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6Al-6V-2Sn

6Al-6V-2Sn Titanium

6Al-6V-2Sn Titanium (6-6-2) is a heat treatable, high strength titanium alloy with higher strength and section hardenability that 6Al-4V. but with lower toughness and ductility and limited weldability. The typical applications, but not limited to, of 6Al-6V-2Sn include airframe and jet engine parts, rocket engine cases, and ordnance components. If you have a current or upcoming project requiring 6Al-6V-2Sn please Request a Quote to see if Fighter Jet Metals is a good fit for your program requirements.

A close-up view of a stack of shiny, cylindrical metal rods resting in a workshop. The rods, likely forged from fighter jet metals, are uniformly cut with smooth surfaces, arranged parallel to each other, and the background contains blurred machinery and workshop tools.

ROUND BAR

6Al-6V-2Sn Round Bar diameters range from 0.125″ to 14.00″ diameter.
A stack of flat metal bars piled on top of each other. The bars, possibly crafted from fighter jet metals, are aligned horizontally, showcasing their thin, rectangular shape and metallic finish. The image highlights the texture and edges of the bars in close detail.

FLAT BAR

6Al-6V-2Sn Flat Bar comes in a variety of thicknesses and widths. For more information please request a quote.
Close-up of several stacked aluminum sheets in an industrial setting. The smooth, reflective surfaces of the sheets are clearly visible, akin to the polished finish found in fighter jet metals. The edges show precision cuts, and the background includes blurred industrial equipment and shelving units.

PLATE

6Al-6V-2Sn Plate Thickness ranges from 0.1875″ to 6.50″ Thick.
A stack of shiny, rectangular metal sheets, reminiscent of fighter jet metals, is placed on a wooden palette in an industrial setting. The sheets have smooth surfaces and uniform thickness, with the image focused on the layered edges. The background shows blurred industrial equipment.

SHEET

6Al-6V-2Sn Sheet Thicknesses range from 0.002″ to .150″ Thick.

Applications of 6Al-6V-2Sn

WING SPARS

The wing spars of an aircraft are the structural beams that run along the length of the wing and provide support for the wing’s skin and other components. They are typically made from high-strength materials such as 6Al-6V-2Sn in order to support the loads placed on the wing during flight.

FUSELAGE FRAME

The fuselage of an aircraft is the main body of the aircraft, and the fuselage frames are the structural components that give the fuselage its shape and support the skin. These frames are typically made from high-strength materials such as 6Al-6V-2Sn in order to support the loads placed on the fuselage during flight.

LANDING GEAR

The fuselage of an aircraft is the main body of the aircraft, and the fuselage frames are the structural components that give the fuselage its shape and support the skin. These frames are typically made from high-strength materials such as 6Al-6V-2Sn in order to support the loads placed on the fuselage during flight.

LANDING GEAR

The fuselage of an aircraft is the main body of the aircraft, and the fuselage frames are the structural components that give the fuselage its shape and support the skin. These frames are typically made from high-strength materials such as 6Al-6V-2Sn in order to support the loads placed on the fuselage during flight.

A table shows the content range of various elements in a material used for fighter jet metals. Titanium: 82.89-87.8, Aluminum: 5-6, Vanadium: 5-6, Tin: 1.5-2.5, Iron: 0.35-1, Copper: 0.35-1, Oxygen: ≤0.20,

6Al-6V-2Sn TITANIUM SPECIFICATIONS

SHEET & PLATE

GULFSTREAM AEROSPACE SPECIFICATIONS

BOEING SPECIFICATIONS

BARS & FORGINGS

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