Page 47 - Welding of Aluminium and its Alloys
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Material standards, designations and alloys  39

               a low temperature to soften them to the required degree of hardness
               and strength.
            •  H3 – strain hardened and stabilised. Stabilisation is a low-temperature
               heat treatment applied during or on completion of fabrication. This
               improves ductility and stabilises the properties of those strain-hardened
               alloys that soften with time.
            •  H4 – strain hardened and painted. This is for alloys that may be sub-
               jected to low-temperature heat treatment as part of a paint baking or
               adhesive curing operation.
            The second digit after ‘H’ indicates the amount of strain hardening in the
            alloy. H18 is strain hardened only and in the most heavily cold worked con-
            dition. It is therefore the hardest and highest strength condition. Ductility
            will be very low and further cold work may cause the component to crack.
            Intermediate conditions are identified by the numbers 1 to 7 and are based
            on the strength relative to that of the annealed alloy, O condition and the
            H18 condition, e.g. an H14 alloy will have a strength halfway between the
            annealed and fully hard condition, H12 halfway between O and H14.There
            is an H9 condition in which the ultimate tensile strength exceeds that of the
                                               2
            H8 condition by a minimum of 10N/mm .
              The third digit after ‘H’ is not mandatory and is used when the alloy
            requires special control to achieve the specific temper identified by the
            second digit or when some other characteristic of the alloy is  affected.
            Examples of such characteristics are exfoliation corrosion resistance, seam
            welded tube or additional working after the final temper has been achieved,
            e.g. by embossing.
              The ‘T’ designations are applied to those alloys that are age hardened,
            the first digit identifying the basic heat treatment:

            •  T1 – cooled from an elevated temperature-shaping treatment and
               naturally aged.
            •  T2 – cooled from an elevated temperature-shaping process, cold worked
               and naturally aged.
            •  T3 – solution heat treated, cold worked and naturally aged.
            •  T4 – solution heat treated and naturally aged.
            •  T5 – cooled from an elevated temperature-shaping process and artifi-
               cially aged.
            •  T6 – solution heat treated and artificially aged.
            •  T7 – solution heat treated and overaged or stabilised.
            •  T8 – solution heat treated, cold worked and artificially aged.
            •  T9 – solution heat treated, artificially aged and cold worked.
            More digits may be added to the designation to indicate variations in heat
            treatments or cold work. For example, TX51, 510, 511, 52 or 54 all indicate
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