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High Strength Titanium Forged Components TA1 TA2 TC4 GR1 for Aerospace

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High Strength Titanium Forged Components TA1 TA2 TC4 GR1 for Aerospace

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Brand Name :	JIMA Aluminum
Model Number :	8011,3003，5005,5052
Certification :	IRIS,ISO9001，ISO 14001.
Price :	Negotiations
Payment Terms :	T/T, L/C
Supply Ability :	2000 MT per month
Delivery Time :	20~25days

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High Strength Titanium Forged Components TA1 TA2 TC4 GR1 for Aerospace

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	-

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