AMS 5786 is a high-strength titanium alloy commonly used in critical aircraft engine components such as turbine disks and compressor blades. This alloy is known for its excellent fatigue and high temperature properties, making it a reliable choice for ensuring safe and efficient air travel.
AMS 5786 Chemistry Composition:
AMS 5786 is made from a nickel-iron-chromium-molybdenum-niobium (ni-fe-cr-mo-cb) alloy. This ingredient gives the material excellent strength, toughness and corrosion resistance. It also has high temperature stability, making it ideal for turbine engine components operating at high temperatures.
| Elements | Content (%) |
|---|---|
| Nickel, Ni | 63 |
| Molybdenum, Mo | 24 |
| Iron, Fe | 6 |
| Chromium, Cr | 5 |
| Cobalt, Co | 2.50 |
| Vanadium, V | 0.60 |
AMS 5786 Physical Properties:
AMS 5786 has a density of 8.19 g/cm3 and a melting point of 1336°C. It has good thermal and electrical conductivity, making it an ideal material for high temperature applications. It also has excellent resistance to oxidation and corrosion.
AMS 5786 mechanical properties:
AMS 5786 has excellent mechanical properties. It has a minimum tensile strength of 185 ksi (1276 MPa) and a minimum yield strength of 150 ksi (1034 MPa). It also has high fatigue strength and good creep resistance. The material has a maximum hardness of 363 HBW.
AMS 5786 uses:
The primary use of AMS 5786 is in the production of turbine engine components. It is commonly used in the manufacture of turbine disks, gaskets and shafts. It is also used in other high temperature applications such as nuclear reactors and gas turbines.
AMS 5786 Hardness:
AMS 5786 has a maximum hardness of 363 HBW. This makes it a relatively rigid material, critical for high stress applications.
AMS 5786 Heat Treatment:
AMS 5786 can be heat treated to improve its properties. It can be solution treated and then age hardened to increase its strength and hardness. The material can also be cold worked to increase its strength and fatigue resistance.
in conclusion:
To sum up, AMS 5786 material is a Ni-Fe-Cr-Mo-Cb alloy with excellent strength, toughness and corrosion resistance. Its high temperature stability makes it ideal for turbine engine components operating at high temperatures. The material has excellent mechanical properties with a minimum tensile strength of 185 ksi and a maximum hardness of 363 HBW. It can be heat treated to improve its properties and is commonly used in the aerospace and automotive industries. If you are looking for a high-quality material that can withstand high temperatures and pressure, consider AMS 5786.
Tianjin Anton Metal Manufacture Co., Ltd. is a company specializing in the production of various nickel-based alloys, Hastelloy alloys and high-temperature alloy materials. The company was established in 1989 with a registered capital of 10.0 million, specializing in the production and sales of alloy materials. Anton Metal’s products are widely used in aerospace, chemical industry, electric power, automobile, nuclear energy and other fields, and can also provide customized alloy material solutions according to customer needs. If you need to know the price consultation of alloy materials or provide customized alloy material solutions, please feel free to contact the sales staff.
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Post time: Feb-23-2024
