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GH4180 Alloy Nickel Based Superalloy High Strength Excellent Oxidation Resistance

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GH4180 Alloy Nickel Based Superalloy High Strength Excellent Oxidation Resistance

GH4180 Alloy Nickel Based Superalloy High Strength Excellent Oxidation Resistance
GH4180 Alloy Nickel Based Superalloy High Strength Excellent Oxidation Resistance GH4180 Alloy Nickel Based Superalloy High Strength Excellent Oxidation Resistance GH4180 Alloy Nickel Based Superalloy High Strength Excellent Oxidation Resistance

Large Image :  GH4180 Alloy Nickel Based Superalloy High Strength Excellent Oxidation Resistance

Product Details:
Place of Origin: China
Brand Name: Zhonggong Special Metallurgy
Certification: ISO Certificate
Model Number: GH4180 alloy
Payment & Shipping Terms:
Minimum Order Quantity: 100KG
Price: Price is negotiated based on the required specifications and quantity
Packaging Details: Standard export packaging, or packaging as required
Delivery Time: 5-8 working days, depending on the parameters required for negotiation
Payment Terms: Payment Terms: Mainly T/T.. L/C, D/A, D/P,
Supply Ability: 5000 tons per month

GH4180 Alloy Nickel Based Superalloy High Strength Excellent Oxidation Resistance

Description
Density: ~8.3 G/cm³ Melting Point: ~1390°C (2530°F)
Thermal Conductivity: ~11-13 W/m·K Yield Strength: ~700 MPa (102 Ksi)
Ultimate Tensile Strength: ~900 MPa (130 Ksi) Elongation: ~10%
Hardness (Rockwell): ~HRB 90-95 Applications: Aerospace Components, Gas Turbines, And High-temperature Engines
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Nickel Based Superalloy High Strength

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GH4180 Nickel Based Superalloy

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aerospace components nickel based alloys

GH4180 Alloy Nickel Based Superalloy
High Strength with Excellent Oxidation Resistance
GH4180 is a high-performance nickel-based superalloy engineered for superior strength and oxidation resistance in extreme environments. Designed for applications requiring high-temperature stability and durability.
Key Specifications
Attribute Value
Density ~8.3 g/cm³
Melting Point ~1390°C (2530°F)
Thermal Conductivity ~11-13 W/m·K
Yield Strength ~700 MPa (102 ksi)
Ultimate Tensile Strength ~900 MPa (130 ksi)
Elongation ~10%
Hardness (Rockwell) ~HRB 90-95
Applications Aerospace components, gas turbines, and high-temperature engines
Material Composition
Element Content Range
Nickel (Ni) Balance
Chromium (Cr) 19.0-21.0%
Iron (Fe) 9.0-11.0%
Cobalt (Co) 8.0-10.0%
Molybdenum (Mo) 2.0-3.0%
Titanium (Ti) 2.0-3.0%
Aluminum (Al) 1.0-2.0%
Boron (B) 0.005-0.015%
Performance Characteristics
  • High Temperature Performance: Maintains structural integrity up to 1390°C (2530°F)
  • Mechanical Strength: Exceptional yield and tensile strength for high-stress applications
  • Oxidation Resistance: Superior protection against high-temperature corrosion
  • Thermal Stability: Reliable performance under severe thermal conditions
GH4180's unique combination of high strength, thermal stability, and corrosion resistance makes it ideal for demanding aerospace and industrial applications where performance under extreme conditions is critical.
GH4180 Alloy Nickel Based Superalloy High Strength Excellent Oxidation Resistance 0

Contact Details
Jiangsu Zhonggongte Metallurgical Technology Co., Ltd.

Contact Person: John zhou

Tel: +8613306184668

Fax: 86-510-88232386

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