GH3536

Alloy composition

GH3536 high-temperature alloy is typically composed of 65% nickel, 22% chromium, 6% iron, 2.5% aluminum, 1.5% titanium, and 1% molybdenum, with nickel being the primary constituent.

Physical Properties

The density of GH3536 high-temperature alloy is approximately 8.11 g/cm³, with a melting point of about 1395-1425°C.

Mechanical properties

GH3536 high-temperature alloy boasts excellent strength and ductility in high-temperature environments. Its specific mechanical properties are as follows:

Tensile Strength: Approximately 105 Ksi (725 MPa).

Yield strength: Approximately 45 Ksi (310 MPa).

Tensile elongation: Approximately 40%.

Welding Performance

GH3536 high-temperature alloy is easy to machine and can be processed using welding methods such as TIG, MIG, MAG, and arc welding. It is important to note that during the welding process, heat and welding speed should be controlled to avoid issues like thermal cracks.

Corrosion resistance

GH3536 high-temperature alloy exhibits excellent corrosion resistance in both high-temperature and high-pressure environments, maintaining good corrosion resistance in oxidizing and reducing atmospheres.

Application Fields

GH3536 high-temperature alloy is used in aerospace, petrochemical, and other fields, particularly suitable for manufacturing high-temperature, high-strength components and structural parts that are used long-term in corrosive environments under high temperature and pressure.

Typical Engineering Applications

GH3536 high-temperature alloy is commonly used in the aerospace industry for high-temperature components in gas turbine engines; it is also frequently utilized in the chemical and petrochemical sectors for manufacturing high-temperature reactors, steam generators, and catalyst carriers, among other equipment.

Execution Standards

GH3536 high-temperature alloy conforms to domestic standards GB/T 14992-2005 and international standards ASTM B637, among others.