7 Material and General Pipe Design
7.1 Goal
7.1.1 The goal of this chapter is to ensure the safe handling of fuel, under all
operating conditions, to minimize the risk to the ship, personnel and to the
environment, having regard to the nature of the products involved.
7.2 Functional requirements
7.2.1 This chapter relates to functional requirements in 3.2.1, 3.2.5, 3.2.6, 3.2.8,
3.2.9 and 3.2.10. In particular the following apply:
7.2.1.1 Fuel piping shall be capable of absorbing thermal expansion or contraction
caused by extreme temperatures of the fuel without developing substantial stresses.
7.2.1.2 Provision shall be made to protect the piping, piping system and components
and fuel tanks from excessive stresses due to thermal movement and from movements of
the fuel tank and hull structure.
7.2.1.3 If the fuel gas contains heavier constituents that may condense in the
system, means for safely removing the liquid shall be fitted.
7.2.1.4 Low temperature piping shall be thermally isolated from the adjacent hull
structure, where necessary, to prevent the temperature of the hull from falling
below the design temperature of the hull material.
7.3 Regulations for general pipe
design
7.3.1 General
7.3.1.1 Fuel pipes and all the other piping needed for a safe and
reliable operation and maintenance shall be colour marked in accordance with a
standard at least equivalent to those acceptable to the Organization.footnote
7.3.1.2 Where tanks or piping are separated from the ship's structure by
thermal isolation, provision shall be made for electrically bonding to the ship's
structure both the piping and the tanks. All gasketed pipe joints and hose
connections shall be electrically bonded.
7.3.1.3 All pipelines or components which may be isolated in a liquid
full condition shall be provided with relief valves.
LR 7.3-01 All pipelines or components which may be isolated
automatically due to a fire with a liquid volume of more than 0,05 m3
entrapped shall be provided with pressure relief valves sized for a fire
condition.
7.3.1.4 Pipework, which may contain low temperature fuel, shall be
thermally insulated to an extent which will minimize condensation of moisture.
7.3.1.5 Piping other than fuel supply piping and cabling may be arranged
in the double wall piping or duct provided that they do not create a source of
ignition or compromise the integrity of the double pipe or duct. The double wall
piping or duct shall only contain piping or cabling necessary for operational
purposes.
7.3.2 Wall thickness
7.3.2.1 The minimum wall thickness shall be calculated as follows:
- t = (t0 + b + c) / (1 – a/100)
(mm)
where:
- t0 = theoretical thickness
- t0 = PD / (2.0Ke + P) (mm)
- with:
- P = design pressure (MPa) referred to in 7.3.3;
- D = outside diameter (mm);
- K = allowable stress (N/mm²) referred to in 7.3.4;
and
- e = efficiency factor equal to 1.0 for seamless pipes
and for longitudinally or spirally welded pipes, delivered by approved
manufacturers of welded pipes, that are considered equivalent to
seamless pipes when non-destructive testing on welds is carried out in
accordance with recognized standards. In other cases an efficiency
factor of less than 1.0, in accordance with recognized standards, may be
required depending on the manufacturing process;
- b = allowance for bending (mm). The value of b shall be
chosen so that the calculated stress in the bend, due to internal pressure only,
does not exceed the allowable stress. Where such justification is not given, b
shall be:
- b = D·t0 / 2.5r (mm)
- with:
- r = mean radius of the bend (mm);
- c = corrosion allowance (mm). If corrosion or erosion is
expected the wall thickness of the piping shall be increased over that required
by other design regulations. This allowance shall be consistent with the
expected life of the piping; and
- a = negative manufacturing tolerance for thickness (%).
7.3.2.2 The absolute minimum wall thickness shall be in accordance with
a standard acceptable to the Administration.
LR 7.3-02 The nominal thickness of steel pipes is to be not less
than shown in Table LR 5.1 of the Rules for
Ships for Liquefied Gases. The nominal thickness of austenitic stainless steel pipes
is to be not less than shown in Pt 5, Ch 12, Table 12.10.1 of the
Rules for Ships.
7.3.3 Design condition
7.3.3.1 The greater of the following design conditions shall be used for
piping, piping system and components as appropriate:footnote,footnote
- .1 for systems or components which may be separated from their
relief valves and which contain only vapour at all times, vapour pressure at
45°C assuming an initial condition of saturated vapour in the system at the
system operating pressure and temperature; or
- .2 the MARVS of the fuel tanks and fuel processing systems; or
- .3 the pressure setting of the associated pump or compressor
discharge relief valve; or
- .4 the maximum total discharge or loading head of the fuel piping
system; or
- .5 the relief valve setting on a pipeline system.
7.3.3.2 Piping, piping systems and components shall have a minimum design
pressure of 1.0 MPa except for open ended lines where it is not to be less than 0.5
MPa.
7.3.4 Allowable stress
7.3.4.1 For pipes made of steel including stainless steel, the allowable
stress to be considered in the formula of the strength thickness in 7.3.2.1 shall be
the lower of the following values:
where:
- Rm = specified minimum tensile strength at room
temperature (N/mm²); and
- Re = specified minimum yield stress at room
temperature (N/mm²). If the stress strain curve does not show a defined yield
stress, the 0.2% proof stress applies.
