Section
2 Piping Design Requirements
2.1 Application
2.1.3 Piping systems are to be so designed that protuberances are faired to
reduce the possibility of damage, for example, when alongside support craft or
during work operations.
2.1.4 Where necessary external pipes may be protected against corrosion by
suitable bonding or coatings.
2.1.5 Piping systems should be so designed as to minimize the noise inside the
diving bell and surface compression chamber during normal operation.
2.1.6 Piping systems which could be subjected to higher pressures than their
design pressure are to be fitted with a pressure relief valve.
2.1.7 Piping systems carrying mixed gas or oxygen under high pressure are not
to pass through accommodation spaces, engine rooms or similar compartments.
2.1.8 High pressure gas systems are to be reduced in pressure as close as
possible to the gas storage.
2.1.9 All pipes penetrating pressure chambers including diving bells are to be
provided with internal and external isolating values. These valves are to have
positive means of indication to show whether they are open or shut and are to be
capable of being secured in either position. The securing arrangements are to be
such that the valves can be operated in an emergency. Where appropriate, one valve
should be of the non-return type. Where it is not practicable to fit isolating
valves direct to the shell, distance pieces of short rigid construction may be
fitted between the valves and shell plating. The number of screwed fittings, if
employed for this purpose, should be kept to a minimum.
2.1.10 Any components fitted between the shell penetrations and isolating valves
are to be designed for an internal and external pressure of not less than that
equivalent to the maximum diving depth.
2.1.11 All high pressure piping should be well protected against mechanical
damage.
2.1.12 All piping is to be approved metallic construction suitable for the
service intended, except where flexibility is essential in which case flexible hoses
of approved type having integral closely woven wire braid reinforcement with
properly attached end fittings of swaged crimped or similar type are acceptable as
short joining lengths between permanent piping.
2.1.15 All valves, fittings, controls, indicators and warning devices are to be
provided with identification plates made of a material which is at least flame
retardant. The identifying marks are to be clear and unmistakable (e.g. stating the
short designation and/or the function of the item concerned).
2.1.16 Means must be provided for the complete evacuation, drainage and venting
of piping systems.
2.1.17 Compression chambers and diving bells are to have suction guards on
exhaust line openings inside each compartment.
2.1.18 Gas lines and electrical cables are to be routed separately.
2.1.19 Expansion in piping systems is to be compensated by pipe bends or
compensators. Attention is to be given to the suitable sizing of fixed points.
2.1.20 Materials used in the breathing gas system shall not produce noxious,
toxic or flammable products under specified design conditions.
2.1.21 In oxygen pressure systems, all the materials in contact with this gas
shall be shock tested according to EN 738-1, -2 and - 3:1997/1998 “Pressure
regulators for use with medical gases” or equivalent standard applicable to the
particular component. (See also EN 849:1996, EN ISO 11114-3:1997 and EN ISO
2503:1998 in informative references)
2.1.22 For piping systems of copper, corrosion resistant alloys and austenitic
steels with chromium-nickel content above 22%, the test can be waived.
2.1.23 Precautions shall be taken to avoid galvanic corrosion.
2.1.24 Non-metallic materials retaining pressurised gas shall be considered for
gas-permeability.
2.2 Pipe connections
2.2.2 Wherever possible, pipes should be joined by full penetration butt welds.
2.2.3 Flanged connections and flange bolts conforming to a recognized standard
may be used.
2.2.4 Other types of connections may be submitted for consideration.
2.2.5 Screwed pipe connections are to be of an LR approved type.
2.3 Pipe fittings
2.3.1 All surface compression chambers and diving bells are to be equipped at a
centralized position outside the chamber with such valves, gauges and other fittings
as necessary to control and indicate the internal pressure and safe environment of
each compartment. The external pressure on the diving bell is also to be indicated
inside the bell.
2.3.2 Valves in oxygen systems where the system pressure is above the exemption
pressure as defined in IGC13/12/E, are to be screw down type and slow opening except
that ball valves may be used as emergency shut-off valves fitted directly to the
shell.
2.3.3 Gas valves, including pressure-reducing valves and their systems, are to
be tested to 1,5 times design pressure. It is to be demonstrated that they are
capable of delivering the specified quantity of gas at a pressure equivalent to the
intended maximum diving depth.
2.3.4 All valves are to be constructed as to prevent the possibility of valve
covers or glands being loosened when the valves are operated.
2.3.5 All valves are to be clearly labelled and provided with open/shut
indication.
2.3.6 Shutoff devices must conform to a recognized standard. Valves with
screw-down bonnets or spindles are to be protected against unintentional unscrewing
of the bonnet.
2.3.7 Manually operated shutoff devices are to be closed by turning in the
clockwise direction.
2.3.8 Hose fittings are to be made of corrosion resistant material and are to
be so designed that they cannot be disconnected accidentally.
