16.1 General
16.1.1 The manufacture, testing, inspection and documentation shall be
in accordance with recognized standards and the regulations given in this Code.
LR 16.1-01 The manufacture, testing, inspection and certification
are to be in accordance with the requirements of the Rules for the Manufacture,
Testing and Certification of Materials (hereinafter referred to as the Rules
for Materials).
16.1.2 Where post-weld heat treatment is specified or required, the properties of the
base material shall be determined in the heat treated condition, in accordance with
the applicable tables of chapter 7, and the weld properties shall be determined in
the heat treated condition in accordance with 16.3. In cases where a post-weld heat
treatment is applied, the test regulations may be modified at the discretion of the
Administration.
LR 16.1-02 A relaxation in the requirements for Charpy V-notch
impact tests will be permitted for smaller fuel tanks or process pressure vessels
which are post-weld heat treated. The extent of this relaxation will be specially
considered for each application and will depend on the grade of steel and thickness
involved.
16.2 General test regulations and
specifications
16.2.1 Tensile test
16.2.1.1 Tensile testing shall be carried out in accordance with
recognized standards.
16.2.1.2 Tensile strength, yield stress and elongation shall be to the
satisfaction of the Administration. For carbon-manganese steel and other materials
with definitive yield points, consideration shall be given to the limitation of the
yield to tensile ratio.
LR 16.2-01 The grades of materials used are to generally have
mechanical properties complying with the appropriate requirements as given in the
Rules for Materials. Provided that the material has satisfactory ductility, there
will be no limitation on the yield to tensile stress ratio, except for
carbon–manganese steel grades for low temperature service. For carbon–manganese
steel grades for low temperature service, the yield to tensile ratio requirement of
Ch 3, 6 Ferritic steels for low temperature service of the
Rules for the Manufacture, Testing and Certification of
Materials is to be met.
16.2.2 Toughness test
16.2.2.1 Acceptance tests for metallic materials shall include Charpy V-notch
toughness tests unless otherwise specified by the Administration. The specified
Charpy V-notch regulations are minimum average energy values for three full size (10
mm × 10 mm) specimens and minimum single energy values for individual specimens.
Dimensions and tolerances of Charpy V-notch specimens shall be in accordance with
recognized standards. The testing and regulations for specimens smaller than 5.0 mm
in size shall be in accordance with recognized standards. Minimum average values for
sub-sized specimens shall be:
| Charpy V-notch specimen size (mm)
|
Minimum average energy of three
specimens
|
| 10 x 10
|
KV
|
| 10 x 7.5
|
5/6 KV
|
| 10 x 5.0
|
2/3 KV
|
- where:
- KV = the energy values (J) specified in tables 7.1 to 7.4.
Only one individual value may be below the specified average value, provided it is
not less than 70% of that value.
16.2.2.2 For base metal, the largest size Charpy V-notch specimens possible for the
material thickness shall be machined with the specimens located as near as
practicable to a point midway between the surface and the centre of the thickness
and the length of the notch perpendicular to the surface as shown in figure
16.1.
Figure 16.1 – Orientation of base metal test specimen
16.2.2.3 For a weld test specimen, the largest size Charpy V-notch specimens possible
for the material thickness shall be machined, with the specimens located as near as
practicable to a point midway between the surface and the centre of the thickness.
In all cases the distance from the surface of the material to the edge of the
specimen shall be approximately 1 mm or greater. In addition, for double-V butt
welds, specimens shall be machined closer to the surface of the second welded
section. The specimens shall be taken generally at each of the following locations,
as shown in figure 16.2, on the centreline of the welds, the fusion line and 1 mm, 3
mm and 5 mm from the fusion line.
Figure 16.2 – Orientation of weld test specimen
Notch locations in figure 16.2:
- .1 centreline of the weld;
- .2 on fusion line;
- .3 in heat-affected zone (HAZ), 1 mm from fusion line;
- .4 in HAZ, 3 mm from fusion line; and
- .5 in HAZ, 5 mm from fusion line.