7.3.4.2 Where necessary for mechanical strength to prevent damage,
collapse, excessive sag or buckling of pipes due to superimposed loads, the wall
thickness shall be increased over that required by 7.3.2 or, if this is
impracticable or would cause excessive local stresses, these loads shall be reduced,
protected against or eliminated by other design methods. Such superimposed loads may
be due to; supports, ship deflections, liquid pressure surge during transfer
operations, the weight of suspended valves, reaction to loading arm connections, or
otherwise.
7.3.4.3 For pipes made of materials other than steel, the allowable
stress shall be considered by the Administration.
7.3.4.4 High pressure fuel piping systems shall have sufficient
constructive strength. This shall be confirmed by carrying out stress analysis and
taking into account:
- .1 stresses due to the weight of the piping system;
- .2 acceleration loads when significant; and
- .3 internal pressure and loads induced by hog and sag of the ship.
7.3.4.5 When the design temperature is minus 110°C or colder, a complete
stress analysis, taking into account all the stresses due to weight of pipes,
including acceleration loads if significant, internal pressure, thermal contraction
and loads induced by hog and sag of the ship shall be carried out for each branch of
the piping system.
LR 7.3-03 The stress analysis is to be undertaken according to a
standard acceptable to LR. Tank connection space integrity calculations are to also
be included, see LR 6.3-01 and LR 6.3-02.
7.3.5 Flexibility of piping
7.3.5.1 The arrangement and installation of fuel piping shall provide the
necessary flexibility to maintain the integrity of the piping system in the actual
service situations, taking potential for fatigue into account.
LR 7.3-04 Fatigue analysis is required for all pressurised
low-flashpoint fuel piping arrangements subject to vibration or pulsating pressure
where failure of the pipe or its connection or a component would be the cause of a
prime mover being unavailable. The analysis is to recognise the pressures and
fluctuating stresses that the piping system may be subject to in normal service.
7.3.6 Piping fabrication and joining details
7.3.6.1 Flanges, valves and other fittings shall comply with a standard acceptable to
the Administration, taking into account the design pressure defined in 7.3.3.1. For
bellows and expansion joints used in vapour service, a lower minimum design pressure
than defined in 7.3.3.1 may be accepted.
7.3.6.2 All valves and expansion joints used in high pressure fuel piping systems
shall be approved according to a standard acceptable to the Administration.
7.3.6.3 The piping system shall be joined by welding with a minimum of flange
connections. Gaskets shall be protected against blow-out.
7.3.6.4 Piping fabrication and joining details shall comply with the following:
7.3.6.4.1 Direct connections
-
.1 Butt-welded joints with complete penetration at the root may be used in
all applications. For design temperatures colder than minus 10°C, butt welds
shall be either double welded or equivalent to a double welded butt joint.
This may be accomplished by use of a backing ring, consumable insert or
inert gas back-up on the first pass. For design pressures in excess of 1.0
MPa and design temperatures of minus 10°C or colder, backing rings shall be
removed.
-
.2 Slip-on welded joints with sleeves and related welding, having dimensions
in accordance with recognized standards, shall only be used for instrument
lines and open-ended lines with an external diameter of 50 mm or less and
design temperatures not colder than minus 55°C.
-
.3 Screwed couplings complying with recognized standards shall only be used
for accessory lines and instrumentation lines with external diameters of 25
mm or less.
7.3.6.4.2 Flanged connections
-
.1 Flanges in flange connections shall be of the welded neck, slip-on or
socket welded type; and
-
.2 For all piping except open ended, the following restrictions apply:
-
.1 For design temperatures colder than minus 55°C, only welded neck
flanges shall be used; and
-
.2 For design temperatures colder than minus 10°C, slip-on flanges
shall not be used in nominal sizes above 100 mm and socket welded
flanges shall not be used in nominal sizes above 50 mm.
7.3.6.4.3 Expansion joints
Where bellows and expansion joints are provided in accordance with 7.3.6.1 the
following apply:
-
.1 if necessary, bellows shall be protected against icing;
-
.2 slip joints shall not be used except within the liquefied gas fuel storage
tanks; and
-
.3 bellows shall normally not be arranged in enclosed spaces.
7.3.6.4.4 Other connections
Piping connections shall be joined in accordance with 7.3.6.4.1 to 7.3.6.4.3 but for
other exceptional cases the Administration may consider alternative
arrangements.
7.4 Regulations for
materials
LR 7.4-01 The Materials to be used in the construction of gas
bunkering stations, gas storage tanks including piping, gas process equipment and
gas-fuelled machinery have to be considered, as appropriate, in the risk assessment
(see Chapter 4.2), and are to be acceptable to LR. The materials also
need to satisfy the requirements of this Chapter.
7.4.1 Metallic materials
7.4.1.1 Materials for fuel containment and piping systems shall comply
with the minimum regulations given in the following tables:
- Table 7.1: Plates, pipes (seamless and welded), sections and
forgings for fuel tanks and process pressure vessels for design temperatures not
lower than 0°C.
- Table 7.2: Plates, sections and forgings for fuel tanks, secondary
barriers and process pressure vessels for design temperatures below 0°C and down
to minus 55°C.
