Leading Manufacturer for Titanium alloy 10V-2Fe-3Al UNS R56410 for Jeddah Manufacturers

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HY Titanium 10-2-3 Material grades and equivalents

10-2-3 Titanium, UNS R56410

Introduction

HY Titanium 10-2-3 is a near beta alloy developed as a high strength forging alloy. This grade provides the best combination of strength and toughness of the commercially available titanium alloys. Its strength permits about a 27% weight savings when compared to Ti-6Al-4V. At the 180 ksi tensile strength level, the K1cvalue is 40 ksi-in ½ minimum. Solution treated and aged material possesses excellent resistance to stress corrosion cracking, typically K1scc being greater than 0.8 K1c. Solution treated material should not be subject to long term exposure in the 500-800°F range. This could result in high strength but low ductility.

High strength condition: Solution treat 60-100°F below the beta transus (typically 1460-1480°F), not less than 30 minutes, water quench. Age 900-975°F not less than 8 hours, air cool. For lower strength, overage in the 950-1150°F range. This alloy is deep hardenable, capable of high strengths in sections up to approximately 4″ thick.

This grade is usually supplied as billet or bar, finish rolled or forged in the alpha-beta field. For the high strength condition, the forging is usually given a pre-form forge above the beta transus, followed by 15-25% reduction below the beta transus.

Chemistry Composition

 

V

Al

Fe

C

N

O

H

Y

Others,
Each

Others,
Total

Ti

MIN

9.0

2.6

1.6

-

-

-

-

-

-

-

-

MAX

11.0

3.4

2.22

0.05

0.05

0.13

0.015

0.005

0.10

0.30

Balance

Features

  • High strength and toughness
  • Weight savings when compared to Ti-6Al-4V
  • Excellent resistance to stress corrosion cracking

Applications

  • Hand and die forgings
  • Aircraft landing gear
  • Golf club driver faces

Physical Properties

Density: 0.168 lb/inch³
Nominal Beta Transus: 1470°F
Poisson’s ratio: 0.32
Thermal Expansion: 75-800°F, 5.4×10-6 in/in°F
Tensile Modulus: 15.9×106 psi
Modulus: 16.2×106 psi

* 70°F to indicated temperature.

Mechanical Properties

Minimum Mechanical Properties AMS 4984, solution treated and aged

Ultimate Tensile Strength, ksi

173

Ultimate Tensile Strength, ksi

160

0.2% Yield Strength, ksi

4

Reduction of Area, %

Report

fracture toughness, k1C

40 ksi


AMS 4987, single solution heat treat & overage

Ultimate Tensile Strength, ksi

140

0.2% Yield Strength, ksi

130

Elongation, %

8

Reduction of Area, %

20

fracture toughness, k1C

80 ksi

Regular shape for all kinds of alloys
Form Specification Supply Form Others
Sheet Thickness:0.40-4.75mm,General Width:1000、1219、1500mm Whole Coil or piece of it Cold Annealed,Surface 2B、2E
Plate Thickness:4.76-60mm,Width:1500、2000、2500mm,Length:3000、6000、8000、8500mm(Under 10mm plate can be coiled) Whole Coil or piece of it Single hot rolling,Solid solution annealed state,Surface 1D
Belt Thickness:0.10-3.0mm,Width:50-500mm Whole Coil or Specified size Cold Annealed,Surface 2B、2E
Bar & Rod Rolled barΦ5-45mm,Length≤1500mm Polished Bar(circle、Square) Solution annealing,descaling
Forged barΦ26-245mm,Length≤4000mm
Weld tube Outer diameterΦ4.76-135mm,Wall Thickness0.25-4.00mm,Length:≤35000 mm Base on your requirement
Seamless Tube Outer diameterΦ3-114mm,Wall Thickness0.2-4.5mm Base on your requirement
Wire Outer diameterΦ0.1-13mm Base on your requirement Ni & Ni alloy, Ti & Ti alloy
Forged piece discs,rings,squares,blocks,slabs Base on your requirement Steel, Alloy
Flangs All kinds of Flangs Base on your requirement Steel, Alloy
Welding Material Coil wire Φ0.025mm-1.6mm Base on your requirement Certificate of Origin:America, Sweden, Britain, Germany, Austria, Italy, France.
Straight WireΦ1.6mm-4.0mm
Welding rodΦ1.2mm-4.0mm
Tube Elbow, three links, four links, different diameter size Base on your requirement Ni & Ni alloy, Ti & Ti alloy
Explosive bonded laminate Raw Sheet Thickness≥2mm Base on your requirement Ni & Ni alloy, Ti & Ti alloy

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