16.2.2.4 If the average value of the three initial Charpy V-notch specimens fails to
meet the stated regulations, or the value for more than one specimen is below the
required average value, or when the value for one specimen is below the minimum
value permitted for a single specimen, three additional specimens from the same
material may be tested and the results combined with those previously obtained to
form a new average. If this new average complies with the regulations and if no more
than two individual results are lower, than the required average and no more than
one result is lower than the required value for a single specimen, the piece or
batch may be accepted.
16.2.3 Bend test
16.2.3.1 The bend test may be omitted as a material acceptance test, but
is required for weld tests. Where a bend test is performed, this shall be done in
accordance with recognized standards.
LR 16.2-03 Bend tests are to be taken only when such tests are
required in the Rules for Materials.
16.2.3.2 The bend tests shall be transverse bend tests, which may be
face, root or side bends at the discretion of the Administration. However,
longitudinal bend tests may be required in lieu of transverse bend tests in cases
where the base material and weld metal have different strength levels.
16.2.4 Section observation and other testing
Macrosection, microsection observations and hardness tests may also be
required by the Administration, and they shall be carried out in accordance with
recognized standards, where required.
LR 16.2-04 These tests are to be carried out when required by the
Rules for Materials and when required according to the scope of approval of the fuel
containment system.
16.3 Welding of metallic materials
and non-destructive testing for the fuel containment system
LR 16.3-01 Unless otherwise specified below, all welded
construction is to be in accordance with Chapter 13 of the Rules for Materials.
LR 16.3-02 Unless otherwise specified in these Rules, welding
procedure tests are to be performed in accordance with the requirements of Chapter 12 of the Rules for Materials. Generally, impact
tests from aluminium welded joint are not required. For austenitic stainless steel
welded joint, impact tests are not required from the heat affected zone.
16.3.1 General
This section shall apply to primary and secondary barriers only,
including the inner hull where this forms the secondary barrier. Acceptance testing
is specified for carbon, carbon-manganese, nickel alloy and stainless steels, but
these tests may be adapted for other materials. At the discretion of the
Administration, impact testing of stainless steel and aluminium alloy weldments may
be omitted and other tests may be specially required for any material.
16.3.2 Welding consumables
Consumables intended for welding of fuel tanks shall be in accordance
with recognized standards. Deposited weld metal tests and butt weld tests shall be
required for all consumables. The results obtained from tensile and Charpy V-notch
impact tests shall be in accordance with recognized standards. The chemical
composition of the deposited weld metal shall be recorded for information.
LR 16.3-03 Welding consumables are to be approved by LR in
accordance with Chapter 11 of the Rules for Materials.
16.3.3 Welding procedure tests for fuel tanks and process pressure
vessels
16.3.3.1 Welding procedure tests for fuel tanks and process pressure
vessels are required for all butt welds.
16.3.3.2 The test assemblies shall be representative of:
16.3.3.3 For butt welds in plates, the test assemblies shall be so
prepared that the rolling direction is parallel to the direction of welding. The
range of thickness qualified by each welding procedure test shall be in accordance
with recognized standards. Radiographic or ultrasonic testing may be performed at
the option of the fabricator.
LR 16.3-04 Welding procedure tests are to be performed in
accordance with the requirements of Chapter 12 of the Rules for Materials, except where
indicated otherwise in these Rules. Mechanical tests for butt welds are to be in
accordance with 16.3.3.4.
16.3.3.4 The following welding procedure tests for fuel tanks and
process pressure vessels shall be done in accordance with 16.2 with specimens made
from each test assembly:
-
.1 cross-weld tensile tests;
-
.2 longitudinal all-weld testing where required by the recognized standards;
-
.3 transverse bend tests, which may be face, root or side bends. However,
longitudinal bend tests may be required in lieu of transverse bend tests in
cases where the base material and weld metal have different strength levels;
-
.4 one set of three Charpy V-notch impacts, generally at each of the
following locations, as shown in figure 16.2:
-
.1 centreline of the welds;
-
.2 fusion line;
-
.3 1 mm from the fusion line;
-
.4 3 mm from the fusion line; and
-
.5 5 mm from the fusion line;
- .5 macrosection, microsection and hardness survey may also be
required.
