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Ti-6Al-4V. Ti-6Al-4V (UNS designation R56400 ), also sometimes called TC4, Ti64, [ 1] or ASTM Grade 5, is an alpha-beta titanium alloy with a high specific strength and excellent corrosion resistance. It is one of the most commonly used titanium alloys and is applied in a wide range of applications where low density and excellent corrosion ...
2024 aluminium alloy is an aluminium alloy, with copper as the primary alloying element. It is used in applications requiring high strength-to-weight ratio, as well as good fatigue resistance. It is weldable only through friction welding, and has average machinability. Due to poor corrosion resistance, it is often clad with aluminium or Al-1Zn ...
Ti-6Al-2Sn-4Zr-2Mo. Ti-6Al-2Sn-4Zr-2Mo (UNS designation R54620 ), also known as Ti 6-2-4-2, is a near alpha titanium alloy known for its high strength and excellent corrosion resistance. It is often used in the aerospace industry for creating high-temperature jet engines and the automotive industry to create high performance automotive valves.
Titanium alloys are generally classified into four main categories: [ 1] Alpha alloys which contain neutral alloying elements (such as tin) and/ or alpha stabilisers (such as aluminium or oxygen) only. These are not heat treatable. Examples include: [ 2] Ti-5Al-2Sn-ELI, Ti-8Al-1Mo-1V. Near-alpha alloys contain small amount of ductile beta-phase.
6061 sheet in the T4 condition can be formed with limited ductility in the cold state. For deep draw and complex shapes, and for the avoidance of spring-back, an aluminium hot stamping process ( Hot Form Quench ) can be used, which forms a blank at a elevated temperature (~ 550 C) in a cooled die, leaving a part in W-temper condition before ...
List of Air Ministry specifications. This is a partial list of the British Air Ministry (AM) specifications for aircraft. A specification stemmed from an Operational Requirement, abbreviated "OR", describing what the aircraft would be used for. This in turn led to the specification itself, e.g. a two-engined fighter with four machine guns.
Typical material properties for 2014 aluminium alloy are: [ 5] Density: 2.80 g/cm 3, or 175 lb/ft 3. Young's modulus: 73 GPa, or 11 Msi. Electrical conductivity: 34 to 50% IACS. Ultimate tensile strength: 190 to 480 MPa, or 28 to 70 ksi. Thermal Conductivity: 130 to 190 W/m-K. Thermal Expansion: 23 μm/m-K.
The Unified Numbering System for Metals and Alloys ( UNS) is an alloy designation system widely accepted in North America. Each UNS number relates to a specific metal or alloy and defines its specific chemical composition, or in some cases a specific mechanical or physical property. A UNS number alone does not constitute a full material ...