Section 5 Materials and construction
5.1 Materials
5.1.2
Materials forming the structure of the ship unit
- To determine the grade of plate and sections
used in the hull structure, a temperature calculation shall be performed for
all tank types when the cargo temperature is below –10°C. The following
assumptions should be made in this calculation:
- The primary barrier of all tanks shall be assumed to be at
the cargo temperature.
- In addition to item 1, where a complete or partial secondary
barrier is required it shall be assumed to be at the cargo temperature at
atmospheric pressure for any one tank only.
- The ambient temperatures for air and
sea-water are to be taken at their lowest daily mean temperatures for the
unit’s proposed area of operation based on the 100 year average return
period. The ambient temperatures are to be rounded down to the nearest
degree Celsius. The ambient temperatures are not to be taken as greater
than 5°C for air and 0°C for sea-water unless agreed by LR.
- Still air and sea water conditions shall be assumed, i.e. no
adjustment for forced convection.
- Degradation of the thermal insulation
properties over the life of the ship unit due to factors such as thermal
and mechanical ageing, compaction, ship motions and tank vibrations as
defined in Pt 11, Ch 4, 5.1 Materials 5.1.4 and Pt 11, Ch 4, 5.1 Materials 5.1.4 shall be assumed.
- The cooling effect of the rising boil-off
vapour from the leaked cargo should be taken into account where
applicable.
- No credit shall be given for any means of heating, except as
described in Pt 11, Ch 4, 5.1 Materials 5.1.2 and provided the heating
arrangements are in compliance with Pt 11, Ch 4, 5.1 Materials 5.1.2.
- For members connecting inner and outer hulls, the mean
temperature may be taken for determining the steel grade.
When heat transmission studies are carried out, the heat
balance method is acceptable to LR.
- The shell and deck plating of the ship unit and
all stiffeners attached thereto shall be in accordance with the requirements of
Pt 10 SHIP UNITS and this Part. If the calculated
temperature of the material in the design condition is below –5°C due to the
influence of the cargo temperature and ambient sea and air temperatures, the
material shall be in accordance with Pt 11, Ch 6, 1.4 Requirements for metallic materials 1.4.1. The ambient sea and air temperatures
are to be determined as defined in Pt 11, Ch 4, 5.1 Materials 5.1.2.
- The materials of all other hull structures for
which the calculated temperature in the design condition is below 0°C, due to
the influence of cargo temperature and ambient sea and air temperatures, and
that do not form the secondary barrier, shall also be in accordance with Pt 11, Ch 6, 1.4 Requirements for metallic materials 1.4.1. This includes hull structure
supporting the cargo tanks, inner bottom plating, longitudinal bulkhead
plating, transverse bulkhead plating, floors, webs, stringers and all attached
stiffening members. The ambient sea and air temperatures are to be determined
as defined in Pt 11, Ch 4, 5.1 Materials 5.1.2.
- The hull material forming the secondary barrier shall be in
accordance with Pt 11, Ch 6, 1.4 Requirements for metallic materials 1.4.1. Where the secondary
barrier is formed by the deck or side shell plating, the material grade
required by Pt 11, Ch 6, 1.4 Requirements for metallic materials 1.4.1 shall be carried into
the adjacent deck or side shell plating, where applicable, to a suitable
extent.
- Means of heating structural materials may be
used to ensure that the material temperature does not fall below the minimum
allowed for the grade of material specified in Pt 11, Ch 6, 1.4 Requirements for metallic materials 1.4.1. In the calculations required in Pt 11, Ch 4, 5.1 Materials 5.1.2, credit for such heating may be taken
in accordance with the following:
- for any transverse hull structure;
- for longitudinal hull structure referred
to in Pt 11, Ch 4, 5.1 Materials 5.1.2 and Pt 11, Ch 4, 5.1 Materials 5.1.2 where colder ambient temperatures
are specified, provided the material remains suitable for the ambient
temperature conditions of +5°C for air and 0°C for sea-water with no
credit taken in the calculations for heating; and
- as an alternative to Pt 11, Ch 4, 5.1 Materials 5.1.2, for longitudinal bulkhead
between cargo tanks, credit may be taken for heating provided the
material remains suitable for a minimum design temperature of –30°C, or a
temperature 30°C lower than that determined by Pt 11, Ch 4, 5.1 Materials 5.1.2 with the heating considered,
whichever is less. In this case, the longitudinal strength of the ship
unit shall comply with SOLAS Regulation Regulation 3-1 - Structural, mechanical and electrical requirements for ships for both when those bulkhead(s)
are considered effective and not.
- The means of heating referred to in Pt 11, Ch 4, 5.1 Materials 5.1.2 shall comply with the following
requirements:
- the heating system shall be arranged so that, in the event
of failure in any part of the system, standby heating can be maintained
equal to not less than 100 per cent of the theoretical heat
requirement;
- the heating system shall be considered as an essential
auxiliary. All electrical components of at least one of the systems
provided in accordance with Pt 11, Ch 4, 5.1 Materials 5.1.2 shall be supplied
from the essential source of electrical power; and
- the design and construction of the heating system shall be
included in the approval of the containment system by LR.