LR 16.3-05 Additionally, an all-weld metal tensile test is
required from welding procedure tests for Type C independent fuel tanks. A
macrosection and hardness survey is required for all welding procedure tests, except
that the hardness survey is not required for austenitic stainless steel. Generally,
microsections are not required.
LR 16.3-06 For alloys where the weld metal has a lower tensile
strength than that of the parent metal, and such an application has prior approval
by LR, the transverse weld tensile strength is not to be less than the specified
design tensile strength.
16.3.3.5 Each test shall satisfy the following:
-
.1 tensile tests: cross-weld tensile strength is not to be less than the
specified minimum tensile strength for the appropriate parent materials. For
aluminium alloys, reference shall be made to 6.4.12.1.1.3 with regard to the
regulations for weld metal strength of under-matched welds (where the weld
metal has a lower tensile strength than the parent metal). In every case,
the position of fracture shall be recorded for information;
-
.2 bend tests: no fracture is acceptable after a 180° bend over a former of a
diameter four times the thickness of the test pieces; and
-
.3 Charpy V-notch impact tests: Charpy V-notch tests shall be conducted at
the temperature prescribed for the base material being joined. The results
of weld metal impact tests, minimum average energy (KV), shall be no less
than 27 J. The weld metal regulations for sub-size specimens and single
energy values shall be in accordance with 16.2.2. The results of fusion line
and heat affected zone impact tests shall show a minimum average energy (KV)
in accordance with the transverse or longitudinal regulations of the base
material, whichever is applicable, and for sub-size specimens, the minimum
average energy (KV) shall be in accordance with 16.2.2. If the material
thickness does not permit machining either full-size or standard sub-size
specimens, the testing procedure and acceptance standards shall be in
accordance with recognized standards.
LR 16.3-07 For aluminium alloys, the bend test required in
16.3.3.4.3 is to be carried out over a former with D/t according to Ch 12,4 of the Rules for Materials.
LR 16.3-08 Bend tests revealing small openings up to a maximum of
3 mm in any direction are acceptable.
16.3.3.6 Procedure tests for fillet welding shall be in accordance with
recognized standards. In such cases, consumables shall be so selected that exhibit
satisfactory impact properties.
LR 16.3-09
Ch 12 of the Rules for Materials is to be followed for
procedure tests for fillet welding, and LR approved welding consumables are to be
used.
16.3.4 Welding procedure tests for piping
Welding procedure tests for piping shall be carried out and shall be
similar to those detailed for fuel tanks in 16.3.3.
16.3.5 Production weld tests
16.3.5.1 For all fuel tanks and process pressure vessels except membrane
tanks, production weld tests shall generally be performed for approximately each 50
m of butt-weld joints and shall be representative of each welding position. For
secondary barriers, the same type production tests as required for primary tanks
shall be performed, except that the number of tests may be reduced subject to
agreement with the Administration. Tests, other than those specified in 16.3.5.2 to
16.3.5.5 may be required for fuel tanks or secondary barriers.
16.3.5.2 The production tests for types A and B independent tanks shall
include bend tests and, where required for procedure tests, one set of three Charpy
V-notch tests. The tests shall be made for each 50 m of weld. The Charpy V-notch
tests shall be made with specimens having the notch alternately located in the
centre of the weld and in the heat affected zone (most critical location based on
procedure qualification results). For austenitic stainless steel, all notches shall
be in the centre of the weld.
LR 16.3-10 The production weld tests shall satisfy the applicable
requirements of 16.3.3.5.
16.3.5.3 For type C independent tanks and process pressure vessels,
transverse weld tensile tests are required in addition to the tests listed in
16.3.5.2. Tensile tests shall meet regulation 16.3.3.5.
LR 16.3-11 In addition, an all-weld metal tensile test for Type C
independent fuel tanks and Class 1 and Class 2/1 process pressure vessels is
required.
LR 16.3-12 In addition, a macrosection examination and hardness
survey are required according to Ch 13,4.8 of the Rules for Materials.
16.3.5.4 The quality assurance/quality control (QA/QC) program shall
ensure the continued conformity of the production welds as defined in the material
manufacturers quality manual (QM).
16.3.5.5 The test regulations for membrane tanks are the same as the
applicable test regulations listed in 16.3.3.