2.4 Hose lines and umbilicals
2.4.1 Except for umbilicals, non-metallic hoses are to be reduced to a minimum
and are only to be installed in short lengths.
2.4.2 Hose lines, including their connectors, must be of proven suitability for
the media, pressures and temperatures concerned. When selecting the material,
special attention is to be paid to toxicity, incombustibility, gas permeability, and
where applicable, compatibility with oxygen. Only types approved by LR may be
used.
2.4.3 Hose lines for liquids/gases are to be designed for a bursting pressure
equivalent to at least 4 and 5 times respectively the maximum permissible working
pressure, see
Pt 5, Ch 5, 4.6 Resistance to burst.
2.4.4 Hoses are to be permanently coupled to their connectors.
2.4.5 Systems with hose lines are to be fitted with a device for relieving the
pressure before the hoses are disconnected.
2.4.6 Unless equipped with load cables, umbilical hose lines must be fitted
with load relieving devices.
2.4.7 Umbilicals must be protected against abrasion and damage. Where
protective sheathing is used, care is to be taken to ensure that minor leaks cannot
lead to an internal pressure build-up. Metal inserts are to be avoided.
2.5 Safety Relief Valves
2.5.1 Equipment and piping systems which may be subjected to pressures higher
than the design pressure must be fitted with overpressure protection.
2.5.2 All compression chambers and diving bells shall be provided with pressure
relief valves or overpressure alarms. Where pressure relief valves are proposed
these may be fitted on the chamber or bell or, alternatively on each gas
pressurizing line. Where relief valves are fitted on a chamber a quick operating
manual shut-off valve should be installed between the chamber and the pressure
relief valve which should be wired open with a frangible wire. This valve should be
readily accessible to the diving supervisor monitoring the operation of the
chamber.
2.5.3 Heat exchangers and heaters in life support system are to be protected by
suitably sized safety relief devices set at a pressure not exceeding their maximum
allowable working pressure (MAWP) and they are to be installed with no intervening
valves between the pressure container and the safety relief device with the
exception of PVO's. The maximum allowable working pressure is the maximum pressure
permissible at the top of the pressure vessel, heat exchanger or heater in its
normal operating condition and at the designated concurrent temperature specified
for that pressure. If the safety devices are mounted outside the main pressure hull,
they are to be constructed of suitable non-corrosive materials and are to be
inspected on a regular basis in accordance with the procedure outlined in the
approved Maintenance Manual. For these safety devices, the designer is to consider
the effect of seawater back-pressure acting on the downstream side of the safety
device.
2.5.4 If the safety devices are mounted on equipment or piping within PVHO,
then it is to be demonstrated by calculations that the release of the fluid
contained in the pressure vessel will not increase the pressure within the main
pressure hull by more than 1 atmosphere, nor raise the partial pressure of the
atmospheric gases above their maximum allowable levels. Special consideration will
be given to the equivalent alternative arrangements.
2.6 Ballast systems
2.6.1 Ballast systems should be designed to operate under all specified angles
of heel and trim including maximum anticipated damage conditions.
2.6.2 In an autonomous or free-swimming submersible where pumps are required
for the transfer or discharge of ballast a stand-by pump should be provided.
2.6.3 On passenger submersibles, pumps are to be provided which are capable of
quickly transferring ballast and altering trim according to the number of passengers
embarked on each trip.
2.6.4 Internal ballast or trim systems which may be subjected to the dive
pressure should be suitable for the maximum design diving depth and are to be tested
to 1,5 times this pressure.
2.6.5 Ballast control and tank flow valves are to be of a failsafe design or,
alternatively provided with stand-by facilities.
2.6.6 Where compressed air is used to discharge ballast or to trim tanks the
capacity should be sufficient to discharge all the tanks at the maximum diving depth
with a reserve of 50 per cent. On passenger submersibles the reserve should be 100
per cent.
2.6.7 The compressed air storage vessels should not be used for other purposes
and should be fully charged before the start of each dive.
2.6.8 In a passenger submersible two separate means of enabling the craft to return to the
surface should be provided and for keeping the surfaced craft in a stable
condition.
2.6.9 Sufficient instrumentation and equipment should be provided to ensure that the
operator is fully aware of the ballast, heel and trim conditions at all times.
2.6.10 Water leakage monitoring devices should be provided in all compartments with audible
and visual alarms at the control station. Monitoring devices for battery
compartments should be suitable for use in such spaces.
2.7 Bilge systems
2.7.1 Autonomous submersibles should be provided with
an efficient bilge system capable of pumping out all
watertight compartments except those containing
water ballast, fuel oil, etc., under all practicable
conditions of list and trim.
2.7.2 Autonomous submersibles are to be provided with
at least two self-priming pumps capable of draining
all compartments. Where appropriate, one pump may be
driven off propulsion shafting.
