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  2. 6061 aluminium alloy - Wikipedia

    en.wikipedia.org/wiki/6061_aluminium_alloy

    6061-T6 aluminium standard heat treating process. T6 temper 6061 has been treated to provide the maximum precipitation hardening (and therefore maximum yield strength) for a 6061 aluminium alloy. It has an ultimate tensile strength of at least 290 MPa (42 ksi) and yield strength of at least 240 MPa (35 ksi).

  3. Titanium alloys - Wikipedia

    en.wikipedia.org/wiki/Titanium_alloys

    contains 4.5% aluminium, 2% molybdenum, 1.6% vanadium, 0.5% iron, and 0.3% silicon. Grade 36 contains 45% niobium. Grade 37 contains 1.5% aluminium. Grade 38 contains 4% aluminium, 2.5% vanadium, and 1.5% iron. This grade was developed in the 1990s for use as an armor plating. The iron reduces the amount of Vanadium needed as a beta stabilizer.

  4. 6060 aluminium alloy - Wikipedia

    en.wikipedia.org/wiki/6060_aluminium_alloy

    6060 aluminium alloy is an alloy in the wrought aluminium-magnesium-silicon family (6000 or 6xxx series). It is much more closely related to the alloy 6063 than to 6061. The main difference between 6060 and 6063 is that 6063 has a slightly higher magnesium content.

  5. Strain hardening exponent - Wikipedia

    en.wikipedia.org/wiki/Strain_hardening_exponent

    Aluminum 1100–O (annealed) 0.20: 180 2024 aluminum alloy (heat treated—T3) 0.16: 690 5052-O 0.13 210 Aluminum 6061–O (annealed) 0.20: 205 Aluminum 6061T6: 0.05: 410 Aluminum 7075–O (annealed) 0.17: 400 Brass, Naval (annealed) 0.49: 895 Brass 70–30 (annealed) 0.49: 900 Brass 85–15 (cold-rolled) 0.34: 580 Cobalt-base alloy (heat ...

  6. Aluminium alloy - Wikipedia

    en.wikipedia.org/wiki/Aluminium_alloy

    The temper designation follows the cast or wrought designation number with a dash, a letter, and potentially a one to three digit number, e.g. 6061-T6. The definitions for the tempers are: [5] [6]-F : As fabricated-H : Strain hardened (cold worked) with or without thermal treatment -H1 : Strain hardened without thermal treatment

  7. Aluminium–magnesium–silicon alloys - Wikipedia

    en.wikipedia.org/wiki/Aluminium–magnesium...

    In addition, there is the phase before the for the Aluminium-copper alloys are typical. Alloys with higher copper content (alloyings 6061, 6056, 6013) are mainly used in aviation. Iron occurs in all aluminium alloys as an impurity in quantities of 0.05-0.5%.

  8. 6063 aluminium alloy - Wikipedia

    en.wikipedia.org/wiki/6063_aluminium_alloy

    6063 is the most common alloy used for aluminium extrusion. It allows complex shapes to be formed with very smooth surfaces fit for anodizing and is popular for visible architectural applications such as window frames, door frames, roofs, and sign frames. [3] Applications requiring higher strength typically use 6061 or 6082 instead.

  9. 6105 aluminium alloy - Wikipedia

    en.wikipedia.org/wiki/6105_aluminium_alloy

    6105 aluminium alloy is an alloy in the wrought aluminium-magnesium-silicon family (6000 or 6xxx series). It is one of the least common of the alloys in this series. While most wrought aluminium alloys are covered by multiple standards (from any mixture of ASTM, EN, ISO, and national standard bodies), 6105 is only dealt with in ASTM B221: Standard Specification for Aluminum and Aluminum-Alloy ...

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