
| Cu | | 0.5 | |
| Ni | Balance | | |
Density
Tensile Strength
Yield Strength
Elongation
Specifications
AMS 5888, ASTM B168, ASME SB-168, DIN 17744
Composition
| Element | Minimum (weight %) | Maximum (weight %) | Typical (weight %) |
|---|
| C | 0.05 | 0.15 | |
| Mn | | 0.50 | |
| Si | | 0.50 | |
| P | | 0.015 | |
| S | | 0.015 | |
| Cr | 20.00 | 24.00 | |
| Co | 10.00 | 15.00 | |
| Mo | 8.00 | 10.00 | |
| Al | 0.80 | 1.50 | |
| Ti | &nbps; | 0.60 | |
| B | | 0.006 | |
| Fe | | 3.00 | |
| Cu | | 0.5 | |
| Ni | Balance | | |
Density
Tensile Strength
Yield Strength
Elongation
Specifications
AMS 5889, ASTM B168, ASME SB-168, DIN 17744
Contact
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