© ISO 2012 Wrought aluminium and aluminium alloys — Cold drawn rods/bars and tubes and wires — Part 2 Mechanical properties Aluminium et alliages d’aluminium corroyés — Barres, tubes et fils étirés à[.]
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Wrought aluminium and aluminium alloys — Cold-drawn rods/bars and tubes and wires —
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© ISO 2012
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3 Terms and definitions 1
4 Tensile testing 1
5 Mechanical properties 1
Annex A (normative) Rules for rounding 15
Annex B (normative) List of tempers used in Tables 1 and 2 16
Bibliography 18
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Trang 4ISO (the International Organization for Standardization) is a worldwide federation of national standards bodies (ISO member bodies) The work of preparing International Standards is normally carried out through ISO technical committees Each member body interested in a subject for which a technical committee has been established has the right to be represented on that committee International organizations, governmental and non–governmental, in liaison with ISO, also take part in the work ISO collaborates closely with the International Electrotechnical Commission (IEC) on all matters of electrotechnical standardization.
International Standards are drafted in accordance with the rules given in the ISO/IEC Directives, Part 2 The main task of technical committees is to prepare International Standards Draft International Standards adopted by the technical committees are circulated to the member bodies for voting Publication as an International Standard requires approval by at least 75 % of the member bodies casting a vote.
Attention is drawn to the possibility that some of the elements of this document may be the subject of patent rights ISO shall not be held responsible for identifying any or all such patent rights.
ISO 6363-2 was prepared by Technical Committee ISO/TC 79, Light metals and their alloys, Subcommittee
SC 6, Wrought aluminium and aluminium alloys.
This second edition cancels and replaces the first edition (ISO 6363-2:1993) which has been technically revised.
ISO 6363 consists of the following parts, under the general title Wrought aluminium and aluminium alloys —
Cold-drawn rods/bars, tubes and wires:
— Part 1: Technical conditions for inspection and delivery
— Part 2: Mechanical properties
— Part 3: Drawn round bars and wires — Tolerances on form and dimensions (symmetric plus and minus
tolerances on diameter)
— Part 4: Drawn rectangular bars and wires — Tolerances on form and dimensions
— Part 5: Drawn square and hexagonal bars and wires — Tolerances on form and dimensions
— Part 6: Drawn round tubes — Tolerances on form and dimensions
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1 Scope
This part of ISO 6363 specifies the mechanical properties of wrought aluminium and aluminium alloy rods/bars, tubes and wires for general engineering applications (except aeronautical rivets).
It applies to products which are extruded and then cold drawn.
It does not apply to:
— products which are rolled and then cold drawn, including seam-welded tubes;
— forging stock, wire for drawing stock;
— drawn wires for aeronautical application, electrical or welding purposes.
2 Normative references
The following referenced documents are indispensable for the application of this document For dated references, only the edition cited applies For undated references, the latest edition of the referenced document (including any amendments) applies.
ISO 6363-1, Wrought aluminium and aluminium alloys — Cold-drawn rods/bars, tubes and wires — Part 1:
Technical conditions for inspection and delivery
ISO 6892-1, Metallic materials — Tensile testing — Part 1: Method of test at room temperature
ASTM B557M, Standard Test Methods for Tension Testing Wrought and Cast Aluminum- and
Values for mechanical properties of aluminium and aluminium alloys are given in Tables 1 and 2.
For elongation, two different gauge lengths are used The choice of the gauge length for elongation
measurements (A or A50mm) is at the discretion of the producer, unless otherwise agreed.
NOTE A is the percentage elongation on a gauge length of 5,65 So · A50mm is the percentage elongation on a gauge length of 50 mm
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Table 1 — Mechanical properties of rods/bars and wires
Rm
MPa
0,2 % proof stress
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Rm
MPa
0,2 % proof stress
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`,,```,,,,````-`-`,,`,,`,`,,` -Alloy Temper Dimensionsa Tensile strength
Rm
MPa
0,2 % proof stress
H18H28H38
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Rm
MPa
0,2 % proof stress
a D (mm) = diameter for round bar.