- Table 7.3: Plates, sections and forgings for fuel tanks, secondary
barriers and process pressure vessels for design temperatures below minus 55°C
and down to minus 165°C.
- Table 7.4: Pipes (seamless and welded), forgings and castings for
fuel and process piping for design temperatures below 0°C and down to minus
165°C.
- Table 7.5: Plates and sections for hull structures required by
6.4.13.1.1.2.
Table 7.1
PLATES, PIPES (SEAMLESS AND WELDED) 1, 2,
SECTIONS AND FORGINGS FOR FUEL TANKS AND PROCESS PRESSURE
VESSELS FOR DESIGN TEMPERATURES NOT LOWER THAN
0°C
|
CHEMICAL
COMPOSITION AND HEAT TREATMENT
|
◆ Carbon-manganese
steel
|
◆ Fully killed fine
grain steel
|
◆ Small additions of
alloying elements by agreement with the Administration
|
◆ Composition limits to
be approved by the Administration
|
◆ Normalized, or
quenched and tempered4
|
TENSILE AND TOUGHNESS
(IMPACT) TEST REGULATIONS
|
Sampling
frequency
|
◆ Plates
|
Each "piece" to be
tested
|
◆ Sections and forgings
|
Each "batch" to be
tested.
|
Mechanical properties
|
◆ Tensile properties
|
Specified minimum yield
stress not to exceed 410 N/mm2 5
|
Toughness (Charpy V-notch test)
|
◆ Plates
|
Transverse test pieces.
Minimum average energy value (KV) 27J
|
◆ Sections and forgings
|
Longitudinal test
pieces. Minimum average energy (KV) 41J
|
◆ Test
temperature
|
Thickness t (mm)
|
Test temperature (°C)
|
T ≤ 20
|
0
|
20 < t ≤ 403
|
-20
|
Notes
|
1. For
seamless pipes and fittings normal practice applies. The use of
longitudinally and spirally welded pipes shall be specially
approved by the Administration.
|
2. Charpy
V-notch impact tests are not required for pipes.
|
3. This
Table is generally applicable for material thicknesses up to 40
mm. Proposals for greater thicknesses shall be approved by the
Administration.
|
4. A
controlled rolling procedure or thermo-mechanical controlled
processing (TMCP) may be used as an alternative.
|
5. Materials
with specified minimum yield stress exceeding 410
N/mm2 may be approved by the Administration. For
these materials, particular attention shall be given to the
hardness of the welded and heat affected zones.
|
Table LR 7.1
PLATES,
PIPES (SEAMLESS AND WELDED) 1, 2, SECTIONS AND
FORGINGS FOR FUEL TANKS AND PROCESS PRESSURE VESSELS FOR DESIGN
TEMPERATURES NOT LOWER THAN 0°C
|
CHEMICAL
COMPOSITION AND HEAT TREATMENT (See LR 2)
|
◆ Carbon-manganese
steel
|
◆ Fully killed fine grain
steel (See LR 4)
|
◆ Small additions of
alloying elements by agreement with the Administration
|
◆ Composition limits to be
approved by the Administration
|
◆ Normalized, or quenched
and tempered4 (See LR 4)
|
TENSILE AND TOUGHNESS
(IMPACT) TEST REGULATIONS
|
Sampling
frequency
|
◆ Plates
|
Each "piece" to be
tested
|
◆ Sections and forgings
|
Each "batch" to be
tested.
|
Mechanical
properties
|
◆ Tensile properties
|
Specified minimum yield
stress not to exceed 410 N/mm2 5 (See LR
4)
|
Toughness
(Charpy V-notch test)
|
◆ Plates
|
Transverse test pieces.
Minimum average energy value (KV) 27J
|
◆ Sections and forgings
|
Longitudinal test pieces.
Minimum average energy (KV) 41J
|
◆ Test
temperature
|
Thickness t (mm)3
|
Test temperature (°C)
|
T ≤ 20
|
0 (See LR 4)
|
20 < t ≤ 40
|
-20
|
Notes
|
1. For seamless
pipes and fittings normal practice applies. The use of
longitudinally and spirally welded pipes shall be specially approved
by the Administration. (See LR 1).
|
2. Charpy
V-notch impact tests are not required for pipes. (See LR
5).
|
3. This Table is
generally applicable for material thicknesses up to 40 mm. Proposals
for greater thicknesses shall be approved by the Administration.