LR 16.3-13 Requirements for production tests from membrane tanks
are to be agreed with LR prior to manufacture.
LR 16.3-14 Unless otherwise stated below, all welds are to be
subject to non-destructive examination in accordance with the requirements of Chapter 13 of the Rules for Materials.
16.3.6 Non-destructive testing
16.3.6.1 All test procedures and acceptance standards shall be in
accordance with recognized standards, unless the designer specifies a higher
standard in order to meet design assumptions. Radiographic testing shall be used in
principle to detect internal defects. However, an approved ultrasonic test procedure
in lieu of radiographic testing may be conducted, but in addition supplementary
radiographic testing at selected locations shall be carried out to verify the
results. Radiographic and ultrasonic testing records shall be retained.
16.3.6.2 For type A independent tanks where the design temperature is
below -20°C, and for type B independent tanks, regardless of temperature, all full
penetration butt welds of the shell plating of fuel tanks shall be subjected to
non-destructive testing suitable to detect internal defects over their full length.
Ultrasonic testing in lieu of radiographic testing may be carried out under the same
conditions as described in 16.3.6.1.
16.3.6.3 In each case the remaining tank structure, including the welding
of stiffeners and other fittings and attachments, shall be examined by magnetic
particle or dye penetrant methods as considered necessary.
16.3.6.4 For type C independent tanks, the extent of non-destructive
testing shall be total or partial according to recognized standards, but the
controls to be carried out shall not be less than the following:
LR 16.3-15 Non-destructive testing is to meet the requirements of
Ch 13,4 of the Rules for Materials for Class 1
pressure vessels.
16.3.6.5 The quality assurance/quality control (QA/QC) program shall ensure the
continued conformity of the non-destructive testing of welds, as defined in the
material manufacturer's quality manual (QM).
16.3.6.6 Inspection of piping shall be carried out in accordance with the regulations
of chapter 7.
16.3.6.7 The secondary barrier shall be non-destructive tested for internal defects
as considered necessary. Where the outer shell of the hull is part of the secondary
barrier, all sheer strake butts and the intersections of all butts and seams in the
side shell shall be tested by radiographic testing.
16.4 Other regulations for
construction in metallic materials
16.4.1 General
Inspection and non-destructive testing of welds shall be in accordance
with regulations in 16.3.5 and 16.3.6. Where higher standards or tolerances are
assumed in the design, they shall also be satisfied.
16.4.2 Independent tank
For type C tanks and type B tanks primarily constructed of bodies of
revolution the tolerances relating to manufacture, such as out-of-roundness, local
deviations from the true form, welded joints alignment and tapering of plates having
different thicknesses, shall comply with recognized standards. The tolerances shall
also be related to the buckling analysis referred to in 6.4.15.2.3.1 and
6.4.15.3.3.2.
LR 16.4-01 For Type C independent tanks, manufacture and
workmanship are to satisfy the requirements of Ch 13,4 of the Rules for Materials for Class 1 pressure
vessels.
LR 16.4-02 For Type C tanks of carbon and carbon-manganese steel
with plate thickness up to 40 mm, post-weld heat treatment shall be performed after
welding, if the design temperature is equal to or less than −10°C.
For Type C independent tanks with plate thickness up to 40 mm, if the
design temperature is higher than −10°C, and for any other carbon and
carbon-manganese tanks, the post-weld heat treatment is to conform to the
requirements of Ch 13, 4.10 Post-weld heat treatment in the Rules for the Manufacture, Testing and Certification of Materials.
For Type C tanks of carbon and carbon-manganese steel with plate thickness greater
than 40 mm and up to 50 mm, post-weld heat treatment shall be performed after
welding. Any proposal for exemption of post-weld heat treatment is to be based on an
alternative approach as approved by LR (e.g. Engineering Critical Assessment in
accordance with BS7910 or an equivalent standard). Mechanical stress relieving as
permitted under Ch 6, 6.6 Other requirements for construction in metallic
materials 6.6.2.3 is not applicable for Type C tanks of carbon and
carbon-manganese steel with plate thickness greater than 40 mm and up to 50 mm.
