Product Details:
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Density: | 8.19 G/cm³ | Melting Point: | 1260-1340°C |
---|---|---|---|
Tensile Strength: | 900-1100 MPa | Yield Strength: | 700-850 MPa |
Elongation: | 20-35% | Hardness: | 250-300 HB |
Thermal Conductivity: | 11.2 W/m·K | Oxidation Resistance: | Excellent |
Applications: | Aerospace, Gas Turbines, High-temp. Components | ||
Highlight: | GH738 Ni Based Superalloy,Ni Based Superalloy High Strength |
Attribute | Value |
---|---|
Density | 8.19 g/cm³ |
Melting Point | 1260-1340°C |
Tensile Strength | 900-1100 MPa |
Yield Strength | 700-850 MPa |
Elongation | 20-35% |
Hardness | 250-300 HB |
Thermal Conductivity | 11.2 W/m·K |
Oxidation Resistance | Excellent |
Applications | Aerospace, Gas Turbines, High-temp. Components |
GH738 Alloy is a high-performance, nickel-based superalloy engineered for exceptional mechanical strength and superior oxidation resistance at elevated temperatures. It is commonly used in aerospace and industrial gas turbine applications due to its ability to maintain structural integrity under extreme conditions.
GH738 Alloy's robust performance characteristics make it a preferred choice for demanding applications where reliability and durability are paramount.
Element | Content (%) |
---|---|
Nickel (Ni) | 50.0 - 60.0 |
Chromium (Cr) | 20.0 - 25.0 |
Cobalt (Co) | 7.0 - 10.0 |
Molybdenum (Mo) | 3.0 - 5.0 |
Titanium (Ti) | 2.5 - 4.0 |
Aluminum (Al) | 1.5 - 2.5 |
Iron (Fe) | Balance |
Carbon (C) | ≤ 0.08 |
Boron (B) | ≤ 0.01 |
Other Elements | Traces |
This composition provides GH738 Alloy with its high-temperature strength and resistance to oxidation and corrosion.
Contact Person: John zhou
Tel: +8613306184668
Fax: 86-510-88232386