(See LR 6).
|
4. A controlled
rolling procedure or thermo-mechanical controlled processing (TMCP)
may be used as an alternative.
|
5. Materials with
specified minimum yield stress exceeding 410 N/mm2 may be
approved by the Administration. For these materials, particular
attention shall be given to the hardness of the welded and heat
affected zones. (See LR 3).
|
LR 1 Welded
pressure pipes complying with the requirements of Chapter 6 of the
Rules for Materials are acceptable, and special approval is not
required. (See LR 4).
|
LR 2 Generally,
the chemical composition and mechanical properties, yield stress,
tensile strength and elongation are to comply with the requirements
for appropriate grades as given in the Rules for Materials.
|
LR 3 Stress
corrosion cracking can occur in tanks carrying natural gas
contaminated with hydrogen sulphide. In order to minimise this risk,
it is recommended that tanks intended for the carriage of this
substance are constructed in steel with a specified minimum tensile
strength not exceeding 410 N/mm2. If steels of higher
tensile strength are used, it is recommended that the completed fuel
tanks or process pressure vessels are given a suitable stress
relieving heat treatment in order to reduce the hardness of the weld
metal and heat affected zone to 250 Vickers Pyramid Number maximum
(HV).
|
LR 4 Stress
corrosion cracking can occur in tanks carrying natural gas
contaminated with hydrogen sulphide. Impact tests are to be made at
–20°C for all thicknesses. For pipes, test specimens are to be taken
in the longitudinal direction and are to have an average energy
value not less than 41J.
|
LR 5 Charpy
V-notch impact tests are to be carried out when required by the
Rules for Materials.
|
LR 6 For plates
of thickness greater than 40 mm and up to 50 mm for a design
temperature not lower than 0°C, the impact tests are to be conducted
in accordance with Table LR 7.1.1.
|
Table LR 7.1.1
PLATES, PIPES (SEAMLESS AND
WELDED) 1, 2, SECTIONS AND FORGINGS FOR FUEL TANKS
AND PROCESS PRESSURE VESSELS FOR DESIGN TEMPERATURES NOT LOWER
THAN 0°C with thickness 40mm < t
< 50mm
|
Test temperature
|
Thickness t (mm)
|
Test temperature (°C)
|
40 < t
< 50
|
−20 (see
LR 6a)
|
40 < t
< 50
|
−30 (see
LR 6b)
|
LR 6a:
Applies to Type C independent tanks and process pressure vessels. In
addition, post-weld heat treatment shall be performed. Proposals for
exemption of post-weld heat treatment based on an alternative
approach (e.g. Engineering Critical Assessment in accordance with
BS7910 or an equivalent Standard) shall be approved by LR.
LR
6b: Applies to fuel tank other than Type C.
|
Table 7.2
PLATES, SECTIONS AND FORGINGS 1 FOR
FUEL TANKS, SECONDARY BARRIERS AND PROCESS PRESSURE VESSELS
FOR DESIGN TEMPERATURES BELOW 0°C AND DOWN TO MINUS
55°C
|
Maximum thickness 25 mm 2
|
CHEMICAL
COMPOSITION AND HEAT TREATMENT
|
◆ Carbon-manganese
steel
|
◆ Fully killed,
aluminium treated fine grain steel
|
◆ Chemical composition
(ladle analysis)
|
|
C
|
Mn
|
Si
|
S
|
P
|
|
|
0.16% max. 3
|
0.70-1.60%
|
0.10-0.50%
|
0.025% max.
|
0.025% max.
|
|
|
Optional additions:
Alloys and grain refining elements may be generally in
accordance with the following
|
|
|
Ni
|
Cr
|
Mo
|
Cu
|
Nb
|
|
|
0.80% max.
|
0.25% max.
|
0.08% max.
|
0.35% max.
|
0.05% max.
|
|
|
V
|
|
|
|
|
|
|
0.10% max.
|
|
|
|
|
|
|
Al content total 0.020%
min. (Acid soluble 0.015% min.)
|
|
◆ Normalized, or
quenched and tempered 4
|
TENSILE AND TOUGHNESS
(IMPACT) TEST REGULATIONS
|
Sampling
frequency
|
◆ Plates
|
Each 'piece' to be
tested
|
◆ Sections and
forgings
|
Each 'batch' to be
tested
|
Mechanical properties
|
◆ Tensile
properties
|
Specified minimum yield
stress not to exceed 410 N/mm2, 5
|
Toughness
(Charpy V-notch test)
|
◆ Plates
|
Transverse test pieces.
Minimum average energy value (KV) 27J
|
◆ Sections and
forgings
|
Longitudinal test
pieces. Minimum average energy (KV) 41J
|
◆ Test
temperature
|
5°C below the design
temperature or -20°C whichever is lower
|
Notes
|
1.
|
The Charpy V-notch and chemistry regulations for forgings may
be specially considered by the Administration.
|
|
2.
|
For material
thickness of more than 25 mm, Charpy V-notch tests shall be
conducted as follows:
|
|
|
Material thickness
(mm)
|
Test
temperature (°C)
|
|
|
25 < t ≤ 30
|
10°C below design
temperature or -20°C whichever is lower
|
|
|
30 < t ≤ 35
|
15°C below design
temperature or -20°C whichever is lower
|
|
|
35 < t ≤ 40
|
20°C below design
temperature
|
|
|
40 < t
|
Temperature approved by
the Administration
|
|
|
The impact energy value shall be in accordance with the table
for the applicable type of test specimen. Materials for tanks
and parts of tanks which are completely thermally stress
relieved after welding may be tested at a temperature 5°C below
design temperature or -20°C whichever is lower. For thermally
stress relieved reinforcements and other fittings, the test
temperature shall be the same as that required for the adjacent
tank-shell thickness.
|
|
3.
|
By
special agreement with the Administration, the carbon content
may be increased to 0.18% maximum provided the design
temperature is not lower than -40°C
|
|
4.
