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3.Aluminum Alloy Materials
             Type   Material Code Applications  Comment             JIS  Flat Bar Square Bar Hexagonal Bar Round Bar Section Steel
          Al−Cu      A2011  General-Use Strength  Free-Cutting Alloy. It excels in machinability but
          Alloy            Materials  has worse corrosion resistance.               k
          Al−Cu            General-Use
          Alloy      A2017  Strength Materials  High Strength and Machinability Duralumin  k  k  k
          Al−M             General Machine  Most typical aluminum alloy with medium strength.
          Alloy      A5052  Parts Covers, cases, etc. With high fatigue strength in comparison with its strength and high corrosion resistance to seawater.   k  k
          Al−M       A5056  General Machine   It has fine machined surface and high corrosion resistance to seawater. It   JIS H 4000  k
          Alloy            Parts    has fine machined surface and high corrosion resistance to seawater.
          Al−M −Si   A6061  General Machine   Heat-treated corrosion resisting alloy.
          Alloy            Parts    High durability owing to T6 treatment.  k       k
          Al−M −Si         General Machine  Weaker than 6061, but more extrudable. Applicable to complex cross-sections shapes.
          Alloy      A6063  Parts and Structural Material Good corrosion resistance and surface treatment.   k  k  k
          Al−Zn−M                   It is one of the strongest aluminum alloys but has
          Alloy      A7075  Jigs and Dies  worse corrosion resistance. Extra Super Duralumin  k
          JIS Acronyms for Non-Ferrous Metal
             P     Plate, Strip, Disk           TW     Welded Tube
             PC    Laminate                     TWA    Arc-Welded Tube
             BE    Extruded Bar                  S     Extruded Section
             BD    Drawn Bar                     BR    Riveted Bar
             W     Drawn Wire                    FD    Die-Forged Part
             TE    Seamless Extruded Tube        FH    Free-Forged Part
             TD    Seamless Drawn Tube
          Quality Codes for Aluminum and Aluminum Alloys
            Code          Definition                            Description
              F    Plain Manufactured Material  Completed as a product, without any order for thermal refining. Extruded or forged material,
                                        not thermally refined.
            H112   Wrought material, for which certain mechanical properties are guaranteed without the need of hardening.
             O     Brought into the softest state by  Completely re-crystallized by annealing. A thermally treated alloy should be cooled at a temperature
                                        below the annealing temperature to prevent the effect of annealing completely.
                   annealing.
               H1n  Hardened by cold working.  n is a numeral from 1 to 9, representing the degree of hardening. "8" represents hard material,
           H   H2n  Hardened and then properly softened by heat.  and "4"represents the state halfway 1/2 between 0 and hard material. "2" represents the level
                                        halfway between 0 and 1/2 hardness, and "6" the state halfway between 1/2 hardness and hard
               H3n  Stabilized after cold working.  material.
                   Cooled after high-temperature working  Quenched at the end of a cold working process and allowed to age and harden at ambient temperature. Extruded material
               T1  and then allowed to age naturally.  is typical material processed in this way. Cold working such as correction may be conducted unless it affects the strength.
                                        Used for an alloy such as 6063, for which the effect of quenching can be realized by cooling after hot working (extrusion).
               T3  Allowed to age naturally after solution   Cold working is conducted for plates, rods, tubes, etc. to enhance the strength in some
                                        cases, and to improve the corrective dimension precision in other cases, with an obvious
                   treatment and cold working.
                                        effect. T361 when cold working is performed to a higher degree than that for T3.
                   Allowed to age naturally after   Cold working is conducted to enhance the strength after solution treatment, and then it is tension processed
               T351 solution            to give 1.5% to 3% permanent distortion to remove residual tension, and allowed to age naturally.
                   treatment and cold working.
                   Natural aging after solution   Aging is usually completed after exposure to ambient temperature for approx. 4 days. In the case of 7NO1,
               T4  treatment            however, aging is a longer process. The tensile property upon the elapse of one month is adopted as
                                        referential data. The variety that is given T4 treatment by a user under specified conditions is called T42.
               T5  Hardened through artificial aging after   Hardened through artificial aging to improve the mechanical properties and stabilize the dimensions. Used for an
                   high-temperature processing and quenching alloy or casting such as 6063, for which the effect of quenching can be realized by cooling after hot working (extrusion).
               T6  Hardened through artificial aging  Excellent strength can be attained for a thermally treated alloy without cold working in the typical heat
                   after solution treatment.
                                        treatment process. An item that is given T6 treatment by a user under specified conditions is called T62.
           T       Wrought Materials:   Quenched with lukewarm water to prevent distortion due to the main hardening.

                        Hardened through artificial aging
               T61      after solution treatment by  The conditions for hardening through artificial aging are adjusted to attain strength
                        quenching with lukewarm water.  exceeding that accomplished by regular T6 treatment.
                   Casting:Tempered after hardening
               T7  Stabilized after solution treatment  Overaging surpassing those needed for hardening through artificial aging is carried out to attain the
                                        maximum strength, because special properties are adjusted somewhat at the expense of strength.
               T73  Overaging after solution   Overaging after solution treatment to rectify the tendency to crack due to corrosion under stress.
                                        Specified in 7075, forgings, of JIS.
                   treatment.
                   Overaging after removal of   Overaging after removal of residual stress by compression to retain 1% to 5% permanent deformation
               T7352 residual           subsequent to solution treatment, in order to rectify the tendency to crack due to corrosion under stress.
                   stress after solution treatment.  Included in free-forged part, 7075.
                   Hardened through artificial aging  Cold working performed, with a noticeable effect, to improve the mechanical properties or to rectify drawbacks
               T8  after cold working subsequent   or improve dimension precision. Called T83 when the sectional area is reduced 3%through cold working.
                   to solution treatment.  Called T86 when the reduction rate is 6%. These procedures are performed to enhance the strength.
                   Cold working after hardening through
               T9  artificial aging subsequent to   Cold working is necessary to enhance the strength.
                   solution treatment.
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