SIST EN 485-2:2004
(Main)Aluminium and aluminium alloys - Sheet, strip and plate - Part 2: Mechanical properties
Aluminium and aluminium alloys - Sheet, strip and plate - Part 2: Mechanical properties
This part of EN 485 specifies the mechanical properties of wrought aluminium and aluminium alloy sheet, strip and plate for general engineering applications. It applies to flat rolled products. It does not apply to semi-finished rolled products in coiled form to be subjected to further rolling (reroll stock) or to special products such as corrugated, embossed, painted, etc., sheets and strips or to special applications such as aerospace, can stock, finstock, etc., which are dealt with in separate EN standards.
Aluminium und Aluminiumlegierungen - Bänder, Bleche und Platten - Teil 2: Mechanische Eigenschaften
Dieser Teil der EN 485 legt die mechanischen Eigenschaften für Bleche, Bänder und Platten aus Aluminium und Aluminium-Knetlegierungen fest, die für allgemeine Verwendung besimmt sind. Er gilt für flachgewalzte Erzeugnisse. Er gilt nicht für Vorwalzbänder, Spezialerzeugnisse wie z.B. rollgeformte, geprägte oder lackierte Bänder und Bleche, oder Erzeugnisse, die für Spezialanwendungen, wie beispielsweise Luft- und Raumfahrt, Getränkedosen, Wärmeaustauscher usw. eingesetzt werden. Diese werden in gesonderten Europäischen Normen abgehandelt.
Aluminium et alliages d'aluminium - Tôles, bandes et tôles épaisses - Partie 2: Caractéristiques mécaniques
La présente partie de l'EN 485 spécifie les caractéristiques mécaniques des tôles, bandes et tôles épaisses en aluminium et alliages d'aluminium corroyés pour applications courantes. Elle s'applique aux produits laminés plats. Elle ne s'applique pas aux demi-produits laminés, livrés en bobines, destinés a etre relaminés (ébauches pour laminage) ni aux produits spéciaux tels que profils de forme, tôles et bandes gravées, laquées, etc., ni aux produits pour applications spéciales telles que la construction aéronautique, le boîtage, les échangeurs thermiques, etc., qui sont traîtés dans des normes EN séparées.
Aluminij in aluminijeve zlitine - Pločevine, trakovi in plošče - 2. del: Mehanske lastnosti
General Information
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Standards Content (Sample)
SLOVENSKI STANDARD
SIST EN 485-2:2004
01-november-2004
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SIST EN 485-2:1998
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Aluminium and aluminium alloys - Sheet, strip and plate - Part 2: Mechanical properties
Aluminium und Aluminiumlegierungen - Bänder, Bleche und Platten - Teil 2:
Mechanische Eigenschaften
Aluminium et alliages d'aluminium - Tôles, bandes et tôles épaisses - Partie 2:
Caractéristiques mécaniques
Ta slovenski standard je istoveten z: EN 485-2:2004
ICS:
77.150.10 Aluminijski izdelki Aluminium products
SIST EN 485-2:2004 en
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.
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EUROPEAN STANDARD
EN 485-2
NORME EUROPÉENNE
EUROPÄISCHE NORM
July 2004
ICS 77.150.10 Supersedes EN 485-2:1994
English version
Aluminium and aluminium alloys - Sheet, strip and plate - Part 2:
Mechanical properties
Aluminium et alliages d'aluminium - Tôles, bandes et tôles Aluminium und Aluminiumlegierungen - Bänder, Bleche
épaisses - Partie 2: Caractéristiques mécaniques und Platten - Teil 2: Mechanische Eigenschaften
This European Standard was approved by CEN on 24 March 2004.
CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this European
Standard the status of a national standard without any alteration. Up-to-date lists and bibliographical references concerning such national
standards may be obtained on application to the Central Secretariat or to any CEN member.