|
A
controlled rolling procedure or thermo-mechanical controlled
processing (TMCP) may be used as an alternative.
|
|
5.
|
Materials with specified minimum yield stress exceeding 410
N/mm2 may be approved by the Administration. For
these materials, particular attention shall be given to the
hardness of the welded and heat affected zones.
|
|
|
Guidance:
|
For materials exceeding
25 mm in thickness for which the test temperature is -60°C or
lower, the application of specially treated steels or steels in
accordance with table 7.3 may be necessary.
|
Table LR 7.2
PLATES, SECTIONS AND FORGINGS1 FOR FUEL TANKS,
SECONDARY BARRIERS AND PROCESS PRESSURE VESSELS FOR DESIGN
TEMPERATURES BELOW 0°C AND DOWN TO MINUS 55°C
|
Maximum
thickness 25 mm2
|
CHEMICAL
COMPOSITION AND HEAT TREATMENT
|
◆ Carbon-manganese
steel
|
◆ Fully killed, aluminium
treated fine grain steel
|
◆ Chemical composition
(ladle analysis)
|
|
C
|
Mn
|
Si
|
S
|
P
|
|
|
0.16% max. 3
|
0.70-1.60%
|
0.10-0.50%
|
0.025% max.
|
0.025% max.
|
|
|
Optional additions: Alloys
and grain refining elements may be generally in accordance with the
following
|
|
|
Ni
|
Cr
|
Mo
|
Cu
|
Nb
|
|
|
0.80% max.
|
0.25%
max.
|
0.08% max.
|
0.35% max.
|
0.05% max.
|
|
|
V
|
|
|
|
|
|
|
0.10% max.
|
|
|
|
|
|
|
Al content total 0.020%
min. (Acid soluble 0.015% min.)
|
|
◆ Normalized, or quenched
and tempered 4
|
TENSILE AND TOUGHNESS
(IMPACT) TEST REGULATIONS
|
Sampling
frequency
|
◆ Plates
|
Each 'piece' to be
tested
|
◆ Sections and
forgings
|
Each 'batch' to be
tested
|
Mechanical
properties
|
◆ Tensile properties
|
Specified minimum yield
stress not to exceed 410 N/mm2, 5
|
Toughness
(Charpy V-notch test)
|
◆ Plates
|
Transverse test pieces.
Minimum average energy value (KV) 27J
|
◆ Sections and
forgings
|
Longitudinal test pieces.
Minimum average energy (KV) 41J
|
◆ Test temperature
|
5°C below the design
temperature or -20°C whichever is lower
|
Notes
|
1.
|
The
Charpy V-notch and chemistry regulations for forgings may be
specially considered by the Administration.
|
|
2.
|
For material
thickness of more than 25 mm, Charpy V-notch tests shall be
conducted as follows:
|
|
|
Material
thickness (mm)
|
Test
temperature (°C)
|
|
|
25 < t ≤
30
|
10°C below design
temperature or -20°C whichever is lower
|
|
|
30 < t ≤
35
|
15°C below design
temperature or -20°C whichever is lower
|
|
|
35 < t ≤
40
|
20°C below design
temperature
|
|
|
40 <
t
|
Temperature approved by the
Administration (See LR 1)
|
|
|
The
impact energy value shall be in accordance with the table for the
applicable type of test specimen. Materials for tanks and parts of
tanks which are completely thermally stress relieved after welding
may be tested at a temperature 5°C below design temperature or -20°C
whichever is lower. For thermally stress relieved reinforcements and
other fittings, the test temperature shall be the same as that
required for the adjacent tank-shell thickness. (See
LR 1a)
|
|
3.
|
By
special agreement with the Administration, the carbon content may be
increased to 0.18% maximum provided the design temperature is not
lower than -40°C
|
|
4.
|
A
controlled rolling procedure or thermo-mechanical controlled
processing (TMCP) may be used as an alternative.
|
|
5.
|
Materials with specified minimum yield stress exceeding 410
N/mm2 may be approved by the Administration. For
these materials, particular attention shall be given to the hardness
of the welded and heat affected zones.
|
|
LR 1
|
For
plates of thickness greater than 40 mm and up to 50 mm for a design
temperature below 0°C and down to −55°C, the impact tests shall be
conducted in accordance with Table LR 7.2.1.
|
|
LR 2
|
Stress corrosion cracking can occur in tanks carrying natural gas
contaminated with hydrogen sulphide, see 17.12 of the Rules
for Ships for Liquefied Gases. If steels of higher tensile strength
are used, it is recommended that the completed fuel tanks or process
pressure vessels are given a suitable stress relieving heat
treatment in order to reduce the hardness of the weld metal and heat
affected zone to 250 HV maximum.
|
|
|
Guidance:
|
For materials exceeding 25
mm in thickness for which the test temperature is -60°C or lower,
the application of specially treated steels or steels in accordance
with table 7.3 may be necessary.
|
Table LR 7.2.1
Test temperature
|
Thickness t (mm)
|
Test temperature (°C)
|
40 < t
< 50
|
5°C below design temperature or –20°C, whichever is lower
(see LR 1a)
|
40 < t
< 45
|
25°C below design temperature (see LR 1b)
|
45 < t
< 50
|
30°C below design temperature (see LR 1b)
|
LR 1a:
Applies to Type C independent tanks and process pressure vessels.