Details of the proposed heating system are to be
submitted.
5.1.3
Materials of primary and secondary barriers
- Metallic materials used in the construction of primary and
secondary barriers not forming the hull, shall be suitable for the design loads
that they may be subjected to, and be in accordance with Pt 11, Ch 6, 1.4 Requirements for metallic materials 1.4.1, Pt 11, Ch 6, 1.4 Requirements for metallic materials 1.4.1 or Pt 11, Ch 6, 1.4 Requirements for metallic materials 1.4.1.
- Materials, either non-metallic or metallic but not covered by
Pt 11, Ch 6, 1.4 Requirements for metallic materials 1.4.1, Pt 11, Ch 6, 1.4 Requirements for metallic materials 1.4.1 and Pt 11, Ch 6, 1.4 Requirements for metallic materials 1.4.1, used in the primary and secondary barriers
may be approved by LR considering the design loads that they may be subjected
to, their properties and their intended use.
- Where non-metallic materials, including composites, are used for or
incorporated in the primary or secondary barriers, they shall be tested for the
following properties, as applicable, to ensure that they are adequate for the
intended service:
- compatibility with the cargoes;
- solubility in cargo;
- absorption of cargo;
- ageing;
- density;
- mechanical properties;
- thermal expansion and contraction;
- abrasion;
- cohesion;
- resistance to vibrations;
- resistance to fire and flame spread;
- resistance to fatigue failure and crack propagation;
- influence of water;
- resistance to cargo pressure.
- The above properties, where applicable, shall be tested for the range between
the expected maximum temperature in service and 5°C below the minimum design
temperature, but not lower than –196°C.
- Where non-metallic materials, including composites, are used for the primary
and secondary barriers, the joining processes shall also be tested as described
above.
- Guidance on the use of non-metallic materials in the
construction of primary and secondary barriers is provided in Pt 11, Ch 21 Appendix 1 Non-Metallic Materials.
- Consideration may be given to the use of materials in the primary and
secondary barrier, which are not resistant to fire and flame spread, provided
they are protected by a suitable system such as a permanent inert gas
environment, or are provided with a fire retardant barrier.
5.1.4
Thermal insulation and other materials used in cargo containment systems
- Load-bearing thermal insulation and other materials used in cargo containment
systems shall be suitable for the design loads.
- Thermal insulation and other materials used in
cargo containment systems shall have the following properties, as applicable,
to ensure that they are adequate for the intended service:
- compatibility with the cargoes;
- solubility in the cargo;
- absorption of the cargo;
- shrinkage;
- ageing;
- closed cell content;
- density;
- mechanical properties, to the extent that they are
subjected to cargo and other loading effects, thermal expansion and
contraction;
- abrasion;
- cohesion;
- thermal conductivity;
- resistance to vibrations;
- resistance to fire and flame spread;
- resistance to fatigue failure and crack propagation.
- In addition to the requirements given in Pt 11, Ch 4, 5.1 Materials 5.1.4, fatigue and crack propagation
properties for insulation in membrane systems are also to be submitted.
Insulation materials are to be approved by LR. Where applicable, these
requirements also apply to any adhesive, sealers, vapour barriers, coatings or
similar products used in the insulation system, any material used to give
strength to the insulation system, components used to hold the insulation in
place and any non-metallic membrane materials. Such products are to be
compatible with the insulation.
- The above properties, where applicable, shall be tested for the range between
the expected maximum temperature in service and 5°C below the minimum design
temperature, but not lower than –196°C.
- Due to location or environmental conditions, thermal insulation materials
shall have suitable properties of resistance to fire and flame spread and shall
be adequately protected against penetration of water vapour and mechanical
damage. Where the thermal insulation is located on or above the exposed deck,
and in way of tank cover penetrations, it shall have suitable fire resistance
properties in accordance with a recognised Standard acceptable to LR or be
covered with a material having low flame spread characteristics and forming an
efficient approved vapour seal.
- Thermal insulation that does not meet recognised Standards acceptable to LR
for fire resistance may be used in hold spaces that are not kept permanently
inerted, provided its surfaces are covered with material with low flame spread
characteristics and that forms an efficient approved vapour seal.
- Testing for thermal conductivity of thermal
insulation shall be carried out on suitably aged samples.
- Where powder or granulated thermal insulation
is used, measures shall be taken to reduce compaction in service, for example
due to vibrations, and to maintain the required thermal conductivity and also
prevent any undue increase of pressure on the cargo containment system.
- Particular attention is to be paid to the cleaning of the steelwork prior to
the application of the insulation. Where insulation is to be foamed or sprayed
in situ, the minimum steelwork temperature at the time of application
is to be indicated in the specification in addition to environmental
conditions.
5.2 Construction processes
5.2.1 A construction, testing and inspection (CTI) plan for the installation
of the containment system is to be submitted for approval. This plan is to list the
following sequentially for each stage of installation, testing and
inspection: (a) The method to be used. (b) The
acceptance criteria. (c) The form of record to be made.
