4.3 Functional requirements
4.3.1 The design life of the cargo containment system
shall not be less than the design life of the ship.
4.3.2 Cargo containment systems shall be designed for
North Atlantic environmental conditions and relevant long-term sea state scatter
diagrams for unrestricted navigation. Lesser environmental conditions, consistent
with the expected usage, may be accepted by the Administration for cargo containment
systems used exclusively for restricted navigation. Greater environmental conditions
may be required for cargo containment systems operated in conditions more severe
than the North Atlantic environment.
4.3.3 Cargo containment systems shall be designed with
suitable safety margins:
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.1 to withstand, in the intact condition, the
environmental conditions anticipated for the cargo containment system's
design life and the loading conditions appropriate for them, which include
full homogeneous and partial load conditions, partial filling within defined
limits and ballast voyage loads; and
-
.2 being appropriate for uncertainties in
loads, structural modelling, fatigue, corrosion, thermal effects, material
variability, ageing and construction tolerances.
LR 4.3-01 Except as otherwise mentioned, the suitable safety
margin is to be considered as 2,0. Designers may propose a lower safety margin
provided that a technical justification is submitted and justified.
4.3.4 The cargo containment system structural strength
shall be assessed against failure modes, including but not limited to plastic
deformation, buckling and fatigue. The specific design conditions which shall be
considered for the design of each cargo containment system are given in 4.21 to
4.26. There are three main categories of design conditions:
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.1 Ultimate design conditions – the cargo
containment system structure and its structural components shall withstand
loads liable to occur during its construction, testing and anticipated use
in service, without loss of structural integrity. The design shall take into
account proper combinations of the following loads:
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.1 internal pressure;
-
.2 external pressure;
-
.3 dynamic loads due to the motion of
the ship;
-
.4 thermal loads;
-
.5 sloshing loads;
-
.6 loads corresponding to ship
deflections;
-
.7 tank and cargo weight with the
corresponding reaction in way of supports;
-
.8 insulation weight;
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.9 loads in way of towers and other
attachments; and
-
.10 test loads.
-
.2 Fatigue design conditions – the cargo
containment system structure and its structural components shall not fail
under accumulated cyclic loading.
-
.3 The cargo containment system shall meet the
following criteria:
-
.1 Collision – the cargo containment
system shall be protectively located in accordance with 2.4.1 and
withstand the collision loads specified in 4.15.1 without
deformation of the supports, or the tank structure in way of the
supports, likely to endanger the tank structure.
-
.2 Fire – the cargo containment systems
shall sustain, without rupture, the rise in internal pressure
specified in 8.4.1 under the fire scenarios envisaged therein.
-
.3 Flooded compartment causing buoyancy
on tank – the anti-flotation arrangements shall sustain the upward
force, specified in 4.15.2, and there shall be no endangering
plastic deformation to the hull.
4.3.5 Measures shall be applied to ensure that
scantlings required meet the structural strength provisions and be maintained
throughout the design life. Measures may include, but are not limited to, material
selection, coatings, corrosion additions, cathodic protection and inerting.
Corrosion allowance need not be required in addition to the thickness resulting from
the structural analysis. However, where there is no environmental control, such as
inerting around the cargo tank, or where the cargo is of a corrosive nature, the
Administration or recognized organization acting on its behalf may require a
suitable corrosion allowance.
4.3.6 An inspection/survey plan for the cargo
containment system shall be developed and approved by the Administration or
recognized organization acting on its behalf. The inspection/survey plan shall
identify areas that need inspection during surveys throughout the cargo containment
system's life and, in particular, all necessary in-service survey and maintenance
that was assumed when selecting cargo containment system design parameters. Cargo
containment systems shall be designed, constructed and equipped to provide adequate
means of access to areas that need inspection as specified in the inspection/survey
plan. Cargo containment systems, including all associated internal equipment, shall
be designed and built to ensure safety during operations, inspection and maintenance
(see 3.5).
LR 4.3-02 Due consideration is to be given to the design
parameters and construction of the cargo containment system, when developing the
inspection/survey plan of the cargo containment system, see also 4.18, 4.19
and 4.20.
