Ti-6AI-4V
It is a titanium alloy strengthened by heat treatment, which has good weldability and sheet formability, and forging properties. Used in the manufacture of jet engine compressor blades, impellers, etc. Others such as landing gear wheels and structural parts, fasteners, brackets, aircraft accessories, frames, stringer structures, pipes, are widely used. Ti-5AI-2. 5Sn
The ability to resist cracks during forging is good, the formability is acceptable, the weldability is good, and the heat treatment cannot be strengthened. It is used for transmission gearbox casing, jet engine casing device and guide vane cover, pipe structure, etc. Ti-8AI-1Mo-1V
The formability and crack resistance during forging are acceptable, and the weldability is good, but it cannot be strengthened by heat treatment. The land is used to make jet engine blades, impellers, casings, gyro gimbal guide vane covers, inner skins and frames of nozzle devices, etc. Ti-6AI-6V-2Sn
It is a heat-treatable-strengthened titanium alloy with good crack resistance during forging, but poor weldability. Used to manufacture fasteners, air inlet control guides, and test structural parts. Ti-13V-11Cr-3AI
It is a heat-treatable and strengthened titanium alloy with good formability, certain crack resistance during forging, and acceptable weldability. It is used for structural forgings, plate stringer structures, skins, frames, brackets, aircraft accessories, and fasteners. Ti-2. 25Al-11Sn-5Zr-1Mo-0. 2Si
It is a heat-treatable and strengthened titanium alloy with good crack resistance during forging. It is used to manufacture jet engine blades, impellers, landing gear rollers, aircraft skeletons, fasteners, etc. Ti-6AI-2Sn-4Zr-2Mo
It has good formability and weldability and has good crack resistance during forging, but it is not strengthened by heat treatment. It is used to manufacture compressor blades, impellers, landing gear rollers, spacer compressor case assemblies, aircraft skeletons, skin components, etc. Ti-4AI-3Mo-1V
It is a heat-treatable-strengthened titanium alloy with good forge ability and formability. Used in the manufacture of aircraft skeleton components. IMI125IMI130IMI160
Industrial pure titanium, excellent corrosion resistance, high specific strength, good fatigue limit, good forge ability, can be forged, formed, and welded by ordinary methods. Can be made into plates, rods, and wires. Used in aviation, medical, chemical, and other fields, such as exhaust pipes, firewalls, heated skins, and parts that require good plasticity and corrosion resistance IMI317
It belongs to α-type titanium alloy, can be welded, has good oxidation resistance, strength, and high-temperature stability at 315~593 ° C, and can be used to manufacture forgings and plate parts, such as aero-engine compressor blades, shells, brackets. IMI315
It belongs to α+β type titanium alloy, which can be strengthened by heat treatment. It is used for aero-engine compressor discs and blades, missile parts, etc.
IMI318
α+β type alloy, with good forge ability and comprehensive performance, is a titanium alloy commonly used in various countries for components such as aero-engine compressor discs and blades. IMI550
α+β titanium alloy, easy to forge, good room temperature strength, high creep resistance (below 400 ℃), high lasting strength, widely used in the manufacture of engine and wing slide rails, power control device casings, etc. IMI551
It belongs to α+β type titanium alloy high-strength titanium alloy, which has the characteristics of high strength, high creep limit (below 400 ℃), good enforceability, etc. It is used to manufacture aircraft components such as landing gear, mounts, and gas turbine components. It can be used in the general engineering and chemical industry, steam turbine blades, compressor parts, and other high-speed rotating parts. IMI685
It is an α+β type titanium alloy with high specific strength at room temperature and medium temperature, good resistance to drosophila at high temperature (520°C), good high-temperature stability, weldability, easy processing, and high operating temperature. Used to make aircraft engine parts. IMI684
It belongs to α+β type titanium alloy, which can be welded, has good creep resistance (below 535℃), and has excellent thermal stability. This alloy has similar properties to IMI685 and has the same purpose. Used to make high-pressure compressor discs and blades. IMI679
It is a complex α-type titanium alloy with good strength, high creep limit, high-temperature stability, and good oxidation resistance at 450~500 ℃, and its cylinder port fatigue strength is high. Used in the manufacture of aero-engine compressor discs, blades, aircraft skeletons, etc. IMI230
α-type titanium alloy, medium strength, good plasticity, weldability, aging strengthening, easy to form, the alloy is used in the annealed state and has high mechanical properties. It is used to make engine ducts, aircraft structures, etc. that work below 350 °C. T-A5E
It has good plasticity and toughness at -253℃. T-A6V
It has good comprehensive performance and is a high-quality material for the aerospace industry. T-A7D
Medium weldability and high mechanical properties are used as forgings. T-A6V6E2
Mainly used to make gas turbine engines and aircraft missile structures. T-TU2
It has weldability and formability in the quenched state and can be used below 350°C. T-T6Zr4DE
Weldable for jet engine blades and discs
Ti-6246
It can be used to make gas turbine disks, fan blades, and structural parts of aircraft and missiles. T-V13CA
It is used to make frames, honeycomb structures, etc. below 250°C. T-A6Z5W
Weldable high-strength titanium alloy with good creep resistance at 520°C. T-A6ZD
Parts (such as blades, discs, etc.) are used to make jet engines. T-A4DE2
The alloy has high strength and creeps resistance below 400°C. 3. 7114
Weldable, qualified formability, medium strength. 3. 7124
Plasticity, weldability, and high-temperature strength are similar to those of industrial pure titanium and are used for parts and corrosion-resistant parts below 350 °C. 3. 7134
It has a low density and high elastic modulus. It is used to make compressor discs and blades that work below 450 °C. It is an important material in the aviation industry. 3. 7144
Used to make aero-engine rotors and blades that work below 450°C. 3. 7154
The alloy has high strength, good screw resistance, and can be welded. Parts used for long-term work below 500 ℃, such as aero-engine compressor parts, etc. 3. 7164
Good comprehensive performance, used for high-stress mechanical parts working below 350 ℃. 3. 7174
It belongs to high-strength titanium alloy, which can be strengthened by heat treatment and has good forging performance. 3. 7184
It is used to make aero-engine components that work below 400°C, such as compressor disks, blades, etc. LT32
The alloy has high strength and good hardenability and is used to make aircraft skeletons and missile forgings that work below 427 °C. LT41 is a heat-treatable titanium alloy with excellent formability and is used to make aircraft skeletons, skins, honeycomb structures, pressure bulk crystals, and high-strength fasteners.
