Page 977 - MiSUMi FA Mechanical Components Economy Series
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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   k
            Alloy            Materials  has worse corrosion resistance.
            Al−Cu     A2017  General-Use   High Strength and Machinability Duralumin  k  k  k
            Alloy            Strength Materials
            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 fi ne machined surface and high corrosion resistance to seawater. It   JIS H 4000  k
            Alloy            Parts    has fi ne machined surface and high corrosion resistance to seawater.
            Al−M −Si  A6061  General Machine   Heat-treated corrosion resisting alloy.  k  k
            Alloy            Parts    High durability owing to T6 treatment.
            Al−M −Si         General Machine  Weaker than 6061, but more extrudable. Applicable to complex cross-sections shapes.  k  k  k
            Alloy     A6063  Parts and Structural Material Good corrosion resistance and surface treatment.
            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          Defi nition                            Description
                                          Completed as a product, without any order for thermal refi ning. Extruded or forged material,
               F     Plain Manufactured Material
                                          not thermally refi ned.
              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
                     annealing.
                                          below the annealing temperature to prevent the eff ect of annealing completely.
                 H1n  Hardened by cold working.  n is a numeral from 1 to 9, representing the degree of hardening. "8" represents hard material,
                                          and "4"represents the state halfway 1/2 between 0 and hard material. "2" represents the level
             H   H2n  Hardened and then properly softened by heat.
                                          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                        is typical material processed in this way. Cold working such as correction may be conducted unless it aff ects the strength.
                     and then allowed to age naturally.  Used for an alloy such as 6063, for which the eff ect of quenching can be realized by cooling after hot working (extrusion).
                     Allowed to age naturally after solution   Cold working is conducted for plates, rods, tubes, etc. to enhance the strength in some
                T3                        cases, and to improve the corrective dimension precision in other cases, with an obvious
                     treatment and cold working.  eff ect. 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.
                                          however, aging is a longer process. The tensile property upon the elapse of one month is adopted as
                T4   Natural aging after solution   Aging is usually completed after exposure to ambient temperature for approx. 4 days. In the case of 7NO1,
                     treatment            referential data. The variety that is given T4 treatment by a user under specifi ed conditions is called T42.
                     Hardened through artifi cial aging after   Hardened through artifi cial aging to improve the mechanical properties and stabilize the dimensions. Used for an
                T5
                     high-temperature processing and quenching alloy or casting such as 6063, for which the eff ect of quenching can be realized by cooling after hot working (extrusion).
                     Hardened through artifi cial aging  Excellent strength can be attained for a thermally treated alloy without cold working in the typical heat
                T6
                     after solution treatment.  treatment process. An item that is given T6 treatment by a user under specifi ed conditions is called T62.
             T       Wrought Materials:   Quenched with lukewarm water to prevent distortion due to the main hardening.
                         Hardened through artifi cial 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
                                          Overaging surpassing those needed for hardening through artifi cial aging is carried out to attain the
                T7   Stabilized after solution treatment
                                          maximum strength, because special properties are adjusted somewhat at the expense of strength.
                     Overaging after solution   Overaging after solution treatment to rectify the tendency to crack due to corrosion under stress.
                T73
                     treatment.           Specifi ed in 7075, forgings, of JIS.
                     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 artifi cial aging  Cold working performed, with a noticeable eff ect, 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   artifi cial aging subsequent to   Cold working is necessary to enhance the strength.
                     solution treatment.
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