4.4 Cargo containment safety principles
4.4.1 The containment systems shall be provided with a
full secondary liquid-tight barrier capable of safely containing all potential
leakages through the primary barrier and, in conjunction with the thermal insulation
system, of preventing lowering of the temperature of the ship structure to an unsafe
level.
4.4.2 However, the size and configuration or
arrangement of the secondary barrier may be reduced where an equivalent level of
safety is demonstrated in accordance with the requirements of 4.4.3 to 4.4.5, as
applicable.
4.4.3 Cargo containment systems for which the
probability for structural failures to develop into a critical state has been
determined to be extremely low, but where the possibility of leakages through the
primary barrier cannot be excluded, shall be equipped with a partial secondary
barrier and small leak protection system capable of safely handling and disposing of
the leakages. The arrangements shall comply with the following requirements:
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.1 failure developments that can be reliably
detected before reaching a critical state (e.g. by gas detection or
inspection) shall have a sufficiently long development time for remedial
actions to be taken; and
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.2 failure developments that cannot be safely
detected before reaching a critical state shall have a predicted development
time that is much longer than the expected lifetime of the tank.
4.4.4 No secondary barrier is required for cargo
containment systems, e.g. type C independent tanks, where the probability for
structural failures and leakages through the primary barrier is extremely low and
can be neglected.
4.4.5 No secondary barrier is required where the cargo
temperature at atmospheric pressure is at or above -10°C.
4.5
Secondary barriers in relation to tank types
Secondary barriers in relation to the tank types defined in 4.21 to 4.26
shall be provided in accordance with the following table.
Cargo temperature at atmospheric pressure
|
-10°C and above
|
Below -10°C down to -55°C
|
Below -55°C
|
Basic tank
type
|
No secondary
barrier required
|
Hull may act as
secondary barrier
|
Separate
secondary barrier where required
|
Integral
|
|
Tank type not normally allowed1
|
Membrane
|
|
Complete secondary barrier
|
Semi-membrane
|
|
Complete secondary barrier2
|
Independent:
|
|
|
-type A
|
|
Complete secondary barrier
|
-type B
|
|
Partial secondary barrier
|
-type C
|
|
No secondary barrier required
|
Note 1: A complete secondary barrier shall normally be required if
cargoes with a temperature at atmospheric pressure below -10°C are
permitted in accordance with 4.25.1.
|
Note 2: In the case of semi-membrane tanks that comply in all
respects with the requirements applicable to type B independent
tanks, except for the manner of support, the Administration may,
after special consideration, accept a partial secondary
barrier.
|
4.6
Design of secondary barriers
4.6.1 Where the cargo temperature at atmospheric
pressure is not below -55°C, the hull structure may act as a secondary barrier based
on the following:
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.1 the hull material shall be suitable for the
cargo temperature at atmospheric pressure as required by 4.19.1.4; and
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.2 the design shall be such that this
temperature will not result in unacceptable hull stresses.
4.6.2 The design of the secondary barrier shall be such
that:
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.1 it is capable of containing any envisaged
leakage of liquid cargo for a period of 15 days, unless different criteria
apply for particular voyages, taking into account the load spectrum referred
to in 4.18.2.6;
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.2 physical, mechanical, or operational events
within the cargo tank that could cause failure of the primary barrier shall
not impair the due function of the secondary barrier, or vice versa;
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.3 failure of a support or an attachment to the
hull structure will not lead to loss of liquid tightness of both the primary
and secondary barriers;
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.4 it is capable of being periodically checked
for its effectiveness by means acceptable to the Administration or
recognized organization acting on its behalf. This may be by means of a
visual inspection or a pressure/vacuum test or other suitable means carried
out according to a documented procedure agreed with the Administration or
the recognized organization acting on its behalf;
LR 4.6-01 For containment systems with glued secondary barriers
the following factors are to be taken into account:
- At the time of construction, a tightness test is to be carried out
in accordance with approved system designers’ procedures and acceptance criteria
before and after initial cool down. Low differential pressures tests are not
considered an acceptable test.
- If the designer’s threshold values are exceeded, an investigation
is to be carried out and additional testing such as thermographic or acoustic
emissions testing should be carried out.