The requirements of Ch 13, 1.16 Post-weld heat treatment and Ch 13, 4.11 Basic requirements for post-weld heat treatment of
fusion welded pressure vessels in the Rules for the Manufacture, Testing and Certification of Materials are to
be followed for the method and technique of post-weld heat treatment.
16.4.3 Secondary barriers
During construction the regulations for testing and inspection of secondary barriers
shall be approved or accepted by the Administration (see also 6.4.4.5 and 6.4.4.6).
16.4.4 Membrane tanks
The quality assurance/quality control (QA/QC) program shall ensure the continued
conformity of the weld procedure qualification, design details, materials,
construction, inspection and production testing of components. These standards and
procedures shall be developed during the prototype testing programme.
16.5 Testing
16.5.1 Testing and inspections during construction
16.5.1.1 All liquefied gas fuel tanks and process pressure vessels shall
be subjected to hydrostatic or hydro-pneumatic pressure testing in accordance with
16.5.2 to 16.5.5, as applicable for the tank type.
16.5.1.2 All tanks shall be subject to a tightness test which may be
performed in combination with the pressure test referred to in 16.5.1.1.
16.5.1.3 The gas tightness of the fuel containment system with reference
to 6.3.3 shall be tested.
16.5.1.4 Regulations with respect to inspection of secondary barriers
shall be decided by the Administration in each case, taking into account the
accessibility of the barrier (see also 6.4.4).
16.5.1.5 The Administration may require that for ships fitted with novel
type B independent tanks, or tanks designed according to 6.4.16 at least one
prototype tank and its support shall be instrumented with strain gauges or other
suitable equipment to confirm stress levels during the testing required in 16.5.1.1.
Similar instrumentation may be required for type C independent tanks, depending on
their configuration and on the arrangement of their supports and attachments.
16.5.1.6 The overall performance of the fuel containment system shall be
verified for compliance with the design parameters during the first LNG bunkering,
when steady thermal conditions of the liquefied gas fuel are reached, in accordance
with the requirements of the Administration. Records of the performance of the
components and equipment, essential to verify the design parameters, shall be
maintained on board and be available to the Administration.
LR 16.5-01 The overall performance of the fuel containment system
is to be verified for compliance with the design parameters during initial 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 and bunkered 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 fuel temperature.
LR 16.5-02 Where refrigeration plant is fitted, or other means to
control the fuel tank(s) vapour pressure, its operation is to be demonstrated to the
Surveyors. Records of the plant performance taken during the first bunkered voyage
at minimum temperature are to be submitted. The above tests may be carried out in
conjunction with the vessel’s normal trading commitments. Normal voyage logs of
plant performance are to be maintained for examination by the Surveyors when
requested.
16.5.1.7 The fuel containment system shall be inspected for cold spots
during or immediately following the first LNG bunkering, when steady thermal
conditions are reached. Inspection of the integrity of thermal insulation surfaces
that cannot be visually checked shall be carried out in accordance with the
requirements of the Administration.
16.5.1.8 Heating arrangements, if fitted in accordance with 6.4.13.1.1.3
and 6.4.13.1.1.4, shall be tested for required heat output and heat
distribution.
16.5.2 Type A independent tanks
All type A independent tanks shall be subjected to a hydrostatic or
hydro-pneumatic pressure testing. This test shall be performed such that the
stresses approximate, as far as practicable, the design stresses, and that the
pressure at the top of the tank corresponds at least to the MARVS. When a
hydropneumatic test is performed, the conditions shall simulate, as far as
practicable, the design loading of the tank and of its support structure including
dynamic components, while avoiding stress levels that could cause permanent
deformation.
LR 16.5-03 If a hydropneumatic or a hydrostatic test is utilised, the test
head of water and air pressure are to be specified by designers. Details and
procedures of the hydropneumatic or hydrostatic test are to be submitted for
approval.
LR 16.5-04 The scantlings of the tanks are to comply with LR 6.4-38,using
equivalent internal pressure for the test condition.
