logo
Send Message
Home ProductsTitanium Alloy

TC4 Ti-6Al-4V Titanium Sheet For Aerospace High Performance Materials For Aircraft

TC4 Ti-6Al-4V Titanium Sheet For Aerospace High Performance Materials For Aircraft

  • TC4 Ti-6Al-4V Titanium Sheet For Aerospace High Performance Materials For Aircraft
TC4 Ti-6Al-4V Titanium Sheet For Aerospace High Performance Materials For Aircraft
Product Details:
Place of Origin: CHINA
Brand Name: JIMA Aluminum
Certification: IRIS,ISO9001,ISO 14001.
Model Number: 8011,3003,5005,5052
Payment & Shipping Terms:
Minimum Order Quantity: Negotiations
Price: Negotiations
Packaging Details: wooden pallet
Delivery Time: 20~25days
Payment Terms: T/T, L/C
Supply Ability: 2000 MT per month
Contact Now
Detailed Product Description
Name: TC4 (Ti-6l-4V) Titanium Alloy Sheet Alloy: TC4 (Ti-6l-4V)
Execution Standards: GB/T 3621 AMS 4911 ASTM B265 AMS-T-9046 Application: Materials Used In Aerospace, Automotive And New Energy, Industrial Molds And Dies, And Semiconductor Fields
Highlight:

TC4 Titanium Sheet

,

High Performance Titanium Sheet

,

Aerospace Titanium Sheet

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


TC4 Ti-6Al-4V Titanium Sheet For Aerospace High Performance Materials For Aircraft 0
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
 

 

Contact Details
JIMA Aluminum

Contact Person: Annie

Tel: Whatsapp:+8615000729029

Send your inquiry directly to us (0 / 3000)

Other Products