Post-weld heat treatment shall be performed. Proposals for exemption
of post-weld heat treatment based on an alternative approach (e.g.
Engineering Critical Assessment in accordance with BS7910 or an
equivalent Standard) shall be approved by LR.
LR 1b:
Applies to fuel tank other than Type C.
|
Table 7.3
PLATES, SECTIONS AND FORGINGS 1 FOR
FUEL TANKS, SECONDARY BARRIERS AND PROCESS PRESSURE VESSELS
FOR DESIGN TEMPERATURES BELOW MINUS 55°C AND DOWN TO MINUS
165°C2
|
Maximum thickness 25 mm 3, 4
|
Minimum
design temp. (°C)
|
Chemical
composition5 and heat treatment
|
Impact
test temp. (°C)
|
-60
|
1.5% nickel steel –
normalized or normalized and tempered or quenched and tempered
or TMCP see note 6
|
-65
|
-65
|
2.25% nickel steel –
normalized or normalized and tempered or quenched and tempered
or TMCP6, 7
|
-70
|
-90
|
3.5% nickel steel –
normalized or normalized and tempered or quenched and tempered
or TMCP6, 7
|
-95
|
-105
|
5% nickel steel –
normalized or normalized and tempered or quenched and
tempered6, 7 and 8
|
-110
|
-165
|
9% nickel steel –
double normalized and tempered or quenched and
tempered6
|
-196
|
-165
|
Austenitic steels, such
as types 304, 304L, 316, 316L, 321 and 347 solution
treated9
|
-196
|
-165
|
Aluminium alloys; such
as type 5083 annealed
|
Not
required
|
-165
|
Austenitic Fe-Ni alloy
(36% nickel) Heat treatment as agreed
|
Not
required
|
TENSILE AND TOUGHNESS
(IMPACT) TEST REGULATIONS
|
Sampling
frequency
|
◆ Plates
|
Each 'piece' to be
tested
|
◆ Sections and
forgings
|
Each 'batch' to be
tested
|
Toughness
(Charpy V-notch test)
|
◆ Plates
|
Transverse test pieces.
Minimum average energy value (KV) 27J
|
◆ Sections and
forgings
|
Longitudinal test
pieces. Minimum average energy (KV) 41J
|
Notes
|
1.
|
The impact
test required for forgings used in critical applications shall
be subject to special consideration by the
Administration.
|
2.
|
The
regulations for design temperatures below –165°C shall be
specially agreed with the Administration.
|
3.
|
For
materials 1.5% Ni, 2.25% Ni, 3.5% Ni and 5% Ni, with thicknesses
greater than 25 mm, the impact tests shall be conducted as
follows:
|
|
|
Material
thickness (mm)
|
Test
temperature (°C)
|
|
|
25 <
t ≤ 30
|
10°C below design
temperature
|
|
|
30 < t
≤ 35
|
15°C below design
temperature
|
|
|
35 < t
≤ 40
|
20°C below design
temperature
|
|
|
The energy value shall be in accordance with the table for the
applicable type of test specimen. For material thickness of more
than 40 mm, the Charpy V-notch values shall be specially
considered.
|
4.
|
For 9% Ni steels, austenitic stainless steels and aluminium
alloys, thickness greater than 25 mm may be used.
|
5.
|
The chemical composition limits shall be in accordance with
recognized standards.
|
6.
|
Thermo-mechanical controlled processing (TMCP) nickel steels
will be subject to acceptance by the Administration.
|
7.
|
A
lower minimum design temperature for quenched and tempered
steels may be specially agreed with the Administration.
|
8.
|
A
specially heat treated 5% nickel steel, for example triple heat
treated 5% nickel steel, may be used down to –165°C, provided
that the impact tests are carried out at –196°C.
|
9.
|
The impact test may be omitted subject to agreement with the
Administration.
|
|
|
|
|
|
|
Table LR 7.3
PLATES, SECTIONS AND FORGINGS1 FOR FUEL TANKS,
SECONDARY BARRIERS AND PROCESS PRESSURE VESSELS FOR DESIGN
TEMPERATURES BELOW MINUS 55°C AND DOWN TO MINUS
165°C2
|
Maximum thickness 25 mm 3, 4
|
Minimum
design temp. (°C)
|
Chemical
composition5 and heat treatment
|
Impact test
temp. (°C)
|
-60
|
1.5% nickel steel –
normalized or normalized and tempered or quenched and tempered or
TMCP see note 6
|
-65
|
-65
|
2.25% nickel steel –
normalized or normalized and tempered or quenched and tempered or
TMCP6, 7
|
-70
|
-90
|
3.5% nickel steel –
normalized or normalized and tempered or quenched and tempered or
TMCP6, 7
|
-95
|
-105
|
5% nickel steel – normalized
or normalized and tempered or quenched and tempered6, 7 and
8
|
-110
|
-165
|
9% nickel steel – double
normalized and tempered or quenched and tempered6
|
-196
|
-165
|
Austenitic steels, such as
types 304, 304L, 316, 316L, 321 and 347 solution treated9
(See LR 4)
|
-196
|
-165
|
Aluminium alloys; such as
type 5083 annealed
|
Not
required
|
-165
|
Austenitic Fe-Ni alloy (36%
nickel) Heat treatment as agreed
|
Not
required
|
TENSILE AND TOUGHNESS
(IMPACT) TEST REGULATIONS
|
Sampling
frequency
|
◆ Plates
|
Each 'piece' to be
tested
|
◆ Sections and
forgings
|
Each 'batch' to be
tested
|
Toughness
(Charpy V-notch test)
|
◆ Plates
|
Transverse test pieces.