LR 16.5-05 The primary structures of the tanks are to comply with Ch 2, 4.7
Tank test condition of the ShipRight Structural Design Assessment
Procedure for Type A Tank Liquefied Gas Carriers and Ch 2, 4.7 Tank test
condition of the ShipRight Structural Design Assessment Primary Hull and
Cargo Tank Structure of Liquefied Gas Carriers Fitted with Type B Independent
Tanks Primarily Constructed of Plane Surfaces for type A tanks and type B
primarily constructed of plane surfaces tanks respectively. The designer may propose
an alternative equivalent procedure subject to agreement with LR.
16.5.3 Type B independent tanks
Type B independent tanks shall be subjected to a hydrostatic or
hydro-pneumatic pressure testing as follows:
-
.1 The test shall be performed as required in 16.5.2 for type A independent
tanks.
-
.2 In addition, the maximum primary membrane stress or maximum bending stress
in primary members under test conditions shall not exceed 90% of the yield
strength of the material (as fabricated) at the test temperature. To ensure
that this condition is satisfied, when calculations indicate that this
stress exceeds 75% of the yield strength the test of the first of a series
of identical tanks shall be monitored by the use of strain gauges or other
suitable equipment.
16.5.4 Type C independent tanks and other pressure vessels
16.5.4.1 Each pressure vessel shall be subjected to a hydrostatic test
at a pressure measured at the top of the tanks, of not less than 1.5 P0.
In no case during the pressure test shall the calculated primary membrane stress at
any point exceed 90% of the yield strength of the material at the test temperature.
To ensure that this condition is satisfied where calculations indicate that this
stress will exceed 0.75 times the yield strength, the test of the first of a series
of identical tanks shall be monitored by the use of strain gauges or other suitable
equipment in pressure vessels other than simple cylindrical and spherical pressure
vessels.
16.5.4.2 The temperature of the water used for the test shall be at
least 30°C above the nil-ductility transition temperature of the material, as
fabricated.
16.5.4.3 The pressure shall be held for 2 hours per 25 mm of thickness,
but in no case less than 2 hours.
16.5.4.4 Where necessary for liquefied gas fuel pressure vessels, a
hydro-pneumatic test may be carried out under the conditions prescribed in 16.5.4.1
to 16.5.4.3.
LR 16.5-06 When a hydropneumatic test is performed, the
conditions are to simulate, so far as practicable, the actual loading of the tank
and its supports.
16.5.4.5 Special consideration may be given to the testing of tanks in which higher
allowable stresses are used, depending on service temperature. However, regulation
in 16.5.4.1 shall be fully complied with.
16.5.4.6 After completion and assembly, each pressure vessel and its related fittings
shall be subjected to an adequate tightness test, which may be performed in
combination with the pressure testing referred to in 16.5.4.1 or 16.5.4.4 as
applicable.
16.5.4.7 Pneumatic testing of pressure vessels other than liquefied gas fuel tanks
shall be considered on an individual case basis. Such testing shall only be
permitted for those vessels designed or supported such that they cannot be safely
filled with water, or for those vessels that cannot be dried and are to be used in a
service where traces of the testing medium cannot be tolerated.
16.5.5 Membrane tanks
16.5.5.1 Design development testing
16.5.5.1.1 The design development testing required in 6.4.15.4.1.2 shall include a
series of analytical and physical models of both the primary and secondary barriers,
including corners and joints, tested to verify that they will withstand the expected
combined strains due to static, dynamic and thermal loads at all filling levels.
This will culminate in the construction of a prototype scaled model of the complete
liquefied gas fuel containment system. Testing conditions considered in the
analytical and physical model shall represent the most extreme service conditions
the liquefied gas fuel containment system will be likely to encounter over its life.
Proposed acceptance criteria for periodic testing of secondary barriers required in
6.4.4 may be based on the results of testing carried out on the prototype scaled
model.
16.5.5.1.2 The fatigue performance of the membrane materials and representative
welded or bonded joints in the membranes shall be determined by tests. The ultimate
strength and fatigue performance of arrangements for securing the thermal insulation
system to the hull structure shall be determined by analyses or tests.
16.5.5.2 Testing
-
.1 In ships fitted with membrane liquefied gas fuel containment systems, all
tanks and other spaces that may normally contain liquid and are adjacent to
the hull structure supporting the membrane, shall be hydrostatically tested.