S (mm) = width across flats for square and hexagonal bar, thickness for rectangular bar
b Guaranteed values agreed upon between the purchaser and the supplier where requested by the purchaser
c The mechanical properties of temper grade T42 shall be applied only where the material of temper grade O has been naturally age-hardened after solution treatment by the purchaser If the material is cold or hot worked prior to solution treatment by the purchaser, its mechanical properties may be lower than the specified values
d The mechanical properties of temper grade T62 shall be applied only where the material of temper grade O has been artificially age-hardened after solution treatment by the purchaser If the material is cold or hot worked prior to solution treatment by the purchaser, its mechanical properties may be lower than the specified values
e Mechanical properties shall be tested in T4 temper (alloys 2017A, 2117 and 2024) or T6 temper (alloy 2014A).Testing may also be carried out in T42 temper or T62 temper, instead of T4 or T6 respectively In this case, the mechanical property limits are those given for the corresponding T4 and T6 tempers
f The material of temper grade O shall be a basis for materials of temper grades T42 or T62 Where requested by the purchaser, the capability to achieve T42 or T62 properties after appropriate heat treatment is demonstrated
g Applicable to those after extrusion followed by controlled cooling at a rate rapid enough to hold constituents in solution
h Mechanical properties shall be tested in T6 temper Testing may also be carried out in T62 temper, instead of T6 In this case, the mechanical property limits are those given for the corresponding T6 tempers
i For these tempers, the mechanical properties are very dependent on the amount of cold work and, for T89 temper, on the ageing conditions It is recommended that these characteristics be agreed between the supplier and purchaser Consequently, typical values
of Rp0,2 and elongation are not given
Table 1 (continued)
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T6510T6511
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Rm
MPa
0,2 % proof stress
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H18H38
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Rm
MPa
0,2 % proof stress
H18H28H38
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Rm
MPa
0,2 % proof stress
T6510T6511
b The material of temper grade O shall be a basis for materials of temper grades T42 or T62 Where requested by the purchaser,
the capability to achieve T42 or T62 properties after appropriate heat treatment is demonstrated
c The mechanical properties of temper grade T42 shall be applied only where the material of temper grade O has been naturally
age-hardened after solution treatment by the purchaser If the material is cold or hot worked prior to solution treatment by the purchaser,
its mechanical properties may be lower than the specified values
d For temper grade H22, proof stress shall not apply
e Applicable for those after extrusion followed by controlled cooling at a rate rapid enough to hold constituents in solution
f The mechanical property values of temper grade T62 shall be applied where the purchaser carries out solution heat treatment
and subsequent artificial age-hardening treatment for temper grade O However, where a certain cold working or hot working has been
conducted by the purchaser prior to solution heat treatment, the values of mechanical properties may occasionally be lower than the
specified limits
Table 2 (continued)
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A.1.1 Mechanical and chemical properties
The results of mechanical and chemical tests shall be rounded using either the rules specified in the International Standard specifying the method of test or, if the value obtained contains a larger number of significant figures than the guaranteed value, the generally accepted rules for rounding.
A.1.2 Dimensional characteristics
The results of determinations of dimensions (length, width, thickness, rounding, etc.) and shape (squaring, cambering, straightness, flatness, kinking, circularity, etc.) are not rounded These shall comply with the specification in the relevant International Standard, taking into account permissible tolerances also given in that International Standard.
A.2 Rounding of determination of compliance
In recording test results, the number representing the result of a test to determine a given property or to determine chemical composition should be expressed to the same number of decimal places as the corresponding number in the relevant International Standard.
The following rules should be used for rounding.
a) Where the figure immediately after the last figure to be retained is less than 5, the last figure to be retained remains unchanged.
b) Where the figure immediately after the last figure to be retained is greater than 5, or equal to 5 and followed
by at least one figure other than zero, the last figure to be retained remains unchanged if even and is increased by one if odd.
c) Where the figure immediately after the last figure to be retained is equal to 5 and followed by zeros only, the last figure to be retained remains unchanged if even and is increased by one if odd.