Minimum average energy value (KV) 27J
|
◆ Sections and
forgings
|
Longitudinal test pieces.
Minimum average energy (KV) 41J
|
Notes
|
1.
|
The impact test
required for forgings used in critical applications shall be subject
to special consideration by the Administration.
|
2.
|
The regulations
for design temperatures below –165°C shall be specially agreed with
the Administration.
|
3.
|
For materials
1.5% Ni, 2.25% Ni, 3.5% Ni and 5% Ni, with thicknesses greater than
25 mm, the impact tests shall be conducted as follows:
|
|
|
Material
thickness (mm)
|
Test
temperature (°C)
|
|
|
25 < t ≤
30
|
10°C below design
temperature
|
|
|
30 < t ≤
35
|
15°C below design
temperature
|
|
|
35 < t ≤
40
|
20°C below design
temperature
|
|
|
The
energy value shall be in accordance with the table for the
applicable type of test specimen. For material thickness of more
than 40 mm, the Charpy V-notch values shall be specially considered.
(See
LR 5)
|
4.
|
For
9% Ni steels, austenitic stainless steels and aluminium alloys,
thickness greater than 25 mm may be used.
|
5.
|
The
chemical composition limits shall be in accordance with recognized
standards.
|
6.
|
Thermo-mechanical controlled processing (TMCP) nickel steels will
be subject to acceptance by the Administration.
|
7.
|
A
lower minimum design temperature for quenched and tempered steels
may be specially agreed with the Administration.
|
8.
|
A
specially heat treated 5% nickel steel, for example triple heat
treated 5% nickel steel, may be used down to –165°C, provided that
the impact tests are carried out at –196°C.
|
9.
|
The
impact test may be omitted subject to agreement with the
Administration. (See LR 2)
|
LR 1
|
In no
case should the test temperature exceed that shown in the main Table
above.
|
LR 2
|
Generally, impact tests are not required.
|
LR 3
|
Stress corrosion cracking can occur in tanks carrying natural gas
contaminated with hydrogen sulphide, see 17.12 of the Rules
for Ships for Liquefied Gases. If steels of higher tensile strength
are used, it is recommended that the completed fuel tanks or process
pressure vessels are given a suitable stress relieving heat
treatment in order to reduce the hardness of the weld metal and heat
affected zone to 250 HV maximum.
|
LR 4
|
Grades 304 and 316 are not to be used for welded
construction.
|
LR 5
|
For materials
1,5% Ni, 2,25% Ni, 3,5% Ni and 5% Ni, with thicknesses greater than
40 mm and up to 50 mm, the impact tests shall be conducted in
accordance with Table LR 7.3.1.
|
Table LR 7.3.1
Material thickness t (mm)
|
Test temperature (°C)
|
40 < t
< 45
|
25°C below design temperature
|
45 < t
< 50
|
30°C below design temperature
|
Table 7.4
PIPES (SEAMLESS AND WELDED)1,
FORGINGS2 AND CASTINGS2 FOR FUEL
AND PROCESS PIPING FOR DESIGN TEMPERATURES BELOW 0°C AND
DOWN TO MINUS 165°C3
|
Maximum
thickness 25 mm
|
Minimum design
temp.(°C)
|
Chemical
composition5 and heat treatment
|
Impact
test
|
Test temp. (°C)
|
Minimum average energy
(KV)
|
-55
|
Carbon-manganese steel. Fully killed fine grain.
Normalized or as agreed.6
|
See note 4
|
27
|
-65
|
2.25% nickel steel. Normalized, Normalized and
tempered or quenched and tempered.6
|
-70
|
34
|
-90
|
3.5% nickel steel. Normalized, Normalized and
tempered or quenched and tempered.6
|
-95
|
34
|
-165
|
9% nickel steel7. Double normalized
and tempered or quenched and tempered.
|
-196
|
41
|
Austenitic steels, such as types 304, 304L, 316,
316L, 321 and 347. Solution treated.8
|
-196
|
41
|
Aluminium alloys; such as type 5083
annealed
|
|
Not required
|
TENSILE AND TOUGHNESS
(IMPACT) TEST REGULATIONS
|
Sampling
frequency
|
◆ Each 'batch' to be
tested.
|
Toughness
(Charpy V-notch test)
|
◆ Impact test:
Longitudinal test pieces
|
Notes
|
1. The use of
longitudinally or spirally welded pipes shall be specially
approved by the Administration.
|
2. The
regulations for forgings and castings may be subject to special
consideration by the Administration.
