6AL-2SN-4ZR-2MO (6-2-4-2) TITANIUM
6Al-2Sn-4Zr-2Mo Titanium popularly known as 6-2-4-2 Titanium. This alpha-beta titanium alloy can be heat treated to produce higher strengths in larger section sizes than 6Al-4V. Widely used in manufacturing components. 6-2-4-2 beta-forged material has improved strength, ductility, and a combination of good low-cycle fatigue and fatigue-crack development resistance. This alloy found in turbine engine intermediate compressor stages for disks and blades, seals and airframe parts.
ROUND BAR
6-2-4-2 Titanium round bars have a diameter of 0.125″ to 14.00″ diameter
FLAT BAR
6-2-4-2 Titanium flat bars available in different thicknesses and widths. Request a quote for more information
PLATE
The thickness of 6Al-2Sn-4Zr-2Mo plates from 0.1875″ to 6.50″
SHEET
Ti6Al-2Sn-4Zr-6Mo sheets offered in thicknesses from 0.002″ to .150″
BASIC APPLICATIONS OF 6AL-2SN-4ZR-2MO
6-2-4-2 titanium alloy designed for high strength, excellent fatigue resistance, and outstanding performance at elevated temperatures. This alloy ideal for demanding environments where strength, lightweight properties, and thermal stability are critical. Common applications include:
6AL-2SN-4ZR-2MO Aerospace
Jet engine components, airframe parts, and high-temperature structural applications.
Automotive
Racing components, such as connecting rods and suspension systems.
Defense
Armor plating and military aircraft components for extreme conditions.Industrial
Heat exchangers, chemical processing equipment, and high-performance fasteners.
MANUFACTURING STRUCTURAL COMPONENTS
This titanium alloy is utilized in the fuselage to create various structural elements such as beams, frames, and stringers. These components enhance the strength and rigidity of the fuselage, enabling it to withstand the stresses and pressures encountered during flight.
USE IN AN AIRCRAFT ENGINE
Aviation engines manufactured from this titanium alloy incorporate various structural components, including vanes, discs, and turbine blades. The use of this material ensures that these parts possess the necessary strength and can endure the elevated temperatures and stresses encountered during operation.
MISSILE COMPONENTS
This titanium alloy is utilized in the construction of structural components such as the body, fins, and propulsion systems in missile technology. Its application enhances the strength and durability of a missile’s structural elements, enabling them to endure the stresses encountered during Flight.