Inconel 718 is a precipitated hardened deformed high-temperature alloy, can be used at 650 degrees C for a long time, short-term use temperature of up to 800 degrees C, the alloy at 650 degrees C below the strength of higher, with good anti-fatigue, antioxidant and tissue stability. Suitable for the production of aerospace and industrial turbine parts, ring parts, blades, boxes and other structures;

Hastelloy X is a solid-soluble reinforced deformed high-temperature alloy with medium durability and creep strength below 900 ℃, and good antioxidant and corrosion resistance. Suitable for the manufacture of long-term use of aero engine combustion chambers and other components below 900℃;

GH3230 is a solid-soluble reinforced deformed high-temperature alloy, using a temperature of 700-1050 degrees C, the alloy has a high strength and resistance to heat and cold fatigue performance, suitable for the production of aviation engine flame barrel and other parts;

GH4099 is a precipitated reinforced high-temperature alloy that can be used for a long time below 900 ℃. The alloy has high thermal strength, stable organization, and good thermal processing and welding process performance, suitable for the manufacture of aero engine combustion chamber and force combustion chamber and other high temperature structural parts;

K418 is a precipitated hardened casting high temperature alloy with high creep strength, anti-hot and cold fatigue and antioxidant properties. Suitable for the production of hot end rotation and stationary parts for work below 900 ℃，similar to In713C;

K438 is a precipitated hardened casting high temperature alloy, is one of the best anti-thermal corrosion performance of the alloy, the temperature is less than 900 ℃, mainly used in the production of gas turbine and aero engine turbine working blades, guide blades and so on, Similar  to Inconel 738;

K477 is a precipitated hardened casting high-temperature alloy, the temperature is less than 900 ℃, the alloy has a high strength and plasticity, stable organization, and has good casting performance. Suitable for the manufacture of aero engine turbine blades and other high-temperature parts;

GH5188 is a solid-soluble reinforced deformation high-temperature alloy, the use of temperature is less than 1100 degrees C, the alloy has better process properties such as hot and cold processing plasticity and welding, suitable for the production of 980 degrees C required high strength and 1100 degrees C below the requirements of antioxidant aero engine components;