|
3. The
regulations for design temperatures below -165°C shall be
specially agreed with the Administration.
|
4. The test
temperature shall be 5°C below the design temperature or -20°C
whichever is lower.
|
5. The
composition limits shall be in accordance with Recognized
Standards.
|
6. A lower
design temperature may be specially agreed with the
Administration for quenched and tempered materials.
|
7. This
chemical composition is not suitable for castings.
|
8. Impact tests may be
omitted subject to agreement with the Administration.
|
Table LR 7.4
PIPES (SEAMLESS AND WELDED)1,
FORGINGS2 AND CASTINGS2 FOR FUEL AND
PROCESS PIPING FOR DESIGN TEMPERATURES BELOW 0°C AND DOWN TO
MINUS 165°C3
|
Maximum
thickness 25 mm
|
Minimum design
temp.(°C)
|
Chemical
composition5 and heat treatment
|
Impact
test
|
Test temp. (°C)
|
Minimum average energy (KV)
|
-55
|
Carbon-manganese steel. Fully killed fine grain.
Normalized or as agreed.6
|
See note 4
|
27
|
-65
|
2.25% nickel steel. Normalized, Normalized and
tempered or quenched and tempered.6
|
-70
|
34
|
-90
|
3.5% nickel steel. Normalized, Normalized and
tempered or quenched and tempered.6
|
-95
|
34
|
-165
|
9% nickel steel7. Double normalized and
tempered or quenched and tempered.
|
-196
|
41
|
Austenitic steels, such as types 304, 304L, 316,
316L, 321 and 347. Solution treated.8 (See LR
3)
|
-196
|
41
|
Aluminium alloys; such as type 5083 annealed
|
|
Not required
|
TENSILE AND TOUGHNESS
(IMPACT) TEST REGULATIONS
|
Sampling
frequency
|
◆ Each 'batch' to be
tested.
|
Toughness
(Charpy V-notch test)
|
◆ Impact test: Longitudinal
test pieces
|
Notes
|
1. The use of
longitudinally or spirally welded pipes shall be specially approved
by the Administration. (See LR 1)
|
2. The
regulations for forgings and castings may be subject to special
consideration by the Administration.
|
3. The
regulations for design temperatures below -165°C shall be specially
agreed with the Administration.
|
4. The test
temperature shall be 5°C below the design temperature or -20°C
whichever is lower.
|
5. The
composition limits shall be in accordance with Recognized
Standards.
|
6. A lower
design temperature may be specially agreed with the Administration
for quenched and tempered materials.
|
7. This chemical
composition is not suitable for castings.
|
8. Impact tests
may be omitted subject to agreement with the Administration.
(See LR 2)
|
LR 1 Welded
pressure pipes complying with the requirements of Chapter 6 of the
Rules for Materials are acceptable and special approval is not
required.
|
LR 2 Impact tests
are not required except for austenitic steel castings intended for
applications where the design temperature is lower than –55°C.
|
LR 3 Grades 304 and 316 are
not to be used for welded pipework.
|
Table 7.5
PLATES
AND SECTIONS FOR HULL STRUCTURES REQUIRED BY
6.4.13.1.1.2
|
Minimum design temperature of hull structure (°C)
|
Maximum
thickness (mm) for steel grades
|
A
|
B
|
D
|
E
|
AH
|
DH
|
EH
|
FH
|
0 and above
|
Recognized Standards
|
down to -5
|
15
|
25
|
30
|
50
|
25
|
45
|
50
|
50
|
down to -10
|
x
|
20
|
25
|
50
|
20
|
40
|
50
|
50
|
down to -20
|
x
|
x
|
20
|
50
|
x
|
30
|
50
|
50
|
down to -30
|
x
|
x
|
x
|
40
|
x
|
20
|
40
|
50
|
Below -30
|
In
accordance with table 7.2 except that the thickness limitation
given in table 7.2 and in footnote 2 of that table does not
apply.
|
Notes
|
'x' means steel grade
not to be used.
|
LR 7.4–02 The materials of the hull structure are to comply with
the requirements of the Rules for Materials. The requirements of Pt 3, Ch 2 of the
Rules for Ships are also to be complied with, except as indicated otherwise by the
requirements of these Rules.
LR 7.4–03 Where higher tensile steel is used in the hull
structure, the scantling and arrangements are to be as required by Part 3 and Part 4
of the Rules for Ships.
LR 7.4–04 Plans illustrating the means of protection for the ship
steelwork, e.g. drip trays, cladding, etc., at bunkering manifolds; deck tanks, fuel
handling system, etc., are to be submitted for approval.
7.4.1.2 Materials having a melting point below 925°C shall not be used for piping
outside the fuel tanks.
7.4.1.3 For CNG tanks, the use of materials not covered above may be specially
considered by the Administration.
7.4.1.4 Where required the outer pipe or duct containing high pressure gas in the
inner pipe shall as a minimum fulfil the material regulations for pipe materials
with design temperature down to minus 55°C in table 7.4.
7.4.1.5 The outer pipe or duct around liquefied gas fuel pipes shall as a minimum
fulfil the material regulations for pipe materials with design temperature down to
minus 165°C in table 7.4.
|