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TC4 Ti-6Al-4V Titanium Forgings Sheet For Aerospace / Aircraft

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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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TC4 Ti-6Al-4V Titanium Forgings Sheet For Aerospace / Aircraft

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

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TC4 Ti-6Al-4V Titanium Forgings Sheet For Aerospace / Aircraft

TC4 Ti-6Al-4V Titanium Forgings Sheet For Aerospace / Aircraft

TC4 Ti-6Al-4V Titanium Forgings Sheet For Aerospace / Aircraft

TC4 Titanium Forgings

Ti-6Al-4V Titanium Sheet

Aerospace Titanium Forgings

TC4 Ti-6Al-4V Titanium Forgings Sheet For Aerospace / Aircraft

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