This European Standard exists in three official versions (English, French, German). A version in any other language made by translation
under the responsibility of a CEN member into its own language and notified to the Central Secretariat has the same status as the official
versions.
CEN members are the national standards bodies of Austria, Belgium, Cyprus, Czech Republic, Denmark, Estonia, Finland, France,
Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Slovakia,
Slovenia, Spain, Sweden, Switzerland and United Kingdom.
EUROPEAN COMMITTEE FOR STANDARDIZATION
COMITÉ EUROPÉEN DE NORMALISATION
EUROPÄISCHES KOMITEE FÜR NORMUNG
Management Centre: rue de Stassart, 36 B-1050 Brussels
© 2004 CEN All rights of exploitation in any form and by any means reserved Ref. No. EN 485-2:2004: E
worldwide for CEN national Members.
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EN 485-2:2004 (E)
Contents
Foreword.4
1 Scope.6
2 Normative references.6
3 Tensile test.6
4 Bend test.7
5 Hardness test.7
Table 1 — Minimum material gauge and Brinell hardness values .8
6 Electrical conductivity.8
7 Stress-corrosion resistance.8
8 Exfoliation corrosion resistance (5xxx series alloys).9
9 Exfoliation corrosion resistance (7xxx series alloys).9
Table 2 — Aluminium EN AW-1080A [Al 99,8(A)] .12
Table 3 — Aluminium EN AW-1070A [Al 99,7] .13
Table 4 — Aluminium EN AW-1050A [Al 99,5] .14
Table 5 — Aluminium EN AW-1200 [Al 99,0].15
Table 6 — Alloy EN AW-2014 [Al Cu4SiMg] .16
Table 7 — Alloy EN AW-2014A [Al Cu4SiMg(A)].17
Table 8 — Alloy EN AW-2017A [Al Cu4MgSi(A)].18
Table 9 — Alloy EN AW-2024 [Al Cu4Mg1].19
Table 10 — Alloy EN AW-3003 [Al Mn1Cu].20
Table 11 — Alloy EN AW-3103 [Al Mn1].21
Table 12 — Alloy EN AW-3004 [Al Mn1Mg1] .22
Table 13 — Alloy EN AW-3005 [Al Mn1Mg0,5] .23
Table 14 — Alloy EN AW-3105 [Al Mn0,5Mg0,5] .24
Table 15 — Alloy EN AW-4006 [Al Si1Fe] .25
Table 16 — Alloy EN AW-4007 [Al Si1,5Mn] .25
Table 17 — Alloy EN AW-4015 [Al Si2Mn] .26
Table 18 — Alloy EN AW-5005 [Al Mg1(B)], alloy EN AW-5005A [Al Mg1(C)].27
Table 19 — Alloy EN AW-5040 [Al Mg1,5Mn] .28
Table 20 — Alloy EN AW-5049 [Al Mg2Mn0,8] .29
Table 21 — Alloy EN AW-5449 [Al Mg2Mn0,8(B)] .30
Table 22 — Alloy EN AW-5050 [Al Mg1,5(C)] .31
Table 23 — Alloy EN AW-5251 [Al Mg2].32
Table 24 — Alloy EN AW-5052 [Al Mg2,5] .33
Table 25 — Alloy EN AW-5154A [Al Mg3,5(A)].34
Table 26 — Alloy EN AW-5454 [Al Mg3Mn] .35
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EN 485-2:2004 (E)
Table 27 — Alloy EN AW-5754 [Al Mg3] .36
Table 28 — Alloy EN AW-5182 [Al Mg4,5Mn0,4] .37
Table 29 — Alloy EN AW-5083 [Al Mg4,5Mn0,7] .38
Table 30 — Alloy EN AW-5383 [Al Mg4,5Mn0,9] .39
Table 31 — Alloy EN AW-5086 [Al Mg4] .40
Table 32 — Alloy EN AW-6016 [Al Si1,2Mg0,4].41
Table 33 — Alloy EN AW-6061 [Al Mg1SiCu] .41
Table 34 — Alloy EN AW-6082 [Al Si1MgMn].42
Table 35 — Alloy EN AW-7020 [Al Zn4,5Mg1].43
Table 36 — Alloy EN AW-7021 [Al Zn5,5Mg1,5].44
Table 37 — Alloy EN AW-7022 [Al Zn5Mg3Cu] .44
Table 38 — Alloy EN AW-7075 [Al Zn5,5MgCu] .45
Table 38 (concluded).46
Table 39 — Alloy EN AW-8011A [Al FeSi(A)] .47
Annex A (normative) Rules for rounding.48
Bibliography.49
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EN 485-2:2004 (E)
Foreword
This document (EN 485-2:2004) has been prepared by Technical Committee CEN/TC 132 “Aluminium and
aluminium alloys”, the secretariat of which is held by AFNOR.
