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AMS 4928 TC4 Ti-6Al-4V Titanium Alloy Bars Forged In 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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AMS 4928 TC4 Ti-6Al-4V Titanium Alloy Bars Forged In Aerospace

TC4 (Ti-6Al-4V) Titanium Alloy Rods and Bars 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, good 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), and the maximum operating temperature can reach 400°C. This material has good formability and excellent 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 2965
2.Excellent fatigue strength	2.Chemical components	GJB 2218A
3.Good machinability	3.Marine components	GJB 1538A
4.Good strength-to-weight ratio	4.Racing components	AMS 4928, ASTM B348, AMS-T-9047

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
Tensile Strength (Rm) / MPa	895	Tensile Strength (Rm) / MPa	600
Yield Strength (Rp0.2) / MPa	827	Test Stress (σ) / MPa	560
Elongation after Fracture (A) / %	10	Test Time (t) / h	100
Reduction of Area (Z) / %	25	Test Temperature / ℃	400

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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AMS 4928 TC4 Ti-6Al-4V Titanium Alloy Bars Forged In Aerospace

AMS 4928 TC4 Ti-6Al-4V Titanium Alloy Bars Forged In Aerospace

AMS 4928 TC4 Ti-6Al-4V Titanium Alloy Bars Forged In Aerospace

AMS 4928 Titanium Alloy Bars

Ti-6Al-4V Titanium Alloy Bars

TC4 Titanium Alloy Rods

AMS 4928 TC4 Ti-6Al-4V Titanium Alloy Bars Forged In Aerospace

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