Specification For Wrought Aluminium and Aluminium Alloy Plate For General Engineering Purposes
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Indi In dian an Stan Standa darrd
SPECIFICATION SPECIFICA TION FOR WR WROUGHT OUGHT ALUMINIUM AND ALUMINIUM ALLOY PLATE FOR GENERAL ENGINEERING PURPOSES (Fourth Revision)
IS 736 : 2018
Indi In dian an Stan Standa darrd
SPECIFICATION SPECIFICA TION FOR WROU WROUGHT GHT ALUMINIUM AND ALUMINIUM ALLOY PLATE FOR GENERAL ENGINEERING PURPOSES (Fourth Revision)
1 SCOPE
For the purpose of this standard, the definitions as given in IS 5047 (Part 1) and IS 5047 (Part 2)
This Th is stan standa dard rd cove covers rs the the re requ quir irem emen ents ts fo for r
and the following shall apply.
wrought aluminium and aluminium alloy plates
3.1
for general engineering engineering purposes. It also covers orde or deri ring ng in info form rmat atio ion, n, ma mate teri rial al,, sa samp mpli ling ng,,
Plate
Hot or cold rolled product of rectangular section, 6.0 mm thick and thicker. It may be either in
packaging & marking requirements and BIS
straight length or in coil form. It has less control
certification.
of surface finish and tolerance then applied to sheet.
2 REFERENCES
3.2
Thee fo Th foll llow owin ing g stan standa dard rdss co cont ntai ain n pr prov ovis isio ions ns
Heat Treatment Batch
which through reference in this text, constitute
A quantity of material of one alloy of the same
provision of this standard. At the time of
dime dimens nsio ions ns an and d pr prod oduc uced ed in th thee same same way, way,
publication, the editions indicted were valid. All
solution-t solu tion-treated reated and subsequentl subsequently y precipitation precipitation
standards are subject to revision and parties to
treated in one furnace load. More than one heattreatment batch may comprise a furnace load.
agreements based on this standard are en enco cour urag aged ed to in inve vest stig igat atee th thee po possi ssibi bili lity ty of
3.3
app applyin lying g
aluminium and aluminium alloy plate for general
th thee most rece recen nt edit editio ion ns
of th thee
engineering purposes.
standards indicated below. IS No.
Title
10259: 2017
General
3.4
condition
engineering purposes. 3.5
alumin alu minium ium and alumin aluminium ium products
Supp Su ppli lier er – Th Thee su supp ppli lier er of wr wrou ough ghtt
aluminium and aluminium alloy plate for general
of
delive del ivery ry and inspec inspectio tion n of alloy
Purcha Pur chaser ser – The pur purcha chaser ser of wro wrough ughtt
Leve Le vel-A l-A pa pack ckag agin ing g – Th Thee pa pack ckag agin ing g
applicable for transfer of goods from one country
(First
to another country (i.e. import-export).
Revision)
3.6
Commercial Packaging – The packaging
applic appl icab able le fo forr tr tran ansf sfer er of go good odss wi with thin in th thee country.
3 DEFINITION AND TERMINOLOGY
1
IS 736 : 2018
4 ORDERING INFORMATION
8.3
given in IS 1816 with a gauge length of 5O mm.
following information:
Thee te Th test st pi piec ecee shal shalll be cu cutt tran transv sver erse se to th thee
HS Code for custom tariff / HSN Code
direction of rolling for plates 300mm wide and
under GST (for domestic trade);
over, and parallel to the direction of rolling for
4.2
Applicable Indian Standard;
4.3
Gross weight of the consignment;
4.4
Thee requir Th required ed chemic chemical al compos compositi ition on (7)
plates under 300 mm wide. When the width of the material to be tested is insufficient to permit preparation of the standard tensile test piece, a
and dimensions and tolerances (10) 4.5
piece of the full width of material may be used.
Port of delivery (for imported product),
9 CONDITION
and 4.6
The
necessa ssary
cer erttificati ations
and
The material shall be supplied in the condition as
documentations as required by Indian laws.
required by the purchaser. While specifying the condition, the temper designations laid down in
5 SUPPLY OF OF MATERIAL 5.1
IS 5052 shall be followed.
General Gen eral requir requireme ements nts for the supply supply of
10 DIMENS DIMENSION IONS S AND
aluminium and aluminium alloy products shall conform to IS 10259.
TOLERANCES
Thee dimens Th dimension ionss of plate plate and their their toleran tolerances ces
6 FREE FROM DEFECTS
shall be as specified in IS 2677.
Thee mate Th materi rial al shal shalll be soun sound d and and fr free ee fr from om
11 SELECT SELECTION ION OF TES TEST T SAMPLES
harmful defects.