This European Standard shall be given the status of a national standard, either by publication of an identical text or
by endorsement, at the latest by January 2005, and conflicting national standards shall be withdrawn at the latest
by January 2005.
Within its programme of work, Technical Committee CEN/TC 132 entrusted CEN/TC 132/WG 7 "Sheet, strip and
plate" to prepare the following standard:
EN 485-2, Aluminium and aluminium alloys — Sheet, strip and plate — Part 2: Mechanical properties.
This standard is part of a set of four standards. The other standards deal with:
Part 1: Technical conditions for inspection and delivery
Part 3: Tolerances on dimensions and form for hot-rolled products
Part 4: Tolerances on shape and dimensions for cold-rolled products
This document supersedes EN 485-2:1994.
Besides very slight editorial adjustments in the text and update of normative references, the following technical
changes have been made:
Clause 1: NOTE added.
Clause 2: ASTM G34-86 changed into ASTM G34-97
ASTM G66-86 changed into ASTM G66-95
Clause 5: Note added
Tables 2 to 39: Due to the introduction of new alloys, the tables have been renumbered when necessary.
New alloys: EN AW-2014A, 4015, 5005A, 5449, 5383, 6016.
Modified values or extended ranges:
EN AW-1070A: O/H111 (over 12,5 mm up to 25,0 mm) added.
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EN 485-2:2004 (E)
EN AW-1050A: O/H111 (over 12,5 mm up to 80,0 mm) extended.
H14 (over 0,5 mm up to 1,5 mm) A modified.
50 mm
H24 (over 0,5 mm up to 1,5 mm) A modified.
50 mm
EN AW-1200: O/H111 (over 12,5 mm up to 80,0 mm) extended.
EN AW-2014: T6, T651 (over 100,0 mm up to 160,0 mm) extended.
EN AW-2017A: T4, T451 modified, T452 added.
EN AW-3103: H16 (over 4,0 mm up to 8,0 mm) added.
EN AW-5049: H112 (6,0 up to 25,0) modified.
EN AW-5052: F modified, H112 (6,0 mm up to 12,5 mm) modified.
EN AW-5454: F modified and extended.
EN AW-5754: F (over 100,0 mm up to 150,0 mm) added, H112 modified.
EN AW-5083: F modified, O/H111 (over 120,0 mm up to 300,0 mm) extended,
H112 (over 80,0 mm up to 120,0 mm) added.
EN AW-5086: H112 (6,0 mm up to 12,5 mm) modified.
EN AW-6061: T6, T651, T62 (over 150,0 mm up to 400,0 mm) extended.
EN AW-6082: T6, T651, T62 (over 175,0 mm up to 350,0 mm) added.
EN AW-7020: T6, T651, T62 (over 175,0 mm up to 250,0 mm) added.
EN AW-7075: T6, T651, T62 (over 150,0 mm up to 300,0 mm) added, T652 added.
According to the CEN/CENELEC Internal Regulations, the national standards organizations of the following
countries are bound to implement this European Standard: Austria, Belgium, Cyprus, Czech Republic, Denmark,
Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta,
Netherlands, Norway, Poland, Portugal, Slovakia, Slovenia, Spain, Sweden, Switzerland and United Kingdom.