(d) The involvement of the shipyard, containment system designer
where relevant, and LR Surveyor. The testing and inspection should be
commensurate with assumptions made in the design of the containment system,
see
Pt 11, Ch 4, 4.3 Design conditions 4.3.3. Further detailed documents, which may be
cross-referenced by the CTI plan, are to be submitted for approval as applicable.
5.2.2 A detailed quality assurance/quality control (QA/QC) programme shall be
applied to ensure the continued conformity of materials in the containment system
during installation and service. The quality assurance/quality control programme
shall include the procedure for fabrication, storage, handling and preventive actions
to guard against exposure of a material to harmful effects. The proposed procedure is
to be submitted to LR for consideration. All materials in the containment system are
also to be considered and included in the procedure. See also Pt 11, Ch 21, 1.5 Quality control and quality assurance (QA/QC).
5.2.3
Weld joint design
- All welded joints of the shells of independent tanks shall be of the in-plane
butt weld full penetration type. For dome-to-shell connections only, tee welds
of the full penetration type may be used depending on the results of the tests
carried out at the approval of the welding procedure. Except for small
penetrations on domes, nozzle welds are also to be designed with full
penetration.
Except for the dome-to-shell connections,
T-butt welds will not be accepted in the shell.
- Welding joint details for Type C independent tanks, and for the liquid-tight
primary barriers of Type B independent tanks primarily constructed of curved
surfaces, shall be as follows:
- All longitudinal and circumferential joints shall be of
butt welded, full penetration, double vee or single vee type. Full
penetration butt welds shall be obtained by double welding or by the use
of backing rings. If used, backing rings shall be removed except from
very small process pressure vessels. Other edge preparations may be
permitted, depending on the results of the tests carried out at the
approval of the welding procedure.
- The bevel preparation of the joints between the tank body
and domes and between domes and relevant fittings shall be designed
according to a standard acceptable to LR. All welds connecting nozzles,
domes or other penetrations of the vessel and all welds connecting
flanges to the vessel or nozzles shall be full penetration welds.
See also
Pt 5, Ch 10, 14 Construction of the Rules for Ships.
- Where applicable, all the construction processes and testing,
except that specified in Pt 11, Ch 4, 5.2 Construction processes 5.2.5 shall be done in accordance with the
applicable provisions of Pt 11, Ch 6 Materials of Construction and Quality Control .
5.2.4
Design for gluing and other joining processes
The design of the joint to be glued (or joined by some other process
except welding) shall take account of the strength characteristics of the joining
process.
5.2.5
Testing during construction
- All cargo tanks and process pressure vessels
shall be subjected to hydrostatic or hydro-pneumatic pressure testing in
accordance with Pt 11, Ch 4, 6.1 Type A independent tanks to Pt 11, Ch 4, 6.6 Semi-membrane tanks, as applicable for the tank type.
- All tanks shall be subject to a tightness test which may be
performed in combination with the pressure test referred to in Pt 11, Ch 4, 5.2 Construction processes 5.2.5.
- Requirements with respect to inspection of secondary barriers shall be decided
by LR in each case, taking into account the accessibility of the barrier.
See also
4.6.2.
- The Administration may require that, for ship units fitted with
novel Type B independent tanks or tanks designed according to Pt 11, Ch 4, 8 Cargo containment systems of novel configuration, at least one prototype tank and its
supporting structures shall be instrumented with strain gauges or other
suitable equipment to confirm stress levels. Similar instrumentation may be
required for Type C independent tanks, depending on their configuration and on
the arrangement of their supports and attachments.
- The overall performance of the cargo containment system shall be verified for
compliance with the design parameters during entry into service in accordance
with the survey procedure. Records of the performance of the components and
equipment, essential to verify the design parameters, shall be maintained and
be available to the Administration.
- The overall performance of the cargo containment system is to be verified for
compliance with the design parameters during initial acceptance cargo trials.
The initial trials are to be witnessed by LR’s Surveyors, and are to
demonstrate that the system is capable of being inerted, cooled, loaded and
discharged in a satisfactory manner, and that all safety devices function
correctly.
The temperature at which these tests are carried out
is to be at or near the minimum cargo temperature. Where a refrigeration
plant is fitted, its operation is to be demonstrated to the Surveyors.
Records of the plant performance taken during entry into service at minimum
temperature are to be submitted. Logs of plant performance are to be
maintained for examination by the Surveyors when requested.
- Heating arrangements, if fitted in accordance with Pt 11, Ch 4, 5.1 Materials 5.1.2 and Pt 11, Ch 4, 5.1 Materials 5.1.2 , shall be tested for required heat
output and heat distribution.
- The cargo containment system shall be inspected for cold spots during or
immediately following entry into service. Inspection of the integrity of
thermal insulation surfaces that can not be visually checked shall be carried
out in accordance with recognised Standards.
- Repair Procedures shall define imperfection and defects and their
allowable limits, identification of failure type and subsequent repair
processes.
Repairs shall be of a quality standard as defined
in Pt 11, Ch 4, 5.2 Construction processes.
Records of the
performance of the repaired components and equipment, essential to verify
the design parameters, shall be maintained and be available.
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