TC4 Ti-6Al-4V Titanium Sheet For Aerospace High Performance Materials For Aircraft
Brand Name:JIMA Aluminum
Certification:IRIS,ISO9001，ISO 14001.
Model Number:8011,3003，5005,5052
Minimum Order Quantity:Negotiations
Delivery Time:20~25days
Payment Terms:T/T, L/C
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TC4 (Ti-6l-4V) Titanium Alloy Sheet 1,Products: TC4 (Ti-6Al-4V) is one of the most widely used high-strength
titanium alloys at present. TC4 titanium alloy combines excellent
corrosion resistance, favorable mechanical strength and low density
(about 4.5 kg/dm³). TC4 titanium alloy is a heat-treatable titanium
alloy product that can be processed up to 25mm (solution heat
treatment + aging), with a maximum operating temperature of up to
400°C. This material has good formability and outstanding specific
strength, so it is widely used in aerospace and motorsports.
Approximately 50% of the global titanium alloy procurement volume
is TC4 (Ti-6Al-4V). 2,Application Areas: Materials used in aerospace, automotive and new energy, industrial
molds and dies, and semiconductor fields 3,Product Details:
Unique Advantages | Main Applications | Execution Standards |
1.Excellent corrosion resistance | 1.Medical components | GB/T 3621 |
2.Excellent fatigue strength | 2.Chemical components | AMS 4911 |
3.Good machinability | 3.Marine components | ASTM B265 |
4.Good strength-to-weight ratio | 4.Racing components | AMS-T-904 |
4,Technical Parameters:
Element | Ti | Al | V | Fe | C | N | H | O | Other Single | Other Total |
Min | Balance | 5.5 | 3.5 | |||||||
Max | Balance | 6.75 | 4.5 | 0.3 | 0.08 | 0.05 | 0.015 | 0.2 | 0.1 | 0.4 |
Room - Temperature Tensile Properties | High - Temperature Mechanical Properties | |||
Minimum | Minimum | Minimum | ||
Tensile Strength (Rm)/MPa | 895 | Tensile Strength (Rm)/MPa | 590 | 440 |
Yield Strength (Rp0.2)/MPa | 825 | Test Stress (σ)/MPa | 540 | 195 |
Elongation after Fracture (A)/% | 9 | Test Time (t)/h | 100 | 100 |
Reduction of Area (Z)/% | - | Test Temperature/℃ | 400 | 500 |
5,Product Showcase 6,Mechanical/Mechanical Properties of Titanium and Titanium Alloy
Plates
Alloy | Condition | Thickness Range/mm | Tensile Strength (Rm)/MPa | Yield Strength (Rp0.2)/MPa | Elongation after Fracture /% ≥ | Bending Radius |
TA2 | M | 0.3 - 1.0 | 440 - 620 | ≥320 | ≥35 | ≥100°, 3t |
> 1.0 - 2.0 | 440 - 620 | ≥320 | ≥30 | ≥100°, 3t | ||
> 2 - 5.0 | 440 - 620 | ≥320 | ≥25 | ≥90°, 3t | ||
> 5 - 10.0 | 440 - 620 | ≥320 | ≥25 | - | ||
> 10.0 - 30 | 440 - 620 | ≥320 | ≥18 | - | ||
TC4 | M | 0.5 - 1.8 | 925 - 1150 | ≥870 | ≥12 | ≥105°, 9t |
> 1.8 - 4.0 | 925 - 1150 | ≥870 | ≥12 | ≥105°, 10t | ||
> 4.0 - 5.0 | 925 - 1150 | ≥870 | ≥10 | ≥105°, 10t | ||
> 5.0 - 10.0 | 925 - 1150 | ≥825 | ≥10 | - | ||
> 10.0 - 100 | 925 - 1150 | ≥825 | ≥9 | - |
Alloy | Condition | Thickness Range/mm | Tensile Strength (Rm)/MPa | Test Temperature/℃ | Test Stress(σ)/MPa | Test Time(t)/h |
TC4 | M | 0.5 - 30.0mm | ≥590 | 400 | 540 | ≥100 |
≥540 | 500 | 195 |
TC4 Ti-6Al-4V Titanium Sheet For Aerospace High Performance Materials For Aircraft
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