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EN 485-2:2004 (E)
1 Scope
This part of EN 485 specifies the mechanical properties of wrought aluminium and aluminium alloy sheet, strip and
plate for general engineering applications.
It applies to flat rolled products.
It does not apply to semi-finished rolled products in coiled form to be subjected to further rolling (reroll stock) or to
special products such as corrugated, embossed, painted, etc. sheets and strips or to special applications such as
aerospace, can stock, finstock, etc. which are dealt with in separate European Standards.
The systems for designating these materials are described in EN 573-1 and EN 573-2. Their chemical composition
limits are specified in EN 573-3.
Mechanical property limits are specified for all Class A alloys, as defined in EN 573-4.
Temper designations are defined in EN 515.
NOTE Some of the products listed in the present standard can be subject to patent or patent applications, and their listing
herein does not in any way imply the granting of a licence under such patent right.
CEN/TC 132 affirms it is its policy that in the case when a patentee refuses to grant licences on standardised
standard products under reasonable and not discriminatory conditions then this product shall be removed from the
corresponding standard.
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.
EN 485-1, Aluminium and aluminium alloys — Sheet, strip and plate — Part 1: Technical conditions for inspection
and delivery.
EN 2004-1, Aerospace series — Test methods for aluminium and aluminium alloy products — Part 1:
Determination of electrical conductivity of wrought aluminium alloys.
EN 10002-1, Metallic materials — Tensile testing — Part 1: Method of test at ambient temperature.
EN ISO 6506-1, Metallic materials — Brinell hardness test — Part 1: Test method (ISO 6506-1:1999).
EN ISO 7438, Metallic materials — Bend test (ISO 7438:1985).
ISO 9591, Corrosion of aluminium alloys — Determination of resistance to stress-corrosion cracking.
ASTM G34-97, Exfoliation Corrosion Susceptibility in 2xxx and 7xxx Series Aluminum Alloys (EXCO test).
ASTM G66-95, Visual Assessment of Exfoliation Corrosion Susceptibility of 5xxx Series Aluminium Alloys
(ASSET test).
3 Tensile test
The selection, preparation and number of specimens and test-pieces is specified in EN 485-1.
The test shall be carried out in accordance with EN 10002-1, particular attention being paid to the following:
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EN 485-2:2004 (E)
normally the test-pieces shall be taken with their length transverse (or long transverse) to the principal direction
of rolling. If the width of the product is less than 300 mm, then test in the longitudinal direction is permitted. In
both cases the mechanical property limits specified in Tables 2 to 39 shall apply;
machined test-pieces of rectangular or circular cross-section (as applicable) shall be used;
for specified thicknesses up to and including 12,5 mm the test-piece shall have a rectangular (or square)
cross-section. Its reduced section shall be 12,5 mm wide and its thickness equal to the full thickness of the
product;
for specified thicknesses from 10,0 mm up to and including 12,5 mm a round test-piece or a rectangular test-
piece may be used;
for specified thicknesses exceeding 12,5 mm the test-piece shall have a circular cross section with a
recommended diameter of 10 mm for its reduced section;
recommended shapes for rectangular and round test-pieces are shown in Figures 1 and 2;
during a test to determine proof stress, the rate of stress application shall not exceed 12 MPa/s. After removal
of the extensometer the rate of straining may be increased but it shall not exceed 50 % of the length of the
reduced section per minute;
elongation for rectangular (or square) test-pieces shall be measured using an original gauge length of 50 mm;
elongation for round test-pieces shall be measured using an original gauge length equal to 5 D where D is the
diameter of the reduced section;
for determination of compliance, proof stress and tensile strength values shall be rounded to the nearest
1 MPa and elongation values to the nearest 1 % using the rounding rules set out in annex A.
4 Bend test
Sheet, strip and plate shall be capable of being bent cold through an angle of 90° or 180°, as applicable, around a
pin having a radius equal to k times the thickness t of the sheet, strip or plate (e.g. 2,5 t) without cracking.