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(normative)
List of tempers used in Tables 1 and 2
Table B.1 — Description of the tempers used in Tables 1 and 2
F As fabricated (no mechanical property limits specified)
O Annealed — products achieving the required annealed properties after hot forming processes may be
designated as O temperH11 Strain-hardened — 1/8 hard
H111 Annealed and slightly strain-hardened (less than H11) during subsequent operations such as stretching or
straighteningH12 Strain-hardened — 1/4 hard
H18 Strain-hardened — 4/4 hard (fully hardened)
H22 Strain-hardened and partially annealed — 1/4 hard
H24 Strain-hardened and partially annealed — 1/2 hard
H26 Strain-hardened and partially annealed — 3/4 hard
H28 Strain-hardened and partially annealed — 4/4 hard (fully hardened)
H32 Strain-hardened and stabilized — 1/4 hard
H34 Strain-hardened and stabilized — 1/2 hard
H36 Strain-hardened and stabilized — 3/4 hard
H38 Strain-hardened and stabilized — 4/4 hard (fully hardened)
T3 Solution heat-treated, cold worked and naturally aged
T351 Solution heat-treated, stress-relieved by stretching a controlled amount (permanent set 1 %, to 3 %) and
naturally aged The products receive no further straightening after stretchingT3510 Solution heat-treated, stress-relieved by stretching a controlled amount (permanent set 1 % to 3 %) and
naturally aged The products receive no further straightening after stretchingT3511 Same as T3510 except that minor straightening is allowed after stretching to comply with standard
tolerancesT39* Solution heat-treated and cold worked an appropriate amount to achieve the specified mechanical
properties Cold work may be carried out before or after natural ageingT4 Solution heat-treated and naturally aged
T42 Solution heat-treated and naturally aged Applies to test material heat-treated from annealed or F temper or
to products heat-treated from any temper by the userT451 Solution heat-treated, stress-relieved by stretching a controlled amount (permanent set 1 % to 3 %) and
naturally aged The products receive no further straightening after stretchingT4510 Solution heat-treated, stress-relieved by stretching a controlled amount (permanent set 1 % to 3 %) and
naturally aged The products receive no further straightening after stretchingT4511 Same as T4510 except that minor straightening is allowed after stretching to comply with standard
tolerancesT5 Cooled from an elevated temperature shaping process and then artificially aged
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`,,```,,,,````-`-`,,`,,`,`,,` -formabilityT651 Solution heat-treated, stress-relieved by stretching a controlled amount (permanent set 1 % to 3 %) and
then artificially aged The products receive no further straightening after stretchingT6510 Solution heat-treated, stress-relieved by stretching a controlled amount (permanent set 1 % to 3 %) and
then artificially aged The products receive no further straightening after stretchingT6511 Same as T6510 except that minor straightening is allowed after stretching to comply with standard
tolerancesT66* Solution heat-treated and then artificially aged — mechanical property level higher than T6 achieved
through special control of the process (6000 series alloys)T7 Solution heat-treated, and then artificially overaged
T73 Solution heat-treated, and then artificially overaged in order to achieve the best stress corrosion resistanceT73510 Solution heat-treated, stress-relieved by stretching a controlled amount (permanent set 1 % to 3 %) and
then artificially overaged in order to achieve the best stress corrosion resistance The products receive no further straightening after stretching
T73511 Same as T73510 except that minor straightening is allowed after stretching to comply with standard
tolerancesT8 Solution heat-treated, cold worked and then artificially aged
T832* Solution heat-treated, cold worked a controlled specific amount and then artificially aged (applied to 6063
drawn tube)T851 Solution heat-treated, stress-relieved by stretching a controlled amount (permanent set 1 % to 3 %) and
then artificially aged The products receive no further straightening after stretchingT8510 Solution heat-treated, stress-relieved by stretching a controlled amount (permanent set 1 % to 3 %) and
then artificially aged The products receive no further straightening after stretchingT8511 Same as T8510 except that minor straightening is allowed after stretching to comply with standard
tolerancesT89a Solution heat-treated, cold worked an appropriate amount to achieve the specified mechanical properties
and then artificially agedT9 Solution heat-treated, artificially aged and then cold worked
a Regional designation quoted from EN 754-2
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