Section
6 Carbon–manganese and nickel alloy steels for low temperature service
6.1 Scope
6.1.1 This Section
gives specific requirements for carbon-manganese and nickel alloy
steels intended for use in the construction of cargo tanks, storage
tanks and process pressure vessels for liquefied gases.
6.1.2 The requirements of this Section are also applicable for other types of
pressure vessels where the use of steels with guaranteed impact properties at minimum
design temperature lower than 0°C is required.
6.1.3 Provision is made for plates and sections up to 50 mm thick.
6.1.4 Alternative steels which comply with National Standard specifications may
be accepted under special consideration provided that these specifications give
equivalence to the requirements of this Chapter or alternatively are approved for a
specific application. For plates of thickness greater than 40 mm and up to 50 mm that
are accepted in accordance with a National Standard specification, in addition to each
set of impact tests required by the standard, a set of impact tests is required at
mid-thickness position; the orientation and acceptance criteria are to be the same as
those required by Ch 3, 6.4 Mechanical tests.
6.1.6 For high manganese austenitic steels with thickness up to 40 mm, the specific
requirements for approval, manufacturing and inspection are specified in LR’s
Guidance Notes for Approval, Manufacture, Testing and Certification of High
Manganese Austenitic Steel for Low Temperature Service.
6.2 Manufacture and chemical composition
6.2.1 All steels
are to be in the killed and fine grain treated condition.
6.2.2 The chemical compositions of carbon-manganese steels are to comply with the
appropriate requirements for grades AH, DH, EH and FH strength levels 27S, 32, 36 and
40,see
Table 3.3.2 Chemical composition for higher strength steels. For the uses defined in Ch 3, 6.1 Scope 6.1.1 and Ch 3, 6.1 Scope 6.1.2, however, these grades are to be designated LT−AH,
LT−DH, LT−EH and LT−FH respectively.
6.2.3 The chemical compositions of nickel alloy steels are to comply with the
appropriate requirements of Table 3.6.1 Chemical compositions of nickel
alloy steels.
Table 3.6.1 Chemical compositions of nickel
alloy steels
Grade
of steel
|
C
|
Si
|
Mn
|
Ni
|
P
|
S
|
Residual elements
|
Aluminium (see Note 1)
|
11/2 Ni
|
0,18
max.
|
0,10 – 0,35
|
0,30 –
1,50
|
1,30 –
1,70
|
0,025 max.
|
0,020 max.
|
|
|
21/4 Ni
|
0,18
max
|
0.30 -
0.80
|
2.10 -
2.50
|
|
Total 0,020% min.
|
31/2 Ni
|
0,15
max.
|
0,30 – 0,90
|
3,20 –
3,80
|
Cr 0,25 max.
Cu 0,35 max.
|
|
5Ni
|
0,12
max.
|
4,70 –
5,30
|
Mo 0,08
max.
|
Acid soluble 0,015%
min.
|
9Ni
|
0,10
max.
|
8,50 –
10,0
|
Total
0,60 max.
|
Note
1. The specified minimum aluminium
content may not be applicable when an alternative grain refining
method is approved.
|
6.2.4 For plate
supplied from coil, the chemical analysis may be transposed from the
certificate of the coil manufacture onto the re-processor’s
certificate.
6.3 Heat treatment
6.3.1 All materials
are to be supplied in a condition complying with the requirements
given in Table 3.6.2 Supply conditions.
Table 3.6.2 Supply conditions
Grade
|
Plates
|
Sections and bars
|
LT –
AH
|
N TM
|
Any
|
LT –
DH
|
LT –
EH
|
Normalised (see
Note) T.M.C.P. Quenched and tempered
|
LT –
FH
|
N
TM
|
11/2 Ni
|
Normalised (see Note)
|
2 1/4
Ni
|
Normalised or
Normalised and tempered
|
31/2 Ni
|
Normalised and tempered
|
5Ni
|
Quenched and tempered
|
9Ni
|
Double normalised and tempered or Quenched and
tempered
|
Note Where the term ‘Normalised’ is used it does not include
normalising rolling.
|
6.4 Mechanical tests
6.4.1 For plates, one tensile test specimen is to be taken from one end of each
piece. A piece is to be regarded as the rolled product from a single slab or from a
single ingot if this is rolled directly into plates.