7 CHEMI EMICAL CAL C CO OMPOSITIO ITION N 7.1
The
chemi emical
test piece shall be of
rectangular section and having the dimensions as
Thee orde Th orderin ring g in info form rmati ation on sh shal alll in incl clud udee th thee 4.1
The tensile
composi sittion
of
11.1
Plate
of
Aluminium
or
Non-Hea -Heatt-
Treatable Aluminium Alloys
the
alumin alu minium ium and alumin aluminium ium all alloys oys used used for the
Material of the same thickness, produced in the
plates shall be as per Table 2. 2.
same way, and of the same nominal composition
7.2
The chemical composition of the material
shall be grouped. into batches of not more than 4
shall
be
000 kg.
determ rmiined
by
any
est staablish shed ed
instrumental method.
11.1.1 The supplier shall sample each batch at
su such ch ra rate te th that at he may, may, on th thee re resu sult ltss of th thee
8 MECHANICAL PROPERTIES 8.1
mechanical tests on the samples, certify that the material conforms to this standard.
Thee mechan Th mechanical ical proper propertie tiess of the plate plate
11.1.2 Before the test samples are cut-off, they
sh shal alll co comp mply ly with with th thee requi require reme ment ntss give given n in
shall be marked to identify them with the batch
Table 3. 3. 8.2
they represent. The test samples shall be taken
The tensile test shall be carried out and
from the material as supplied and shall not be
proof stress determined thereby in accordance
further annealed or mechanically worked (except
with IS 1816. for preparing the test piece) before being tested. The test samples may be out from the margins of the material before cutting it to size.
2
IS 736 : 2018 11.2
Pl Plat atee
of
Heat Heat-T -Tre reat atab able le
Al Alum umin iniu ium m
12.2
Forr he Fo heat at-tr -treat eatab able le al allo loys ys th thee supp suppli lier er
Alloys
shall have the right if he so desires, to reheat-
One test sample shall be cut from a plate, from
treat the material material before the two further further samples
ea each ch heat heat-t -tre reat atme ment nt batc batch. h. Befo Before re the the te test st
are selected.
sampl sam ples es are cu cutt off, off, th they ey shal shalll be mark marked ed to
12.3
identify ident ify them with the heat-treatmen heat-treatmentt batch they
additional samples pass, the batch represented by
represent.
the test samples shall be deemed to comply with
11.2.1 For material supplied in M condition, the
test samples shall be tested in the O, W or WP
this standard. Should the test pieces from either of th thes esee ad addi diti tion onal al sa samp mple less fa fail il,, th thee ba batc tch h
condition, after heat-treatment as appropriate or
represented by the test samples shall be deemed
as specified by the purchaser. The test samples,
not to comply with this standard.
after heat-treatment, heat-treatment, shall not be mechanically mechanically
12.4
worked (except for straightening and preparing
with each consignment giving details of grade,
the test piece) before being tested.
co cond ndit itio ion, n, ba batc tch h nu numb mber er an and d co corr rresp espon ondi ding ng
Should Sho uld the test test pieces pieces from from both both these these
The Suppli Supplier er shall shall furnis furnish h a certifi certificate cate
chemi emical
11.2.2 Material in the O condition, when heat-
composit sition
and
mechan aniical
properties.
treated, may be expected to have properties of the the orde orderr of 15 MPa MPa less less than than the the spec specif ifie ied d
REST STRI RICT CTIO ION N ON HE HEAV AVY Y 13 RE
properties for the W or WP conditions as
METALS
appropriate.
13.1
11.2.3 For material supplied in the W condition
Thee co Th cont nten entt of he heav avy y meta metals ls in th thee
wrought aluminium and aluminium alloy plate
the test samples shall be tested in the condition
forr ge fo gene neral ral en engi gine neeri ering ng pu purp rpos oses es sh shal alll no nott
as supplied, unless the purchaser has specified
exceed the limit as given in Table 1. 1.
that he requires the test samples to be tested in
Table 1: Maximum Limit of Heavy Materials (in PPM)
the WP condition. The test samples shall not be Heavy Metal
mechanically worked (except for preparing the test piece) before being tested. The test samples
Lead Mercury Cadmium Hexavalent Chromium
may be cut from the margins of the material before cutting it to size. 11.2.4 For material supplied in the WP condition, the test samples shall be tested in the
13.2
Maximum limit (in PPM) 1 000 1 000 100 1 000
The testing for the heavy metals shall be
conducted as mentioned in IS 10259.
condition as supplied. The test samples shall not
14 PACKAGING
be further heat treated or mechanically worked (except for preparing the test piece) before being
For the purpose of this standard, the following
tested. The test samples may be cut from the
packaging methods and those given in IS 10259
margins of the material before cutting it to size.
shall apply.