Recommended values of the minimum bend radii for different alloys, tempers and thicknesses are given in
Tables 2 to 39. Compliance with these values and/or conduct of the test is only required when so specified on the
order.
The test shall be carried out in accordance with EN ISO 7438, particular attention being paid to the following:
bend test shall be carried out on a specimen taken adjacent to the tensile test specimen;
test-piece shall be taken in the transverse direction, the bend axis being parallel to the rolling direction. For
material less than 150 mm wide, the test-piece may be taken in the rolling direction;
width of the test piece shall be at least 20 mm and preferably 40 mm to 50 mm. For material less than 20 mm
wide, the width of the test-piece shall be the full width of the material;
edges of the test-piece may be machined when practical. They may be rounded to a radius of approximately 2
mm.
5 Hardness test
Hardness test can be a convenient means for checking the homogeneity of a lot ; it can also be used for a quick
semi-quantitative check of the thermal treatment to which the material has been submitted or, as a first approach,
for material identification purpose. However its accuracy is generally less than can be expected from a tensile test
which it cannot replace.
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EN 485-2:2004 (E)
NOTE Hardness can be measured at different locations, e.g. on the surface of the product or on the tensile specimen. For
some materials, results can be different.
The values in Tables 2 to 39 are typical Brinell hardness (HBW) values for a test carried out according to
EN ISO 6506-1 with a 2,5 mm diameter steel ball. They are given for information only.
If the Brinell hardness test is not possible (because of thin gauge or soft temper) then Vickers hardness test,
according to EN ISO 6507-1, can be used. In that case the values will be approximately 10 % above the stated
Brinell values.
Table 1, given for convenience, shows for several HBW values the minimum gauge down to which the hardness
measurement remains valid, according to the rules stated in EN ISO 6506-1, using a 2,5 mm diameter steel ball
and a load of 612,9 N.
Table 1 — Minimum material gauge and Brinell hardness values
Brinell hardness (HBW)
30 40 50 60 70 80 90 100
minimum gauge (mm) 2,1 1,6 1,3 1,1 0,91 0,80 0,71 0,64
Brinell hardness (HBW) 110 120 130 140 150 160 170 180
minimum gauge (mm)
0,58 0,53 0,49 0,45 0,42 0,40 0,37 0,35
6 Electrical conductivity
Electrical conductivity measurements are required for lot acceptance-purposes, in the case of alloy EN AW-7075 in
the tempers T73, T7351, T76 and T7651, in order to assess the resistance to stress-corrosion cracking or the
exfoliation-corrosion resistance of the material as applicable.
The specimen for electrical conductivity testing shall be taken adjacent to the tensile test specimen.
The measurement shall be carried out by the eddy-current method as specified in EN 2004-1. The reference blocks
to be used shall be agreed between producer and purchaser. The results shall be rounded to the nearest
0,1 MS/m, using the rounding rules set out in annex A.
The acceptance criteria are specified in Table 38.
7 Stress-corrosion resistance
7.1 Plate made of alloy EN AW-7075 in the T73 and T7351 tempers and over 25 mm in thickness, shall be
capable of exhibiting no evidence of stress-corrosion cracking when subjected to ISO 9591 accelerated
stress-corrosion cracking test.
For the purpose of this standard the following provisions shall apply:
a minimum of three adjacent replicate test pieces shall be taken from each specimen and submitted to the test;
exposure shall be carried out by alternate immersion in a 3,5 % by mass sodium chloride solution in water;
test-pieces shall be stressed in the short transverse direction with a stress level of 75 % of the specified proof
stress;
no stress-corrosion related rupture shall be observed after a minimum exposure time of 20 days.