-
.2 All hold structures supporting the membrane shall be tested for tightness
before installation of the liquefied gas fuel containment system.
-
.3 Pipe tunnels and other compartments that do not normally contain liquid
need not be hydrostatically tested.
16.6 Welding, post-weld heat
treatment and non-destructive testing
16.6.1 General
Welding shall be carried out in accordance with 16.3.
16.6.2 Post-weld heat treatment
Post-weld heat treatment shall be required for all butt welds of pipes
made with carbon, carbon-manganese and low alloy steels. The Administration may
waive the regulations for thermal stress relieving of pipes with wall thickness less
than 10 mm in relation to the design temperature and pressure of the piping system
concerned.
LR 16.6-01 Post-weld heat treatment is required for all butt welds
in pipes carrying natural gas contaminated with hydrogen sulphide which are
constructed in steel with a minimum tensile strength exceeding 410 N/mm2.
LR 16.6-02 Unless otherwise stated below, all welds are to be
subject to non-destructive examination in accordance with the requirements of Ch 13 of the Rules for Materials.
16.6.3 Non-destructive testing
In addition to normal controls before and during the welding, and to the visual
inspection of the finished welds, as necessary for proving that the welding has been
carried out correctly and according to the regulations in this paragraph, the
following tests shall be required:
-
.1 100% radiographic or ultrasonic inspection of butt-welded joints for
piping systems with;
- .1 design temperatures colder than minus 10°C; or
- .2 design pressure greater than 1.0 MPa; or
- .3 gas supply pipes in ESD protected machinery spaces; or
- .4 inside diameters of more than 75 mm; or
- .5 wall thicknesses greater than 10 mm.
-
.2 When such butt welded joints of piping sections are made by automatic
welding procedures approved by the Administration, then a progressive
reduction in the extent of radiographic or ultrasonic inspection can be
agreed, but in no case to less than 10% of each joint. If defects are
revealed the extent of examination shall be increased to 100% and shall
include inspection of previously accepted welds. This approval can only be
granted if well-documented quality assurance procedures and records are
available to assess the ability of the manufacturer to produce satisfactory
welds consistently.
-
.3 The radiographic or ultrasonic inspection regulation may be reduced to 10%
for butt-welded joints in the outer pipe of double-walled fuel piping.
-
.4 For other butt-welded joints of pipes not covered by 16.6.3.1 and
16.6.3.3, spot radiographic or ultrasonic inspection or other
non-destructive tests shall be carried out depending upon service, position
and materials. In general, at least 10% of butt-welded joints of pipes shall
be subjected to radiographic or ultrasonic inspection.
LR 16.6-03 Non-destructive testing is to meet the requirements of
Ch 13,5 of the Rules for Materials for
pressure piping.
16.7 Testing regulations
16.7.1 Type testing of piping components
Valves
Each type of piping component intended to be used at a working
temperature below minus 55°C shall be subject to the following type tests:
-
.1 Each size and type of valve shall be subjected to seat tightness testing
over the full range of operating pressures and temperatures, at intervals,
up to the rated design pressure of the valve. Allowable leakage rates shall
be to the requirements of the Administration During the testing satisfactory
operation of the valve shall be verified.
-
.2 The flow or capacity shall be certified to a recognized standard for each
size and type of valve.
-
.3 Pressurized components shall be pressure tested to at least 1.5 times the
design pressure.
-
.4 For emergency shutdown valves, with materials having melting temperatures
lower than 925°C, the type testing shall include a fire test to a standard
at least equivalent to those acceptable to the Organization.footnote
16.7.2 Expansion bellows
The following type tests shall be performed on each type of expansion
bellows intended for use on fuel piping outside the fuel tank as found acceptable in
7.3.6.4.3.1. and .3 and where required by the Administration, on those installed
within the fuel tanks:
-
.1 Elements of the bellows, not pre-compressed, but axially restrained shall
be pressure tested at not less than five times the design pressure without
bursting. The duration of the test shall not be less than five minutes.
