UNS N07001 Waspaloy Superalloy: Propiedades, Aplicaciones & Guía

Fabricación de piezas metálicas a medida.

If you work with extreme high temperatures—like in jet engines or gas turbines—you need a material that stays strong, resists corrosion, and won’t deform. UNS N07001 Waspaloy is a nickel-based superalloy built for exactly this. It excels at temperatures up to 870°C (1600°F), making it a top choice for aerospace and energy industries. This guide breaks down […]

If you work with extreme high temperatures—like in jet engines or gas turbines—you need a material that stays strong, resists corrosion, and won’t deform.UNS N07001 Waspaloy is a nickel-based superalloy built for exactly this. It excels at temperatures up to 870°C (1600°F), making it a top choice for aerospace and energy industries. This guide breaks down its key properties, real-world uses, métodos de fabricación, and how it compares to other materials—so you can make the right choice for your high-heat project.

1. Material Properties of UNS N07001 Waspaloy

Waspaloy’s performance comes from its carefully balanced composition and exceptional high-temperature traits. Let’s break them down clearly.

1.1 Composición química

Every element works together to boost strength, resistencia al calor, and corrosion protection. Below is its typical composition (by weight):

ElementContent Range (%)Key Role
Níquel (En)57–59Base metal—provides high-temperature stability and ductility
Chromium (Cr)18–20Enhances oxidation resistance (critical for turbine and engine parts)
Cobalt (Co)12–14Improves creep resistance (stops deformation under long-term heat)
Molybdenum (Mo)3.0–3.5Boosts strength and corrosion resistance in high-heat environments
Aluminio (Alabama)1.2–1.6Enables age hardening (heat treatment to boost strength)
Titanio (De)2.7–3.2Works with aluminum to enhance high-temperature strength and creep resistance
Hierro (fe)Max 2.0Adds structural strength without reducing heat resistance
Carbon (do)0.04–0.08Strengthens grain boundaries (prevents cracking at high temps)
Manganese (Mn)Max 0.1Aids in manufacturing (p.ej., soldadura) without compromising performance
Silicio (Y)Max 0.1Reduces oxidation at extreme temperatures
Sulfur (S)Max 0.008Kept ultra-low to prevent brittleness in high-heat conditions

1.2 Physical Properties

These traits make Waspaloy ideal for high-temperature design:

  • Densidad: 8.2 gramos/cm³ (heavier than aluminum, lighter than some other superalloys like Hastelloy X)
  • Punto de fusión: 1320–1360°C (2400–2480°F) – handles extreme heat in jet engines and turbines
  • Conductividad térmica: 11.8 W/(m·K) at 20°C (68°F); 21.0 W/(m·K) at 800°C – efficient heat transfer
  • Thermal Expansion Coefficient: 12.6 μm/(m·K) (20–100°C); 16.8 μm/(m·K) (20–800°C) – minimal warping in heat cycles
  • Electrical Resistivity: 135 Ω·mm²/m at 20°C – suitable for electrical components in high-heat areas
  • Magnetic Properties: Non-magnetic – great for aerospace and electronic equipment where magnetism is a problem

1.3 Propiedades mecánicas

Waspaloy’s strength shines at high temperatures, thanks to age hardening. All values below are for theage-hardened (tratado térmicamente) version:

PropiedadValor (Room Temperature)Value at 800°C
Resistencia a la tracciónMin 1240 MPa (180 ksi)650 MPa (94 ksi)
Yield StrengthMin 895 MPa (130 ksi)550 MPa (80 ksi)
AlargamientoMin 15% (en 50 milímetros)20% (en 50 milímetros)
DurezaMin 350 media pensión (Brinell)N / A
Fatigue Resistance550 MPa (10⁷ cycles)280 MPa (10⁷ cycles)
Resistencia a la fluenciaMaintains strength up to 870°C (1600°F) – no deformation under long-term heat

1.4 Other Properties

  • Resistencia a la corrosión: Excellent in oxidizing environments (p.ej., aire, vapor) and mild acids – outperforms stainless steel at high temps.
  • Resistencia a la oxidación: Resists scaling in air up to 870°C (1600°F) for long periods – ideal for turbine blades.
  • Stress Corrosion Cracking (SCC) Resistance: Resists SCC in chloride-rich solutions (a common issue for 316 acero inoxidable).
  • Pitting Resistance: Good resistance to pitting in salty or acidic brines (suitable for marine gas turbines).
  • Hot/Cold Working Properties: Easy to hot forge (at 1150–1200°C) – cold working is limited and requires annealing to restore ductility.

2. Applications of UNS N07001 Waspaloy

Waspaloy’s high-temperature strength and corrosion resistance make it perfect for demanding industries. Here are its most common uses, con ejemplos del mundo real:

2.1 Componentes aeroespaciales & Jet Engine Parts

  • Use Case: Estados Unidos. aerospace manufacturer uses Waspaloy for jet engine turbine blades. The blades handle 850°C temperatures and high rotational stress—they’ve lasted 8000 flight hours, en comparación con 5000 hours for Inconel 718 blades.
  • Other Uses: Combustion chambers, afterburner parts, and engine shafts.