The method of stressing (bending, uniaxial loading, C-ring, etc.), the shape and dimensions of the test-pieces and
the frequency of the test are left to the discretion of the producer, who shall maintain records of all lots so tested
and make them available for examination at the producer's facility for not less than five years.
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EN 485-2:2004 (E)
7.2 For lot acceptance-purposes resistance to stress-corrosion cracking for each lot of material shall be
established by testing the previously selected tensile test specimens to the criteria shown in Table 38.
8 Exfoliation corrosion resistance (5xxx series alloys)
8.1 Products made of alloys EN AW-5086, EN AW-5083 and EN AW-5383 in the H116 temper shall be capable
of exhibiting no evidence of exfoliation corrosion when subjected to ASTM G66-95 accelerated exfoliation corrosion
susceptibility test.
The test shall be carried out on full thickness test-pieces for material less than 2,5 mm in thickness. For material
2,5 mm or more in thickness, 10 % of the thickness shall be removed by machining, from one as-rolled surface,
and both the machined and as-rolled surfaces submitted to the test and evaluated.
8.2 For lot-acceptance purposes, the acceptability of each lot of material mentioned in 8.1 shall be determined
by the producer, by metallographic examination of one specimen per lot selected from midsection at one end of a
random sheet, plate or coil, using the following procedure:
a section perpendicular to the rolling surface and parallel to the rolling direction shall be polished (preferably
electrolytic polish) and then microetched for 3 min, using a solution of 40 ml 85 % phosphoric acid in 60 ml
distilled water, at (35 ± 5) °C;
metallographic examination shall be carried out at 500 times magnification;
revealed microstructure shall be predominantly free of a continuous grain boundary network of aluminium-
magnesium precipitate (Al Mg ).
3 2
Acceptability shall be determined by comparison to producer-established reference photomicrographs of
acceptable material. If the microstructure shows evidence of Al Mg precipitates in excess of the relevant
3 2
reference, the lot is either rejected or subjected to the ASTM G66-95 test.
Reference photomicrographs shall be established on acceptable material (according to ASTM G66-95), for each
thickness range specified in Table 29 (EN AW-5083) or Table 30 (EN AW-5383) or Table 31 (EN AW-5086) as
applicable. Production practices shall not be changed after establishment of these references.
Significant changes in production practices that alter the microstructures of the alloy shall require the establishment
of new reference photomicrographs as described above.
The producer shall maintain at the producing facility all records relating to the establishment of reference
photomicrographs and production practices.
9 Exfoliation corrosion resistance (7xxx series alloys)
9.1 Products made of alloy EN AW-7075 in the tempers T76 and T7651 shall be capable of exhibiting no
evidence of exfoliation corrosion in excess of grade EB, as defined in ASTM G34-97, when subjected to the test in
9.3.
9.2 For lot acceptance-purposes, resistance to exfoliation corrosion for each lot of material shall be established
by testing the previously selected tensile test specimens to the criteria shown in Table 38.
9.3 When carried out, for monitoring purposes, the test shall be in accordance with ASTM G34-97 (EXCO test),
and the following additional requirements shall apply:
specimens for test shall be selected at random from material considered acceptable in accordance with the lot
acceptance criteria shown in Table 38, for each thickness range listed in that table;
test-pieces shall be a minimum of (50 x 100) mm with the 50 mm dimension parallel to the direction of final
rolling. They shall include the full-section thickness of the material, except that for material 2,5 mm or more in
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EN 485-2:2004 (E)
thickness, 10 % of the thickness shall be removed by machining the test surface. For machined test-pieces,
the machined surface shall be evaluated by exposure to the test solution ;
the frequency of the test is left to the discretion of the producer, who shall maintain records of all lots so tested
and make them available for examination at the producer's facility for not less than five years.
