CMSX-2 Alloy

CMSX-2 is a first-generation single-crystal superalloy known for its exceptional creep resistance, tensile strength, and high-temperature fatigue performance.

About CMSX-2 Superalloy

Name and Equivalent Name

CMSX-2 is a first-generation nickel-based single-crystal superalloy designated under AMS 5848 and UNS N26320. It was developed to meet the demands of high-stress environments in jet engines and gas turbines. Equivalent alloys, including PWA 1480 and René N4, offer comparable performance characteristics.

CMSX-2 Basic Introduction

CMSX-2 is a nickel-based single-crystal superalloy designed for aerospace and power generation applications. It offers excellent mechanical stability at elevated temperatures, with superior creep resistance and thermal fatigue performance.

The alloy’s carefully balanced composition, including chromium, tungsten, tantalum, and rhenium, allows it to maintain structural integrity under stress. It is widely used in turbine blades, vanes, and other high-temperature components that experience cyclic loading in extreme environments.

cmsx-2-single-crystal-superalloy-investment-casting-blades-manufacturer

Alternative Superalloys of CMSX-2

Alternatives to CMSX-2 include first-generation alloys such as PWA 1480, René N4, and SRR 99. These materials offer similar high-temperature strength and fatigue resistance. Second-generation alloys like CMSX-4 provide enhanced creep resistance but come with increased cost and complexity. CMSX-2 remains a reliable choice due to its balance of mechanical performance and manufacturability, especially for applications requiring precision single-crystal casting.


CMSX-2 Design Intention

The primary design intention behind CMSX-2 was to develop a superalloy with outstanding mechanical properties at temperatures up to 1035°C. The absence of grain boundaries improves fatigue resistance, while elements such as tantalum and rhenium provide superior creep resistance. With high oxidation resistance and excellent fracture toughness, CMSX-2 meets the rigorous demands of gas turbines and jet engines, ensuring long service life.


CMSX-2 Chemical Composition

The chemical elements in CMSX-2 play critical roles in improving its high-temperature performance. Chromium enhances oxidation resistance, tungsten and rhenium improve creep strength, and tantalum strengthens the matrix.

Element

Weight %

Nickel (Ni)

Balance

Chromium (Cr)

8%

Cobalt (Co)

5%

Molybdenum (Mo)

0.6%

Tungsten (W)

8%

Aluminum (Al)

5.6%

Tantalum (Ta)

6%

Rhenium (Re)

3%


CMSX-2 Physical Properties

CMSX-2 offers excellent thermal and mechanical stability at high temperatures, making it ideal for aerospace and power generation components.

Property

Value

Density

8.72 g/cm³

Melting Point

1345°C

Thermal Conductivity

11.5 W/(m·K)

Modulus of Elasticity

218 GPa

Tensile Strength

1100 MPa


Metallographic Structure of CMSX-2 Superalloy

CMSX-2 is a single-crystal nickel-based alloy with a gamma (γ) matrix and gamma-prime (γ') precipitates. The absence of grain boundaries eliminates weak points that typically promote creep and fatigue failures. The γ' phase, consisting of aluminum, tantalum, and nickel, provides enhanced mechanical strength and resistance to plastic deformation under stress.

This microstructure ensures long-term stability even under extreme thermal cycling. The well-dispersed γ' precipitates help maintain the alloy’s strength over extended service periods, making it highly suitable for jet engine components and turbine blades.


CMSX-2 Mechanical Properties

CMSX-2 maintains exceptional tensile strength and creep resistance at temperatures as high as 1035°C, offering reliable performance under cyclic loading conditions.

Property

Value

Tensile Strength

965-1035 MPa

Yield Strength

760-900 MPa

Creep Strength

High at 950°C

Fatigue Strength

~600 MPa

Creep Rupture Life

>10,000 hours at 1000°C

Hardness (HRC)

35-45

Elongation

10-15%


Key Features of CMSX-2 Superalloy

  1. Superior Creep Resistance CMSX-2 offers outstanding creep resistance, allowing it to maintain mechanical integrity under continuous stress at 950°C, with a creep rupture life exceeding 10,000 hours at 1000°C.