12 RETES ETESTS TS 12.1
15 MARK MARKIN ING G AND AND LABELLING
Should any one of the test pieces first
selec sel ecte ted d fail fail to pa pass ss the the mech mechan anic ical al test test,, tw two o For the purpose of this standard, the following marking marki ng and labelling methods methods and those given
fu furt rthe herr samp sample less from from the the sa same me lot lot shal shalll be selected for testing.
in IS 10259 shall apply. apply .
3
IS 736 : 2018 15.1
Each package or, coil of plate(s) shall be
suitable marked with the following details. a) Name Name of the the man manuf ufact actur urer, er, b) Grade and condition of the material; and c) Batch atch nu numb mber er 15.2
Thee mate Th materia riall may may also also be mark marked ed wi with th
the Standard Mark.
16 BIS CERTIF CERTIFICA ICATIO TION N MARKING The use of the Standard Mark is governed by the provision of the Bureau of Indian Standards Act, 1986 and the Rules and Regulations made there under. The details of conditions under which the licencee for the use of the Standard Mark may be licenc granted to manufacturers or producers may be obtained from the Bureau of Indian Standards.
4
IS 736 : 2018
Table 2 Chemical composition of wrought aluminium and aluminium alloy plates (Composition limits are in percent maximum, unless shown otherwise) (Clause 7.1) 7.1)
Microsoft Excel 97-2003 Worksheet
NOTE- It is the responsibility of the supplier to ensure ensure that any element not specially limited is not presen presentt in an amount such as IS generally accepted as having an adverse effect on the product. If a purchaser's requirements necessitate limits for any element not specified. it should be agreed between the purchaser and the supplier. *- Titanium and/or other grain refining elements and/or chromium may be present at the option of the supplier provided the total content does does not exceed 0.3 percent Table 3 Mechanical properties of wrought aluminium and aluminium alloy plates (Clause 8.1) 8.1) Designatio n
(1) 19800
19700
19600
19500
19000
24345
24345 Al clad
31000
40800
Conditio n
0.2 percent Proof Stress MPA
Tensile Strength MPA
Elongation on 50mm Gauge Length, Percent, Min
Min
Min
Max
(2) M O H2 M O H2 M O H2 M
(3) 0 0 0 0 0 0 0 0 0 0
(4) 55 0 85 60 0 90 60 0 95 65
(5) 90 110 95 115 0 100 125 0
Over 6.0 mm, up to and including 12.5 mm (6) 30 34 8 30 34 8 28 30 7 28
O2 H M O H2 M O W WP M O W WP M O
0 0 0 0 0 0 0 225 310 0 0 230 345 0 0
00 10 70 70 110 150 0 390 405 150 0 375 420 95 90
13 05 0 1 0 110 140 0 240 0 0 0 240 0 0 0 130
370 28 28 7 10 12 12 7 10 12 12 7 23 22
300 28 28 0 10 10 10 5 10 10 10 5 23 23
H2 M O H2
0 0 0 0
130 90 85 120
180 0 120 160
5 28 30 7
0 28 30 0
5
Over 12.5 mm, up to and including 25 mm (7) 30 34 0 30 34 0 28 30 0 28
IS 736 : 2018 51000-A
51000-B
52000
53000
54300
55000
64430
65032
74530
65028
M O H2 M O H2 M O W WP H2 M O H2 M O H2 M O H2 M O W WP M O W WP W (naturally aged for 30 days) WP M O T4 T6
0 0 0 0 0 0 0 60 115 250 60 0 85 190 125 115 275 125 100 275 0 0 115 240 0 0 110 235
105 95 140 135 125 170 190 175 200 295 200 215 205 280 280 270 355 275 265 355 110 0 200 280 110 0 200 280
0 145 190 0 170 0 0 215 255 265 325 0 340 0 0 355 0 0 150 0 0 0 150 0 0
20 22 4 17 19 4 12 18 15 5 5 12 16 5 12 16 5 0 16 5 12 15 15 8 12 15 15 8
20 22 0 17 19 0 12 18 15 5 0 12 16 0 12 16 0 0 16 0 12 15 15 8 12 15 15 8
160
265
0
8
8
255 110 235
305 110 200 280
0
7 12 15 15 8
7 12 15 15 8
150
NOTES 1 MPa = 1 N/mm 2 = 0.102 kgf/mm 2 Properties in M temper are for information only.
6
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