Dimensions in millimetres
Standard test-piece
Nominal width 12,5
G - Gauge length 50,0 ± 0,5
W – Width 12,5 ± 0,10
t – Thickness thickness of material
R - Radius of fillet, min. 12,5
L - Overall length, min. 200
A - Length of reduced section, min. 57
B - Length of grip section, min. 50
C - Width of grip section, approximate 20
Figure 1 — Standard rectangular tensile test-piece
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EN 485-2:2004 (E)
Dimensions in millimetres
Standard test-piece Small-size test-pieces proportional to standard
Nominal diameter 10 8 6 4
G - Gauge length 50,0 ± 0,5 40,0 ± 0,5 30,0 ± 0,5 20,0 ± 0,5
D - Diameter 10,0 ± 0,10 8,0 ± 0,10 6,0 ± 0,10 4,0 ± 0,05
R - Radius of fillet, min. 9 8 6 4
A - Length of reduced section, min. 60 48 36 24
Figure 2— Standard 10 mm tensile test-piece with 50 mm gauge length and examples of small-
size proportional test-pieces
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EN 485-2:2004 (E)
Table 2 — Aluminium EN AW-1080A [Al 99,8(A)]
a
Temper Specified R R Elongation Hardness
Bend radius
m p0,2
thickness
min.
a
mm MPa MPa %
HBW
over up to min. max. min. max. A A 180° 90°
50 mm
a
25,0 60
F ≥ 2,5
O/H111 0,2 0,5 60 90 15 26 0 t 0 t 18
0,5 1,5 60 90 15 28 0 t 0 t 18
1,5 3,0 60 90 15 31 0 t 0 t 18
3,0 6,0 60 90 15 35 0,5 t 0,5 t 18
6,0 12,5 60 90 15 35 0,5 t 0,5 t 18
H112 12,5 70 20
≥ 6,0
12,5 25,0 70 20
H12 0,2 0,5 80 120 55 5 0,5 t 0 t 26
0,5 1,5 80 120 55 6 0,5 t 0 t 26
0,5 t 0,5 t
1,5 3,0 80 120 55 7 26
3,0 6,0 80 120 55 9 1,0 t 26
6,0 12,5 80 120 55 12 2,0 t 26
H14 0,2 0,5 100 140 70 4 0,5 t 0 t 32
0,5 t 0,5 t
0,5 1,5 100 140 70 4 32
1,5 3,0 100 140 70 5 1,0 t 1,0 t 32
1,5 t
3,0 6,0 100 140 70 6 32
6,0 12,5 100 140 70 7 2,5 t 32
H16 0,2 0,5 110 150 90 2 1,0 t 0,5 t 36
1,0 t 1,0 t
0,5 1,5 110 150 90 2 36
1,5 4,0 110 150 90 3 1,0 t 1,0 t 36
H18 0,2 0,5 125 105 2 1,0 t 40
0,5 1,5 125 105 2 2,0 t 40
2,5 t
1,5 3,0 125 105 2 40
H22 0,2 0,5 80 120 50 8 0,5 t 0 t 26
0,5 1,5 80 120 50 9 0,5 t 0 t 26
1,5 3,0 80 120 50 11 0,5 t 0,5 t 26
3,0 6,0 80 120 50 13 1,0 t 26
2,0 t
6,0 12,5 80 120 50 15 26
H24 0,2 0,5 100 140 60 5 0,5 t 0 t 31
0,5 1,5 100 140 60 6 0,5 t 0,5 t 31
1,5 3,0 100 140 60 7 1,0 t 1,0 t 31
1,5 t
3,0 6,0 100 140 60 9 31
6,0 12,5 100 140 60 11 2,5 t 31
H26 0,2 0,5 110 150 80 3 0,5 t 35
0,5 1,5 110 150 80 3 1,0 t 35
1,5 4,0 110 150 80 4 1,0 t 35
a
For information only.
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EN 485-2:2004 (E)
Table 3 — Aluminium EN AW-1070A [Al 99,7]
a
Temper Specified R R Elongation Hardness
Bend radius
m p0,2
thickness
min.
a
mm MPa MPa %
HBW
...
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