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Ti-1023 Titanium Alloy Forgings Ti-10V-2Fe-3Al UNS R56410

Material: Titanium Alloy
Composition: Ti-10V-2Fe-3Al
UNS Code: UNS R56410
Standard: AMS4983,AMS4984,AMS4986,AMS4987
Forms typically available: billet,bar,plate,Forgings
Free sample: KS10-2-3 St760ºC; Ti-10-2-3; TIMETAL 10-2-3
Certificate: EN10204-3.1, ISO9001,aerospace certificate

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+86 17719616665

Ti-10V-2Fe-3Al is a near beta alloy capable of a wide range of strengths depending on the heat treatment applied. The alloy has excellent forgeability, high toughness, and good hardenability which allows good properties in sections to 5" thick. Ti-10V-2Fe-3Al is used for high-strength aircraft forgings.

Ti-1023 Ti-10V-2Fe-3Al Composition

Element	Weight %
	Min.	Max.
Vanadium	9	11
Iron	1.6	2.2
Aluminum	2.6	3.4
Oxygen	-	0.13
Carbon	-	0.05
Nitrogen	-	0.05
Hydrogen	-	0.015
Residual Elements, each	-	0.1
Residual Elements, total	-	0.13
Titanium		Remainder

Ti-1023 Ti-10V-2Fe-3Al Physical properties

	English	SI
Density	0.168 lb in-3	4.65 g cm-3
Beta Transus	1470°F	800°C
Mean Coefficient of Thermal Expansion	5.4 x 10-6 in in-1 °F-1 @ 75°-800°F	9.7 x 10-6 mm-1 °C-1 @ 24°-427°C
Tensile Modulus	15.9 Msi	109.6 GPa
Compressive Modulus	16.3 Msi	112.3 GPa
Shear Modulus	6.1 Msi	42.1 GPa
Poisson's Ratio	0.32

Ti-1023 Ti-10V-2Fe-3Al Minimum Mechanical properties

Solution treated d then aged 8 hours

AMS Standard	Aging Temperature °F (°C)	Maximum Section Thickness in (cm)	Ultimate Tensile Strength ksi (MPa)	0.2% Yield Strength ksi (MPa)	Elongation % in 2 in	Reduction in Area %	Fracture Toughness ksi√in (MPa√m)
AMS 4984	900°-950° (482°-510°)	3 (7.6)	173 (1193)	160 (1103)	4	-	40 (44)
AMS 4986	950°-1000° (510°-538°)	4 (10.2)	160 (1103)	145 (998)	6	10	55 (60)
AMS 4987	1050°-1100° (566°-593°)	4 (10.2)	140 (965)	130 (896)	8	20	80 (88)