MOQ | 300 Kilogram/Kilograms |
Place of Origin | China | Application | Compressor discs, blades;Airframe structure, skin |
Thickness | MAX:60mm | Width | MAX:3000mm |
Length | Max 6Meter | Technique | Hot Rolled |
Ti (Min) | Balance | Brand Name | HY |
Model Number | 6-2-4-2 Titanium |
Titanium 6-2-4-2
Material grades and equivalents
6Al-2Sn-4Zr-2Mo,
6-2-4-2 Titanium, 6-2-4-2, UNS R54620
Introduction
A near-alpha alloy,
primarily used for high strength and toughness, with good
creep resistance up to 1000°F. Forging and machining
characteristics similar to those of Ti 6Al-4V. Applications
include compressor components, hot airframe skin, and
engine afterburner structures. The weld ability of Ti
6-2-4-2 is fair, using AMS 4952 weld wire. Several
different treatments are available.
Chemistry
Composition
6Al-2Sn-4Zr-2Mo - Rolled Alloys, Inc.
Features
• Machinability similar to
austenitic stainless steels
• Easily welded if proper
precautions are taken to prevent oxygen, nitrogen and
hydrogen contaminations
• Long term stability for
temperatures up to 800°F
Applications
• Compressor discs,
blades
• Airframe structure,
skin
• Engine afterburner
components
• Hush kits
Physical
Properties
Density: 0.160
lb/in3
Beta Transus:
1825±25°F
Thermal Conductivity: 4.00
Btu • hr/ft2 • hr°F
Coefficient of Thermal
Expansion: 32-212°F 4.3 x10-6 in/in°F
Modulus of Elasticity:
16.5x106 psi
Mechanical
Properties
Minimum Tensile Properties,
AMS 4919, Duplex Annealed
Thickness, in 0.025 ≤ 0.062
> 0.062 ≤ 1.000 > 1.000 ≤ 3.000
Tensile Strength, ksi
135,000 135,000 135,000
0.2% offset Yield Strength,
ksi 125,000 125,000 125,000
Elongation, % 8 10
10
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