  2. High Fatigue Strength The absence of grain boundaries enhances fatigue resistance, making CMSX-2 suitable for components exposed to cyclic loading, such as turbine blades and vanes.

  3. Thermal Stability With a melting point of 1345°C and excellent thermal conductivity, CMSX-2 performs reliably in high-temperature environments like jet engines and gas turbines.

  4. Oxidation Resistance The alloy’s chromium content ensures strong oxidation resistance, reducing degradation and extending the service life of components in harsh environments.

  5. Mechanical Strength CMSX-2 exhibits high tensile strength (up to 1035 MPa) and yield strength (900 MPa), ensuring the durability of components exposed to mechanical stress and high temperatures.

CMSX-2 Superalloy’s Machinability

CMSX-2 can be used in Vacuum Investment Casting due to its high thermal stability and precise casting properties, ensuring dimensional accuracy and mechanical integrity.

This alloy is highly compatible with Single Crystal Casting since it is designed to eliminate grain boundaries, improving fatigue resistance and high-temperature performance.

CMSX-2 is unsuitable for Equiaxed Crystal casting because its performance relies on maintaining a single-crystal structure, which equiaxed grains cannot provide.

Although it offers high thermal performance, CMSX-2 is not typically used in Superalloy Directional Casting as it excels in fully single-crystal applications for better creep resistance.

This material is incompatible with Powder Metallurgy Turbine Disc techniques since its microstructure depends on casting rather than sintered powders for optimal properties.

CMSX-2 is unsuitable for Superalloy Precision Forging due to challenges in preserving the single-crystal structure during deformation processes.

Superalloy 3D Printing is not recommended for CMSX-2 since additive manufacturing cannot reliably produce single-crystal structures, limiting its mechanical potential.

CMSX-2 can undergo CNC Machining to achieve precise tolerances, but specialized tools are required due to its hardness and wear resistance.

It is challenging to use CMSX-2 for Superalloy Welding, as welding may introduce defects that compromise the integrity of the single-crystal structure.

Hot Isostatic Pressing (HIP) benefits CMSX-2, enhancing mechanical properties by eliminating internal porosity and improving structural integrity.


CMSX-2 Superalloy Applications

In the Aerospace and Aviation sector, CMSX-2 is used in turbine blades and vanes to handle extreme temperatures and stress within jet engines.

For Power Generation, CMSX-2 enables long service life in gas turbines, where high thermal stability and creep resistance are critical.

In the Oil and Gas industry, it is employed in components exposed to high temperatures, such as valves and turbine sections, ensuring durability under harsh conditions.

CMSX-2 contributes to the Energy industry by providing reliability in turbines for both conventional and renewable energy systems, especially under cyclic thermal loads.

In the Marine industry, it supports propulsion systems that encounter corrosive environments and high temperatures.

For Mining, CMSX-2 is used in specialized high-temperature tools and components, such as wear-resistant pumps and drill bits.

The Automotive industry leverages CMSX-2 in motorsport and high-performance engines, requiring superior heat resistance and mechanical strength.

In Chemical Processing, CMSX-2 ensures stability in reactors and heat exchangers, providing resistance to high-temperature corrosion.

Pharmaceutical and food industries use CMSX-2, essential for corrosion resistance and high-temperature sterilization.

The Military and Defense sector utilizes CMSX-2 in advanced propulsion systems, including jet engines, requiring high strength and fatigue resistance.

In the Nuclear industry, CMSX-2 is applied in turbines and reactor components, offering long-term stability under high radiation and thermal exposure.


When to Choose CMSX-2 Superalloy

Choose CMSX-2 when your application requires exceptional mechanical stability at high temperatures with prolonged exposure to stress. This alloy is ideal for custom superalloy parts in jet engines, gas turbines, and energy systems where creep resistance, fatigue strength, and oxidation resistance are essential. CMSX-2 is particularly suitable for aerospace, power generation, and military applications, providing long-term performance in harsh operating environments. When superior fatigue life, oxidation resistance, and high mechanical strength are needed, CMSX-2 remains an excellent material choice for components that operate under extreme conditions.

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