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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).
Pursuant to seven ANSI H35 standards, The Aluminum Association registers and publishes specifications describing the composition, mechanical properties and nomenclature of aluminum alloys in the United States. [2] These alloys are identified by the abbreviation "AA", for example AA 6061-T6.
The Questar XLS is made from bolted-together 6061-T6 aluminum tubing, with its flying surfaces covered in doped aircraft fabric. Its 31.30 ft (9.5 m) span wing has a wing area of 146.0 sq ft (13.56 m 2), is supported by "V" struts and the wing can be detached in ten minutes for ground transport or storage.
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
Tempered 6061 aluminium alloy has a density of 2700 kg/m 3, modulus of 69 GPa, and tensile strength of 310 MPa, respectively. [ 24 ] Ti-6Al-4V standard specifications include: [ 25 ] [ 26 ]
T6 temper 6063 has an ultimate tensile strength of at least 190 MPa (28,000 psi) and yield strength of at least 160 MPa (23,000 psi). In thicknesses of 3.15 millimetres (0.124 in) or less, it has elongation of 8% or more; in thicker sections, it has elongation of 10%.
The aircraft is made from 6061-T6 aluminum sheet over a cage of welded aluminum square 6061-T6 aluminum tube. The tail boom is conventional semi-monocoque construction. The non-tapered planform wings have 6061-T6 ribs and spars and employ a NACA 4413 (mod) airfoil. The airfoil modification removes the undercamber on the bottom of the wing ...
The aircraft fuselage is made from bolted-together 6061-T6 aluminium tubing, with a carbon fibre tail boom and support struts. Its two-bladed rotor has a diameter of 5.5 m (18.0 ft) and a chord of 17 cm (6.7 in).
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