GH3625 high-temperature alloy is a solution-strengthened nickel-based wrought superalloy primarily strengthened by molybdenum and niobium. It exhibits excellent corrosion resistance and oxidation resistance, good tensile properties, and fatigue performance from low temperatures up to 980°C, as well as resistance to stress corrosion in salt spray environments. As a result, it is widely used in the manufacture of aircraft engine components, aerospace structural parts, and chemical equipment.

GH3625 Chemical Composition:

C(%): 0.10

Si(%): ≤0.50

Mn(%): ≤0.50

Cr(%): 20-23

Ni(%): 61

Mo(%): 8-10

Co(%): —

W(%): —

Al(%): ≤0.40

Cu(%): —

Ti(%): ≤0.40

Fe(%): 2.5

Others(%): Nb 3.65

GH3625 Mechanical Properties:

Density: 8.4 g/cm3

Melting Point: 1290-1350°C

Introduction

GH3625 high-temperature alloy is a solution-strengthened nickel-based wrought superalloy primarily strengthened by molybdenum and niobium. It exhibits excellent corrosion resistance and oxidation resistance, good tensile properties, and fatigue performance from low temperatures up to 980°C, as well as resistance to stress corrosion in salt spray environments. As a result, it is widely used in the manufacture of aircraft engine components, aerospace structural parts, and chemical equipment.

Application Areas

Components in organic chemical processes involving chlorides, especially in the use of acidic chloride catalysts.

Used in cooking and bleaching in the pulp and paper industry.

Absorber towers, reheaters, flue gas inlet dampers, fans (wet), agitators, baffles, and ducts in FGD systems.

Used in the manufacture of equipment and components for use in acidic gas environments.