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MedicalFry Alloy X is a nickel-chromium-iron-molybdenum alloy that offers excellent oxidation resistance and strength at elevated temperatures. This product possesses good formability, weldability, and machineability. This non-magnetic alloy is typically for parts, such as turbine rotors, shafts, flanges, blades, and bolts, requiring oxidation resistance up to 2200 F (1204 C) and relatively high strength above 1500 F (816 C). Fry Alloy X is frequently used to produce jet engine components, gas turbine parts, afterburners, tailpipes, petro-chemical components, and structural components. (UNS NO6002)
Chemical Makeup
| Element | Min | Max |
|---|---|---|
| Carbon, C | 0.05 | 0.15 |
| Manganese, Mg | -- | 1 |
| Silicon, Si | -- | 1 |
| Phosphorus, P | -- | 0.04 |
| Sulfur, S | -- | 0.03 |
| Chromium, Cr | 20.5 | 23 |
| Cobalt, Co | 0.5 | 2.5 |
| Molybdenum, Mo | 8 | 10 |
| Tungsten, W | 0.2 | 1 |
| Iron, Fe | 17 | 20 |
| Boron, B (3.1.1) | -- | 0.01 |
| Aluminum, Al (3.1.1) | -- | 0.5 |
| Titanium, Ti | -- | 0.15 |
| Copper, Cu | -- | 0.5 |
Common Applications
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Aerospace
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Industrial
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Power Generation
Benefits
- Excellent Oxidation Resistance At High Temperatuies
- High Strength At High Temperatures
- Good Ductility
We stock FRY ALLOY X to the following specifications:
- AMS-5754
Click on a cross-section to see the sizes we stock: