High-performance high-temperature alloys and titanium alloys, suitable for all scenarios including aircraft engines, landing gear, core structural components, and metal additive manufacturing, are the core guarantees for achieving lightweighting of aircraft and long service life of thermal components - the choice of materials in the aerospace field directly determines the thrust-to-weight ratio, extreme condition adaptability and operation and maintenance costs of the equipment.
Inconel 718(UNS N07718)as the most widely used precipitation-hardening type nickel-based high-temperature alloy for aerospace applications, has the highest yield strength among deformation high-temperature alloys below 650℃. It is the preferred material for the core components of the hot end of aircraft engines, including turbine discs, compressor discs, shafts, blades, combustion chamber casings, and high-temperature fasteners, etc. Under the SLM additive manufacturing process, it can achieve complete densification of the microstructure, directly meeting the integrated forming requirements of complex aerospace and aerospace structural components.
Ti-6Al-4V/TC4(UNS R56400)
The most widely used α+β type duplex titanium alloy is the "mainstay" of medium-temperature structural components in the aerospace field. It possesses excellent corrosion resistance, high heat resistance, and extremely high specific strength - its density is only 4.43g/cm³, yet its tensile strength at room temperature is ≥900MPa, yield strength ≥860MPa, and the strength retention rate remains over 80% below 400℃. This characteristic can directly reduce the weight of aircraft structures while meeting the requirements of lightweighting and core load-bearing. It is commonly used in aircraft landing gear links, engine cold end compressor fan blades, aircraft components, and biomedical implants.