- The values recorded are to be used as reference for future
assessment of secondary barrier tightness.
For containment systems with welded metallic secondary barriers, a
tightness test after initial cool down is not required.
LR 4.6-02 The requirement of LR 4.6-01 is to be applied unless
specified otherwise by the National Administration.
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.5 the methods required in .4 above shall be
approved by the Administration or recognized organization acting on its
behalf and shall include, where applicable to the test procedure:
-
.1 details on the size of defect
acceptable and the location within the secondary barrier, before its
liquid-tight effectiveness is compromised;
-
.2 accuracy and range of values of the
proposed method for detecting defects in .1 above;
-
.3 scaling factors to be used in
determining the acceptance criteria, if full scale model testing is
not undertaken; and
-
.4 effects of thermal and mechanical
cyclic loading on the effectiveness of the proposed test; and
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.6 the secondary barrier shall fulfil its
functional requirements at a static angle of heel of 30°.
4.7
Partial secondary barriers and primary barrier small leak protection
system
4.7.1 Partial secondary barriers as permitted in 4.4.3
shall be used with a small leak protection system and meet all the requirements in
4.6.2. The small leak protection system shall include means to detect a leak in the
primary barrier, provision such as a spray shield to deflect any liquid cargo down
into the partial secondary barrier, and means to dispose of the liquid, which may be
by natural evaporation.
4.7.2 The capacity of the partial secondary barrier
shall be determined, based on the cargo leakage corresponding to the extent of
failure resulting from the load spectrum referred to in 4.18.2.6, after the initial
detection of a primary leak. Due account may be taken of liquid evaporation, rate of
leakage, pumping capacity and other relevant factors.
4.7.3 The required liquid leakage detection may be by
means of liquid sensors, or by an effective use of pressure, temperature or gas
detection systems, or any combination thereof.
4.8
Supporting arrangements
4.8.1 The cargo tanks shall be supported by the hull in
a manner that prevents bodily movement of the tank under the static and dynamic
loads defined in 4.12 to 4.15, where applicable, while allowing contraction and
expansion of the tank under temperature variations and hull deflections without
undue stressing of the tank and the hull.
4.8.2 Anti-flotation arrangements shall be provided for
independent tanks and capable of withstanding the loads defined in 4.15.2 without
plastic deformation likely to endanger the hull structure.
4.8.3 Supports and supporting arrangements shall
withstand the loads defined in 4.13.9 and 4.15, but these loads need not be combined
with each other or with wave-induced loads.
LR 4.8-01 Tank supports are to be located in way of the primary
support structure of the tank and the ship’s hull. Steel seatings are to be
arranged, where possible, on both the inner bottom and underside of the cargo tank
so as to ensure an effective distribution of the transmitted load and reactions into
the cargo tanks and double bottom structure.
LR 4.8-02 An adequate clearance is to be provided between the
antiflotation chocks and the ship’s hull in all operational conditions. Details of
the calculations of the clearances between antiflotation chocks are to be submitted
for approval. The inspection/survey plan indicated in 4.3.6 is to include details
for the verification of these clearances during construction and periodical
surveys.
LR 4.8-03 The strength of supports is to be verified by direct
calculation, see LR III.5.
4.9
Associated structure and equipment
4.9.1 Cargo containment systems shall be designed for
the loads imposed by associated structure and equipment. This includes pump towers,
cargo domes, cargo pumps and piping, stripping pumps and piping, nitrogen piping,
access hatches, ladders, piping penetrations, liquid level gauges, independent level
alarm gauges, spray nozzles, and instrumentation systems (such as pressure,
temperature and strain gauges).
4.10
Thermal insulation
4.10.1 Thermal insulation shall be provided, as
required, to protect the hull from temperatures below those allowable (see 4.19.1)
and limit the heat flux into the tank to the levels that can be maintained by the
pressure and temperature control system applied in chapter 7.
4.10.2 In determining the insulation performance, due
regard shall be given to the amount of the acceptable boil-off in association with
the reliquefaction plant on board, main propulsion machinery or other temperature
control system.