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- 4J343(4J43)
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- 4J350(4J50)
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Haynes Alloys Bar Haynes 214
Overview
Haynes 214 is a nickel-chromium-aluminum-iron alloy with additions of yttrium, optimized for extreme high-temperature stability.
Limiting Chemical Composition, %
Nickel...........................................................................................................................................75.0-80.0
Chromium............................................................................................................................................16.0
Aluminum..............................................................................................................................................4.5
Iron.........................................................................................................................................................3.0
Yttrium (Y): Trace amounts (enhances oxide layer adhesion and spallation resistance).
Key Properties
● Ultra-High Temperature Resistance:
Retains strength and oxidation resistance up to 1200°C (2200°F).
Stable Al₂O₃ scale resists spalling due to yttrium’s “anchor” effect.
● Mechanical Performance:
Excellent creep resistance under prolonged stress at high temperatures.
Good thermal fatigue resistance for cyclic heating/cooling applications.
● Corrosion Resistance:
Performs well in oxidizing, carburizing, and nitriding atmospheres (e.g., industrial furnaces).
Fabrication and Processing
● Forming:
Bars are typically produced via hot working (forging, rolling) and supplied in annealed condition (AMS 5877).
● Machining:
Challenging due to high work-hardening rates; use rigid setups, sharp carbide tools, and low-speed/high-feed techniques.
Coolants are recommended to manage heat generation.
● Heat Treatment:
Solution annealing at 1120–1175°C (2050–2150°F) followed by rapid cooling to optimize microstructure.
● Welding:
Compatible with TIG (GTAW) and resistance welding. Post-weld annealing reduces residual stresses.
Applications:
● Aerospace:
Turbine engine components (combustors, seals), structural parts in high-heat zones.
● Industrial:
Furnace fixtures (racks, rails, radiant tubes).
Heat exchangers, burner nozzles, and pyrolysis equipment.
● Energy:
Components in gas turbines and nuclear reactors.
Comparisons:
● vs. Inconel 601/625: Superior oxidation resistance above 1000°C due to Al/Y-enhanced oxide layer.
● vs. Haynes 230: Better resistance to carburization but lower intermediate-temperature strength.
● vs. Nickel 201: Far higher temperature capability but less ductility at room temperature.
Standards and Specifications
● AMS 5877: Aerospace Material Specification for Haynes 214 bar stock.
● ASTM B408: Standard for nickel-alloy bars and forgings (general guidance).
Key Considerations
● Cost: High due to nickel and yttrium content; justified in mission-critical applications.
● Thermal Stability: Avoid prolonged exposure to 650–870°C (1200–1600°F), where sigma phase formation could embrittle the alloy.
● Surface Finish: Grinding or pickling may be required post-machining to remove surface oxides.
Conclusion:
Haynes 214 alloy bar is engineered for extreme environments demanding unmatched oxidation resistance, thermal stability, and mechanical integrity. Its niche lies in aerospace and industrial systems operating at ultra-high temperatures, where most alloys degrade rapidly. While challenging to machine, its performance in harsh conditions makes it a premium choice for critical high-heat applications.
Available Forms
We provide you with a variety of product forms, including but not limited to
● Strip & Foil
● Round Wire &Flat Wire
● Bar & Rod
● Electrothermal Strip
● Flange & Ring
● Wire & Welding
● Reststance Wire
● Electric Alloy Wire
● Electric Furnace Bar
● Customize
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