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Nickel-chromium-based solid solution reinforced super alloy Hastelloy GH3044
Hastelloy GH3044
Application: GH3044 alloy is mainly used in the manufacture of the main combustion chamber, guide blades, fuel ducts and other key components in aviation engines.It has good plasticity, durability and fatigue properties, as well as good stamping and welding properties.
Hastelloy GH3099
Chemical composition: GH3099 is a nickel-chromium-based superalloy with good high temperature resistance and mechanical properties.
Application: GH3099 is usually used in nickel-chromium-based superalloys for high-temperature components in the fields of aviation, aerospace, energy and chemical industry.
Hastelloy GH3030
Chemical composition: GH3030 is a Ni-Cr-based solid solution reinforced deformed superalloy, which contains high chromium and nickel content, as well as a small amount of molybdenum, iron, aluminum and other elements.
Application: GH3030 alloy is mainly used for turbine engine combustion chamber components that work below 800°C, as well as high-temperature parts that require oxidation resistance but bear small loads below 1100°C.It has good thermal strength and high plasticity, as well as resistance to hot and cold fatigue and oxidation resistance, and has good cold stamping and welding process performance.
Summary
High temperature resistance: Both GH3044 and GH3030 alloys have good high temperature resistance and are suitable for use in high temperature environments.
Mechanical properties: GH3044 alloy has good plasticity, durability and fatigue properties, while GH3030 alloy has good thermal strength and high plasticity.
Application areas: GH3044 alloy is mainly used for key components of aviation engines, while GH3030 alloy is suitable for high temperature applications such as turbine engine combustion chamber components.
When choosing these materials, which material to use should be decided according to the specific application needs and environmental conditions.