-
.2 A pressure test shall be performed on a type expansion joint, complete
with all the accessories such as flanges, stays and articulations, at the
minimum design temperature and twice the design pressure at the extreme
displacement conditions recommended by the manufacturer without permanent
deformation.
-
.3 A cyclic test (thermal movements) shall be performed on a complete
expansion joint, which shall withstand at least as many cycles under the
conditions of pressure, temperature, axial movement, rotational movement and
transverse movement as it will encounter in actual service. Testing at
ambient temperature is permitted when this testing is at least as severe as
testing at the service temperature.
-
.4 A cyclic fatigue test (ship deformation, ship accelerations and pipe
vibrations) shall be performed on a complete expansion joint, without
internal pressure, by simulating the bellows movement corresponding to a
compensated pipe length, for at least 2,000,000 cycles at a frequency not
higher than 5 Hz. This test is only required when, due to the piping
arrangement, ship deformation loads are actually experienced.
16.7.3 System testing regulations
16.7.3.1 The regulations for testing in this section apply to fuel
piping inside and outside the fuel tanks. However, relaxation from these regulations
for piping inside fuel tanks and open ended piping may be accepted by the
Administration.
16.7.3.2 After assembly, all fuel piping shall be subjected to a strength
test with a suitable fluid. The test pressure shall be at least 1.5 times the design
pressure for liquid lines and 1.5 times the maximum system working pressure for
vapour lines. When piping systems or parts of systems are completely manufactured
and equipped with all fittings, the test may be conducted prior to installation on
board the ship. Joints welded on board shall be tested to at least 1.5 times the
design pressure.
16.7.3.3 After assembly on board, the fuel piping system shall be
subjected to a leak test using air, or other suitable medium to a pressure depending
on the leak detection method applied.
16.7.3.4 In double wall fuel piping systems the outer pipe or duct shall
also be pressure tested to show that it can withstand the expected maximum pressure
at pipe rupture.
LR 16.7-03 The pressure test required by 16.7.3.4 is to be
carried out after assembly on board. Where this is not feasible, then consideration
will be given to pressure testing of individual piping or ductwork prior to
installation providing calculations verifying the design pressure of the ducting is
submitted and the piping is satisfactorily leak tested after completion of
installation.
16.7.3.5 All piping systems, including valves, fittings and associated
equipment for handling fuel or vapours, shall be tested under normal operating
conditions not later than at the first bunkering operation, in accordance with the
requirements of the Administration.
LR 16.7-04 For gas fuel system with pressure no greater than 1
MPa, the gas fuel piping in the machinery space is to be tested in place by
hydraulic pressure to 0,7 MPa or twice the working pressure, whichever is the
greater. Subsequently, the lines are to be tested by air at the working pressure
using soapy water, or equivalent, to verify that all joints are absolutely tight.
LR 16.7-05 For gas fuel systems with pressure greater than 1 MPa,
all gas fuel piping shall be subjected to a strength test with a suitable fluid. The
test pressure shall be at least 1,5 times the design pressure for liquid lines and
1,5 times the maximum system working pressure for vapour lines. When piping systems
or parts of systems are completely manufactured and equipped with all fittings, the
test may be conducted prior to installation on board the ship. Joints welded on
board shall be tested to at least 1,5 times the design pressure.
LR 16.7-06 After assembly on board, the fuel piping system shall
be subjected to a leak test using air, or another suitable medium to a pressure
depending on the leak detection method applied.
16.7.3.6 Emergency shutdown valves in liquefied gas piping systems shall close fully
and smoothly within 30 s of actuation. Information about the closure time of the
valves and their operating characteristics shall be available on board, and the
closing time shall be verifiable and repeatable.
16.7.3.7 The closing time of the valve referred to in 8.5.8 and 15.4.2.2 (i.e. time
from shutdown signal initiation to complete valve closure) shall not be greater
than:
- where:
- U = ullage volume at operating signal level (m3);
- BR = maximum bunkering rate agreed between ship and shore facility
(m3/h); or
- 5 seconds, whichever is the least.
The bunkering rate shall be adjusted to limit surge pressure on valve closure to an
acceptable level, taking into account the bunkering hose or arm, the ship and the
shore piping systems, where relevant.