MOQ: | 1PCS |
Price: | Negotiations |
Standard Packaging: | wooden pallet |
Delivery Period: | 20~25days |
Payment Method: | T/T, L/C |
Supply Capacity: | 2000 MT per month |
TA1 TA2 TC4 GR1 High Strength Aerospace Titanium Forged Components



1,Titanium Forging Application
1. Aerospace
Aircraft structural components
Jet engine components: fan blades, housings, disks, compressor blades, disks, short shafts, housings
Spacecraft components: blades for fuel tanks, attitude control engine housings, liquid fuel turbopumps
2. Turbine blades for power generation
3. Medical field
Implants: joint replacements (hip and knee implants), spinal implants and fixation devices
Surgical instruments: for the manufacture of surgical tools, forceps and scalpels
4. Automotive
High-performance engine components: connecting rods, crankshafts
Suspension systems
5. High-end equipment manufacturing
High-speed rail and rail transportation
Large machine tools and precision machinery
2.Product Details
Attribute
|
Details
|
Alloy
|
TA1, TA2, TA3, TA9, TC4, GR1, GR2, GR5
|
Standard
|
GB/T 2965 - 2007, GB/T 13810 - 2007, ASTM B348, ASTM F67, ASTM F136, AMS4928, MIL4911
|
Dimensions
|
Diameter: 3.0 - 200mm<br>Length: 1000 - 6000mm<br>Tolerance: H7 - H11
|
Applications
|
Metallurgy, Electronics, Medical, Chemical, Petroleum, Pharmaceutical, Aerospace
|
Process
|
α+β forging,β machining forging,Multi-directional die forging,Partial die forging,Isothermal die forging
|
MOQ
|
1PCS
|
Size
|
Customized
|
3,Production Photos



4,Product Features
High strength
Corrosion resistance
High fatigue and impact resistance
Thermal Stability. Titanium has a melting point of 1,668°C (3,034°F)
5,Mechanical/Mechanical Properties of Titanium forging
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
|
-
|
MOQ: | 1PCS |
Price: | Negotiations |
Standard Packaging: | wooden pallet |
Delivery Period: | 20~25days |
Payment Method: | T/T, L/C |
Supply Capacity: | 2000 MT per month |
TA1 TA2 TC4 GR1 High Strength Aerospace Titanium Forged Components



1,Titanium Forging Application
1. Aerospace
Aircraft structural components
Jet engine components: fan blades, housings, disks, compressor blades, disks, short shafts, housings
Spacecraft components: blades for fuel tanks, attitude control engine housings, liquid fuel turbopumps
2. Turbine blades for power generation
3. Medical field
Implants: joint replacements (hip and knee implants), spinal implants and fixation devices
Surgical instruments: for the manufacture of surgical tools, forceps and scalpels
4. Automotive
High-performance engine components: connecting rods, crankshafts
Suspension systems
5. High-end equipment manufacturing
High-speed rail and rail transportation
Large machine tools and precision machinery
2.Product Details
Attribute
|
Details
|
Alloy
|
TA1, TA2, TA3, TA9, TC4, GR1, GR2, GR5
|
Standard
|
GB/T 2965 - 2007, GB/T 13810 - 2007, ASTM B348, ASTM F67, ASTM F136, AMS4928, MIL4911
|
Dimensions
|
Diameter: 3.0 - 200mm<br>Length: 1000 - 6000mm<br>Tolerance: H7 - H11
|
Applications
|
Metallurgy, Electronics, Medical, Chemical, Petroleum, Pharmaceutical, Aerospace
|
Process
|
α+β forging,β machining forging,Multi-directional die forging,Partial die forging,Isothermal die forging
|
MOQ
|
1PCS
|
Size
|
Customized
|
3,Production Photos



4,Product Features
High strength
Corrosion resistance
High fatigue and impact resistance
Thermal Stability. Titanium has a melting point of 1,668°C (3,034°F)
5,Mechanical/Mechanical Properties of Titanium forging
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
|
-
|