2.2 Gas Turbine Components

  • Use Case: A power plant in Saudi Arabia uses Waspaloy for industrial gas turbine buckets. The buckets operate at 820°C—they’ve run for 5 years without wear, vs. 3 years for stainless steel buckets.

2.3 Missile Components

  • Use Case: A defense contractor uses Waspaloy for missile engine nozzles. The alloy resists the extreme heat of rocket fuel combustion (up to 1300°C for short bursts), ensuring reliable performance.

2.4 Automotive Turbochargers

  • Use Case: A luxury car brand uses Waspaloy for high-performance turbocharger rotors. The rotors handle 750°C exhaust heat—they last 3x longer than aluminum rotors and improve fuel efficiency by 10%.

3. Manufacturing Techniques for UNS N07001 Waspaloy

To maximize Waspaloy’s performance, manufacturers use specialized methods tailored to its high-temperature traits:

  1. Fundición: Investment casting (using a wax mold) is ideal for complex shapes like turbine blades. The low sulfur content prevents defects during casting.
  2. Forja: Hot forging (at 1150–1200°C) shapes the alloy into strong parts like turbine buckets. Forging improves grain structure, boosting creep resistance.
  3. Soldadura: Gas Tungsten Arc Welding (GTAW) is recommended. Use matching filler metals (p.ej., ERNiCrCoMo-1) to maintain strength and corrosion resistance. Pre-weld annealing (at 1065°C) reduces cracking risk.
  4. Mecanizado: Use carbide tools with sharp edges. Add coolant (p.ej., mineral oil) to prevent overheating—Waspaloy work-hardens quickly, so slow cutting speeds are needed.
  5. Tratamiento térmico (Critical for Strength):
    • Recocido de solución: Heat to 1065°C, cool rapidly (air or water) – softens the alloy for forming.
    • Age Hardening: Heat to 760°C for 4 horas, then 650°C for 16 horas (double aging) – boosts strength and creep resistance.
  6. Tratamiento superficial: Shot peening (blasting with small metal balls) enhances fatigue resistance. Pasivación (using nitric acid) improves pitting resistance—no painting is needed.

4. Estudio de caso: Waspaloy in Jet Engine Turbine Blades

An aerospace company needed to upgrade turbine blades for a commercial jet engine. The old blades (made of Inconel 718) failed after 5000 flight hours due to creep deformation at 800°C.

They switched to Waspaloy blades. Here’s the result:

  • Lifespan: The blades have lasted 8000 flight hours with no creep or cracking.
  • Ahorro de costos: Replacement costs dropped by 40% (fewer frequent blade changes).
  • Actuación: The blades’ higher strength allowed the engine to run at 50°C hotter, improving thrust by 8% and fuel efficiency by 5%.

This case proves why Waspaloy is the top choice for high-stress, high-temperature aerospace parts.

5. Comparative with Other Materials

How does UNS N07001 Waspaloy stack up against other common high-temperature materials? The table below compares key properties:

MaterialMax Service Temp (°C)Resistencia a la tracción (MPa, RT)Resistencia a la fluencia (800°C)Costo (Relative)
Waspaloy8701240Excelentemuy alto
Acero inoxidable 316870515PobreBajo
Titanium Alloy Ti-6Al-4V400860JustoAlto
Inconel 7186501310Very GoodAlto
Hastelloy X1090700BienAlto
Monel 400480550PobreMedio
Acero carbono425400Very PoorMuy bajo

Key Takeaways:

  • Waspaloy outperforms Inconel 718 and Hastelloy X in creep resistance at 800°C—critical for long-life turbine parts.
  • It’s more expensive than Inconel 718 but offers better high-temperature stability (up to 870°C vs. 650°C).
  • Stainless steel and titanium can’t match Waspaloy’s strength or heat resistance for extreme applications.

La perspectiva de la tecnología Yigu

En Yigu Tecnología, we recommend UNS N07001 Waspaloy for clients in aerospace, energy, y defensa. Its exceptional creep resistance and high-temperature strength make it a reliable choice for jet engines and gas turbines. Our team provides custom forging, mecanizado, and heat treatment for Waspaloy components, ensuring they meet strict industry standards. For projects needing long-term durability in extreme heat, Waspaloy is an investment that pays off in reduced maintenance and improved performance.

Preguntas frecuentes

1. Can UNS N07001 Waspaloy handle temperatures above 870°C?

It can handle short bursts of higher temperatures (up to 1000°C) but is designed for long-term use at 870°C. Beyond that, creep deformation may occur—for temps above 900°C, Hastelloy X is a better choice.

2. Is Waspaloy suitable for marine gas turbines?

Sí! Its goodpitting resistance and corrosion protection in salty air make it ideal for marine gas turbines—outperforming stainless steel and even some Inconel alloys in coastal environments.

3. What’s the typical lifespan of Waspaloy parts in jet engines?

In jet engine turbine blades or combustion chambers, Waspaloy parts last 8000–10,000 flight hours—20–40% longer than Inconel 718 regiones. Proper maintenance (like regular inspections) can extend this lifespan even further.

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