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GH4080A
Gh4080a is a nickel-based high-temperature alloy composed of nickel-chromium alloy, which has good strength, excellent high-temperature corrosion resistance and oxidation resistance. These advantages make 4080a widely used in aviation, aerospace, power station, transportation and other high temperature hot forging parts.
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Gh4080a is a nickel-based high-temperature alloy composed of nickel-chromium alloy, which has good strength, excellent high-temperature corrosion resistance and oxidation resistance. These advantages make 4080a widely used in aviation, aerospace, power station, transportation and other high temperature hot forging parts.
Chemical composition of GH4080A
% Ni Cr Fe Mo Mn Al Ti W C Si P S Cu Minimum Allowance 18.0 1.0 0.3 Max. 21.0 1.8 0.7 0.1 1.0 0.015 Physical Properties of GH4080A
Density 8.19g/cm² Melting Point 1320-1365 ℃ Scope and areas of GH4080A
An aeroengine combustion chamber flame tube, afterburner housing and regulating plate are introduced.
A Structural Form of Gas Turbine Combustor
A combustion component of a turbine engine
Afterburner component
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GH4080A
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