2.7.3 The arrangement of valves, cocks and their
connections is to be such as to prevent the
possibility of one watertight compartment being
placed in communication with another. For this
reason screw down non-return valves are to be
provided at bilge pump manifold and branch bilge
suctions.
2.7.4 Where bilge pipes pass through watertight
bulkheads, screw down non-return valves attached to
the bulkheads capable of being closed from both
sides are to be provided.
2.7.5 In addition a mud box and screw down non-return
valve should be provided within the space the bilge
suction serves.
2.7.6 Bilge systems which may be subjected to the dive
pressure should be suitable for the maximum design
diving depth and are to be tested to 1,5 times this
pressure.
2.8 Drainage of chambers
2.8.1 Where drainage of pressure chambers is achieved by means of pressure
differential, a self-closing shut-off valve is to be provided inside the chamber
close to the chamber penetration.
2.9 Compressed air systems
2.9.1 Air storage pressure vessels are to be designed and manufactured to a
relevant National Standard.
2.9.2 Where compressed air is used for essential ballasting movements, not less
than two means of supplying the compressed air are to be provided. Alternatively
where the craft is designed for trips of short duration (for example less than 6
hours) consideration could be given to recharging the storage vessels from shore.
2.9.3 Each compressor stage must be equipped with a pressure relief valve or
rupture disc, neither of which can be disabled. This safety device must be designed
and set in such a way that the specified pressure in the compressor stage concerned
cannot be exceeded by more than 10 per cent. The setting must be safeguarded against
unauthorized alteration.
2.9.4 Each compressor stage must be provided with a suitable pressure gauge
indicating clearly the final pressure of that stage.
2.9.5 Where a compressor stage comprises more than one cylinder and each
cylinder can be closed off individually, a pressure relief valve and a pressure
gauge must be provided for each cylinder.
2.9.6 Cooling liquid systems with a shutoff device must be so designed that the
specified coolant pressure cannot be exceeded.
2.9.7 Dry-running reciprocating compressors must be equipped at each stage with
a device which activates a warning signal and shuts down the drive motor if the
final compression temperature stated in the operating instructions is exceeded.
2.9.8 Diaphragm-type compressors must be equipped at each stage with a
diaphragm rupture indicator which shuts down the compressor as soon as damage occurs
to the drive or compressor diaphragm
2.10 Hydraulic equipment
2.10.1 Fluids having low flash points and fluids having high viscosity at low
temperatures are not to be used. Fire-resistant non-toxic fluids are
recommended.
2.10.2 Materials used for all parts of hydraulic seals are to be compatible with
the working fluid at the appropriate working temperature and pressure.
2.10.3 Pumps are to be accessible for maintenance and are to be mounted where
they will be protected from damage and dirt.
2.10.4 Overpressure protection is to be provided on the discharge side of all
pumps. Where relief valves are fitted for this purpose they are to be fitted in
close circuit, i.e. arranged to discharge back to the suction side of the pump.
2.10.5 System piping is not to be used as a means of supporting equipment.
2.10.6 Provision is to be made for operation of the equipment in the event of
loss of pressure in the system.
2.10.7 Hydraulic piping is to be located clear of oxygen or oxygen enriched
systems.
2.11 Wall Thickness of Pipes and Tubes Subjected to External Pressure
2.11.1 The minimum thickness of piping subject to external pressure is to be the
greater of the thickness determined by the following equations:
Where:
W |
= |
External Pressure |
T |
= |
Thickness |
E |
= |
Modulus of Elasticity |
R |
= |
Mean Radius |
Ro |
= |
Outside Radius |
v |
= |
Poisson’s Ratio |
Qy |
= |
Yield Strength |
C |
= |
0.00 for plain-end pipe or tubing |
= |
1.27 mm (0.05 in.) for all threaded pipe 17mm (3/8 in.) O.D. and
smaller |
= |
depth of thread h for all threaded pipe over 17 mm (3/8 in.) O.D. |
= |
depth of groove for grooved pipe |
2.12 Testing
2.12.1 On completion of manufacture but before insulation or painting, all
piping systems are to undergo a hydraulic pressure test at 1,5 times the design
pressure.
2.12.2 The gas storage facilities, diving system and life support systems
including the gas piping are to be subjected to a tightness test at the maximum
permissible working pressure using Nitrogen with 10% He to facilitate locating
possible leaks. The maximum permissible leakage rate is represented by a 1 per cent
pressure drop in 24 hours for the entire compression chamber system taking into
account any temperature change. Please also see
Pt 5, Ch 4, 6.3 Oxygen System Testing and Pt 5, Ch 4, 6.4 Gas leak test for all chambers and breathing gas systems respectively.
2.12.3 Wherever possible, all butt welds in LSS piping systems are to be
subjected to 100 per cent NDT for class I piping systems.
2.12.4 Piping systems for breathing gas and oxygen are to be subjected to a
purity test.
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