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High Strength Nickel Based Superalloy GH4145 Alloy With Excellent Thermal Stability
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High Strength Nickel Based Superalloy GH4145 Alloy With Excellent Thermal Stability
| MOQ: | 100KG |
| Price: | Price is negotiated based on the required specifications and quantity |
| Standard Packaging: | Standard export packaging, or packaging as required |
| Delivery Period: | 5-8 working days, depending on the parameters required for negotiation |
| Payment Method: | Payment Terms: Mainly T/T.. L/C, D/A, D/P, |
| Supply Capacity: | 5000 tons per month |
Detail Information
Place of Origin
China
Brand Name
Zhonggong Special Metallurgy
Certification
ISO Certificate
Model Number
GH4145 alloy
Density:
~8.3 G/cm³
Melting Point:
~1390°C (2530°F)
Thermal Conductivity:
~11-12 W/m·K
Yield Strength:
~700 MPa (102 Ksi)
~700 MPa (102 Ksi):
900 MPa (130 Ksi)
Elongation:
~10%
Hardness (Rockwell):
~HRB 90-95
Applications:
Aerospace Components, Gas Turbines, And High-temperature Industrial Parts
Highlight:
Nickel Based Superalloy GH4145
,Ni Based Superalloy GH4145
Product Description
High Strength Nickel Based Superalloy GH4145 Alloy With Excellent Thermal Stability
Product Specifications
| Attribute | Value |
|---|---|
| Density | ~8.3 g/cm³ |
| Melting Point | ~1390°C (2530°F) |
| Thermal Conductivity | ~11-12 W/m·K |
| Yield Strength | ~700 MPa (102 ksi) |
| Tensile Strength | 900 MPa (130 ksi) |
| Elongation | ~10% |
| Hardness (Rockwell) | ~HRB 90-95 |
| Applications | Aerospace components, gas turbines, and high-temperature industrial parts |
GH4145 Alloy Overview
GH4145 is a high-performance nickel-based superalloy renowned for its exceptional strength, thermal stability, and resistance to oxidation and corrosion. Designed for demanding high-temperature environments, it delivers reliability and durability in critical applications.
Key Features
- Composition: Primarily nickel with chromium, iron, cobalt, molybdenum, titanium, and aluminum for optimal mechanical strength, thermal stability, and corrosion resistance.
- Temperature Resistance: Maintains performance at temperatures up to 1390°C (2530°F) with preserved mechanical properties.
- Mechanical Strength: High yield and tensile strength ensure durability under significant stress and load conditions.
- Oxidation/Corrosion Resistance: Superior protection against high-temperature corrosion extends component lifespan and reduces maintenance.
- Applications: Ideal for aerospace components, gas turbines, and industrial processes requiring strength and stability in harsh environments.
Chemical Composition
| Element | Content Range |
|---|---|
| Nickel (Ni) | Balance |
| Chromium (Cr) | 18.0-21.0% |
| Iron (Fe) | 14.0-17.0% |
| Cobalt (Co) | 8.0-10.0% |
| Molybdenum (Mo) | 2.0-3.0% |
| Titanium (Ti) | 1.5-2.5% |
| Aluminum (Al) | 1.0-1.5% |
| Boron (B) | 0.005-0.015% |
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