Inconel 600-2

MAR-M509 Cobalt-base Superalloy

Manufacture Ultra-high Purity Superalloy By Vacuum Induction Melting (VIM)

MAR-M 509 is among the most widely deployed and thoroughly characterized cast Cobalt-base Superalloys for turbine applications, particularly suited to turbine vanes requiring a balanced combination of high-temperature strength, thermal fatigue resistance and superior oxidation resistance.

Mar M509 Alloy Introduction

Mar M509 is among the most widely deployed and thoroughly characterized cast cobalt-base superalloys for turbine applications, particularly suited to turbine vanes requiring a balanced combination of high-temperature strength, thermal fatigue resistance and superior oxidation resistance.

Cobalt constitutes the balance of the alloy at approximately 55 wt%, while chromium (21.5–23.5 wt%) delivers primary protection against oxidation and hot corrosion. Its designation CoCr24Ni10WTaZrB reflects a nickel addition (~10 wt%) for enhanced ductility. Additional alloying elements including tungsten, tantalum, zirconium and boron work collectively to achieve strengthening via carbide and boride precipitates.

Tantalum (~3.5 wt%) reacts with carbon (~0.6 wt%) to form MC-type carbides dispersed throughout the cast microstructure. Boron (~0.1 wt%) and zirconium (~0.5 wt%) improve grain boundary strength and hot-cracking resistance. Extensive academic studies have been conducted on the structural stability of MARM 509. Accordingly, its machinability is well established among manufacturing shops routinely machining cast cobalt superalloys.

Mar M509 Chemical Composition

Mar-M509 is a high-strength, cobalt-based cast superalloy designed for extreme high-temperature environments up to 1050 °C.

Tungsten,W 6.50-7.50%

Chromium, Cr 23.0-24.25%

Tantalum,Ta 3.00-4.00%

Phosphorus,P ≤0.015%

Carbon,C 0.55-0.65%

Zirconium,Zr 0.30-0.50%

Titanium, Ti 0.15-0.25%

Boron,B 0.005-0.010%

Manganese,Mn ≤0.10%

Sulfur,S ≤0.01%

Silicon,Si, ≤0.30%

Iron,Fe ≤1.00%

Nickel,Ni ≤9.0-11.0%

Cobalt, Co Balance

Mar-M509 Physical Properties

  • Material Type:  Cobalt-based precipitation-hardening equiaxed cast superalloy (CoNiCrWTa group).
  • Density: ~8.85 g/cm³.
  • Maximum Service Temperature: Up to 1050 °C to 1100 °C.
  • Main Strengthening Phase: Carbides dispersed along grain boundaries and dendritic structures.
  • Corrosion & Oxidation Resistance: Good oxidation resistance up to roughly 1038 °C (1900 °F) and strong hot-corrosion resistance at 871 °C (1600 °F).

Features of Mar-M509 Superalloy

  • High-Temperature Strength: Retains structural integrity and resists deformation at service temperatures up to 1050°C (1900°F).
  • Creep Resistance: Features a unique carbide structure that prevents permanent stretching or sagging under heavy loads over time.
  • Corrosion Resistance: Offers excellent resistance to hot-corrosion, oxidation, and sulfidation compared to many nickel-based alternatives.
  • Thermal Shock Resistance: Withstands rapid shifts between extreme heat and cool temperatures without cracking.

Mar-M509 Superalloy Applicaitons

STEP 1

Aerospace & Aviation

Mar-M247 is extensively used for turbine blades, turbine wheels, shrouds and combustion components in aero-engines operating under extreme thermal conditions.

STEP 2

Power Generation

The alloy serves as a key material for industrial gas turbines, delivering long-term durability and stable efficiency under continuous high-temperature operation.

STEP 3

Oil & Gas

It is suitable for high-temperature turbine and compressor equipment requiring superior thermal stability and corrosion resistance in aggressive environments.

STEP 4

Energy Industry

Applied in gas turbine power plants and advanced energy systems, Mar-M247 maintains consistent performance during prolonged service cycles.

STEP 5

Turbine

The alloy performs reliably in marine turbine propulsion systems, turbine nozzle vanes and exhaust assemblies exposed to corrosive and high-temperature operating conditions.

STEP 6

Automotive Industry

Used in high-performance turbocharger turbines and motorsport exhaust components, it effectively withstands intense thermal stress and cyclic loading.

STEP 7

Chemical Processing

Mar-M509 is applicable to high-temperature industrial processing equipment requiring strong oxidation resistance and mechanical durability.

STEP 8

Military & Defense

Widely utilized in military aircraft engines and advanced propulsion systems, it provides exceptional structural reliability and heat resistance for critical defense applications.

STEP 9

Nuclear Industry

The alloy is employed in high-temperature reactor-related systems and power generation equipment demanding excellent structural integrity and long-term thermal stability.

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