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R56401 Titanium vs. Grade 27 Titanium

Both R56401 titanium and grade 27 titanium are titanium alloys. Both are furnished in the annealed condition. They have 90% of their average alloy composition in common.

For each property being compared, the top bar is R56401 titanium and the bottom bar is grade 27 titanium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 110
110
Elongation at Break, % 9.1
27
Fatigue Strength, MPa 480
170
Poisson's Ratio 0.32
0.32
Reduction in Area, % 17
34
Shear Modulus, GPa 40
41
Shear Strength, MPa 560
180
Tensile Strength: Ultimate (UTS), MPa 940
270
Tensile Strength: Yield (Proof), MPa 850
230

Thermal Properties

Latent Heat of Fusion, J/g 410
420
Maximum Temperature: Mechanical, °C 340
320
Melting Completion (Liquidus), °C 1610
1660
Melting Onset (Solidus), °C 1560
1610
Specific Heat Capacity, J/kg-K 560
540
Thermal Conductivity, W/m-K 7.1
21
Thermal Expansion, µm/m-K 9.6
8.7

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.0
3.6
Electrical Conductivity: Equal Weight (Specific), % IACS 2.0
7.1

Otherwise Unclassified Properties

Base Metal Price, % relative 36
37
Density, g/cm3 4.5
4.5
Embodied Carbon, kg CO2/kg material 38
33
Embodied Energy, MJ/kg 610
530
Embodied Water, L/kg 200
320

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 83
70
Resilience: Unit (Modulus of Resilience), kJ/m3 3440
240
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 35
35
Strength to Weight: Axial, points 59
17
Strength to Weight: Bending, points 48
21
Thermal Diffusivity, mm2/s 2.9
8.8
Thermal Shock Resistance, points 67
21

Alloy Composition


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Aluminum (Al), % 5.5 to 6.5
0
Carbon (C), % 0 to 0.080
0 to 0.080
Hydrogen (H), % 0 to 0.012
0 to 0.015
Iron (Fe), % 0 to 0.25
0 to 0.2
Nitrogen (N), % 0 to 0.050
0 to 0.030
Oxygen (O), % 0 to 0.13
0 to 0.18
Ruthenium (Ru), % 0
0.080 to 0.14
Titanium (Ti), % 88.5 to 91
99 to 99.92
Vanadium (V), % 3.5 to 4.5
0
Residuals, % 0
0 to 0.4