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GH169 Alloy is a high-strength, heat-resistant nickel-based superalloy for turbine engines

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GH169 Alloy is a high-strength, heat-resistant nickel-based superalloy for turbine engines

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Brand Name : Zhonggong Special Metallurgy

Model Number : GH169 Alloy

Place of Origin : China

MOQ : 100KG

Price : Price is negotiated based on the required specifications and quantity

Payment Terms : Payment Terms: Mainly T/T.. L/C, D/A, D/P,

Supply Ability : 5000 tons per month

Delivery Time : 5-8 working days, depending on the parameters required for negotiation

Packaging Details : Standard export packaging, or packaging as required

Density : 8.4 g/cm³

Melting Point : 1260-1360°C

Tensile Strength : 950-1150 MPa

Yield Strength : 750-900 MPa

Hardness : 15-25%

Thermal Conductivity : 11.0 W/m·K

Oxidation Resistance : Good

Applications : Turbine Engines, Aerospace Components

Certification : ISO Certificate

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GH169 Alloy is a high-performance, nickel-based superalloy designed for applications requiring exceptional strength and heat resistance. Key features include:

  • High Temperature Strength: GH169 Alloy maintains superior mechanical properties at high temperatures, typically up to 1,300°C (2,372°F), making it ideal for extreme environments.
  • Exceptional Strength: The alloy exhibits high tensile and yield strength, ensuring durability and reliability in high-stress applications such as turbine engines.
  • Good Oxidation and Corrosion Resistance: Offers solid resistance to oxidation and corrosion, enhancing the longevity and performance of components in aggressive environments.
  • Thermal Stability: Demonstrates stability under thermal cycling, reducing the risk of deformation and maintaining structural integrity.
  • Applications: Widely used in turbine engines, aerospace components, and other high-temperature applications where strength, durability, and resistance to extreme conditions are critical.

GH169 Alloy is engineered to meet the demanding requirements of advanced engineering and aerospace industries, providing reliable performance in challenging conditions.

Here's a table summarizing the typical chemical composition of GH169 Alloy:

Element Content (%)
Nickel (Ni) 60.0-65.0
Chromium (Cr) 14.0-16.0
Cobalt (Co) 6.0-8.0
Molybdenum (Mo) 4.0-5.0
Aluminum (Al) 0.8-1.2
Titanium (Ti) 1.5-2.0
Carbon (C) 0.08-0.15
Iron (Fe) Balance
Others Trace elements

This composition provides GH169 Alloy with its desired properties of high strength, heat resistance, and durability. Let me know if you need any further details.

GH169 Alloy is a high-strength, heat-resistant nickel-based superalloy for turbine engines


Product Tags:

aerospace components nickel based alloys

      

aerospace components nickel based superalloy

      
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