6.4.2 For strips,
tensile test specimens are to be taken from both ends of each coil.
6.4.3 Sections
and bars are to be presented for acceptance test in batches containing
not more than 50 lengths, as supplied. The material in each batch
is to be of the same section size, from the same cast and in the same
condition of supply. One tensile test specimen is to be taken from
material representative of each batch, except that additional tests
are to be taken when the mass of a batch exceeds 10 tonnes.
6.4.4 One set of
three Charpy V-notch impact test specimens is to be taken for each
tensile test specimen required.
6.4.5 For plates,
these impact test specimens are to be cut with the principal axis
perpendicular to the final direction of rolling. For sections, the
impact test specimens are to be taken longitudinally.
6.4.6 The results of all tensile tests are to comply with the appropriate
requirements given in Table 3.6.3 Mechanical properties for
acceptance purposes (see Note 1) . For carbon–manganese steel grades, the
ratio between the yield stress and the tensile strength is not to exceed 0,9 for
normalised and TM steels and 0,94 for QT steels.
Table 3.6.3 Mechanical properties for
acceptance purposes (see Note 1)
Grade of steel
|
Yield stress N/mm2 min.
|
Tensile strength N/mm2
|
Elongation on 5,65
% min. (see Note 3)
|
Charpy V-notch impact tests
(see Note 2)
|
Test
temp. °C
|
Impact energy
|
LT – AH
|
27S
|
265
|
400 –
530
|
22
|
0
|
|
32
|
315
|
440 –
590
|
22
|
|
36
|
355
|
490 –
620
|
21
|
|
40
|
390
|
510 –
650
|
20
|
|
LT – DH
|
27S
|
265
|
400 –
530
|
22
|
–20
|
Plates – transverse tests
|
32
|
315
|
440 –
590
|
22
|
36
|
355
|
490 –
620
|
21
|
40
|
390
|
510 –
650
|
20
|
LT – EH
|
27S
|
265
|
400 –
530
|
22
|
–40
|
Average energy
27 J min
|
32
|
315
|
440 –
590
|
22
|
36
|
355
|
490 –
620
|
21
|
40
|
390
|
510 –
650
|
20
|
LT – FH
|
27S
|
265
|
400 –
530
|
22
|
–60
|
Sections and bars – longitudinal tests
|
32
|
315
|
440 –
590
|
22
|
|
36
|
355
|
490 –
620
|
21
|
|
40
|
390
|
510 –
650
|
20
|
Average energy 41 J
min
|
11/2 Ni
|
|
275
|
490 –
640
|
22
|
–65
|
|
2
1/4 Ni
|
|
275
|
490 - 640
|
21
|
-70
|
|
31/2 Ni
|
|
285
|
450 –
610
|
21
|
–95
|
|
5Ni
|
|
390
|
540 –
740
|
21
|
–110
|
|
9Ni
|
|
585
|
680 –
820
|
18
|
–196
|
|
Note
1. These requirements are applicable to
products not exceeding 50 mm in thickness. The requirements for
thicker products for approved applications are subject to agreement.
|
Thickness t, mm
|
t ≤
5
|
5 < t ≤
10
|
10 < t ≤
15
|
15 < t ≤
20
|
20 < t ≤
25
|
25 < t ≤
30
|
30 < t ≤
40
|
40 < t ≤
50
|
t >
50
|
Elongation
|
Strength levels
27S, 32
|
14
|
16
|
17
|
18
|
19
|
20
|
21
|
22
|
To be
specifically agreed
|
Strength levels
36
|
13
|
15
|
16
|
17
|
18
|
19
|
20
|
21
|
Strength levels
40
|
12
|
14
|
15
|
16
|
17
|
18
|
19
|
20
|
6.4.9 Where plate
is supplied from coil, both the tensile tests and the Charpy V-notch
tests are to be taken from the de-coiled plate in accordance with
the frequency specified for the Grade as required by this Section.
6.5 Identification of materials
6.6 Certification of materials
|