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TM1910 Titanium 5553 Master Alloy (Ti-5Al-5Mo-5V-3Cr)

Catalog No. TM1910
Density 4.62 g/cm3
Appearance Metallic solid in various forms (waffle, ingot)
Compositions Ti-5Al-5Mo-5V-3Cr

Stanford Advanced Materials (SAM) supplies superior Ti alloys with high purity and specific material characteristics. Customized shapes and component ratios are available upon request.

Related products: Titanium Ingot (Ti Ingot), Titanium Aluminum clad material, Titanium Nickel clad material, Titanium 6246 Alloy, Titanium 6242 Alloy.

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TM1910 Titanium 5553 Master Alloy (Ti-5Al-5Mo-5V-3C)
TM1910 Titanium 5553 Master Alloy (Ti-5Al-5Mo-5V-3C)
TM1910 Titanium 5553 Master Alloy (Ti-5Al-5Mo-5V-3C)
TM1910 Titanium 5553 Master Alloy (Ti-5Al-5Mo-5V-3C)
Description
Specification

Description of Titanium 5553 Master Alloy

In recent years, with the advancement of titanium alloy material technology, high-strength, high-toughness, and anti-fatigue titanium alloy materials have been continuously developed and applied, and the most typical representative is Ti-5553 alloy.

The Ti-5553 master alloy has the characteristics of α+β titanium alloy and β-type titanium alloy. The tensile strength under the annealing state can reach 1080MPa. After solid-solution aging heat treatment, the tensile strength can exceed 1500MPa, and it has good toughness. Compared with the Ti-6Al-4V alloy, the alloy has the advantages of good hardenability, high strength, and good fracture toughness. It has been successfully applied to the connection between the wing of the Airbus A380 and the engine pylon.

 

Specification of Titanium 5553 Master Alloy

Element %

Ti-5553 Master Alloy

Aluminum

5.00 %

Iron

0.012 %

Phosphorous

0.035% Max

Molybdenum

5.00 %

Tin

-

Titanium

Balance

Zirconium

0.4% Max

Vanadium

5.00 %

Boron

0.003% Max

Carbon

0.10% Max

Chromium

3.00 %

Lead

0.003% Max

Magnesium

-

Manganese

-

Nickel

0.15% Max

Others-Each

-

Selenium

-

Silicon

5.00 %

Sulfur

0.02% Max

Hydrogen

-

Nitrogen

0.02% Max

Oxygen

0.15% Max

 

Applications of Titanium 5553 Master Alloy

- Used as the material of aircraft skeleton and connecting structural parts
- Aircraft landing gear
-Used as medical equipment

 

Packing of Titanium 5553 Master Alloy

All packaging materials are suitable for air, sea, and road freight. Vacuum packing is also available for selected alloys. Great care is taken to avoid any damage which might be caused during storage or transportation.

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