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The MCA have published MIN 25 on the Failure of Engine Low Pressure Fuel Systems. This investigation was in response to the frequent failures and consequent fires on-board due to fuel leakage, often from low pressure rather than high pressure fuel lines.
The
main cause of engine room fires for many years is the ignition of oil on hot
surfaces escaping from pressurised lines.
In
order to reduce this risk;
1. All
hot surfaces should be protected. Although this should be easily carried out,
repetitive maintenance on machinery can often reduce the quality of the fit of
the protective devices, or shields used.
2. Pressurised
oil lines should be encased. It is difficult to protect all lines, as that
would mean all transfer lines would need protecting which is uneconomical.
However an outer protective sheath should cover vulnerable lines that are
exposed to vibration, and are close to the hot surfaces. In fact it is Class
regulations that ALL fuel injection lines are protected in this way for UMS
operated ships.
Although
the Class or Flag requirements do not state that an alarm system has to be
fitted, it is a prudent option, as if a fuel injection line fails, the quantity
injected into the cylinder will fall, and there will be an imbalance of
cylinder developed powers. Various methods have been used to indicate failure
of the main fuel line:
A. Detection
of the pressure between the fuel line and the outer sheath. This pressure
should obviously be zero when no leakage occurs. A pressure sensor is fitted to
monitor this pressure, and when it rises the alarm system will either lift the
fuel pump concerned, or activate the leakage alarm. There is a small vent on
this void space to prevent any small leakage at the connections or joints
falsely activated this alarm. Note that the sheath can not accept high
pressures, so that a vent valve is often fitted which will prevent the sheath
pressure rising above 1 bar. This method was fitted to many MAN B&W GF
series engines.
B. Monitoring
the quantity of liquid leaking from the void space between the sheaths. Under
normal conditions no leakage occurs, but should a fault exist then the leak off
fluid is collected in a small tank. Once the quantity of liquid exceeds a
pre-determined limit, an alarm will be sounded via the activation of a float
switch. To prevent this alarm occurring due to a build-up of liquid, rather
than a definite leak, there is often a small leak-off hole fitted to the tank.
This system is shown on the diagram overleaf.
C. Monitoring of the cylinder exhaust
temperatures will also indicate when a fuel line has failed, although this is
not this system's primary function. It may occur that even though a fuel line
has partially failed, the sensitivity of the exhaust temperature monitor may
not be sufficient to provide an alarm.
The MCA have published MIN 25 on the Failure of Engine Low Pressure Fuel Systems. This investigation was in response to the frequent failures and consequent fires on-board due to fuel leakage, often from low pressure rather than high pressure fuel lines.
The
main contributing factors of this leakage was the effects of high pressure
pulses (up to 60-80 bar) caused by the spill operation at the end of the fuel
injection, coupled with the effects of frequent dismantling and re-assembly for
maintenance.
Some
of the recommendations are listed:
·
More stringent controls on the
installation, inspection and maintenance of low pressure fuel systems
·
ISM assessors should consider whether
the ship’s SMS should contain procedures to identify possible causes of pipe
failure, and protection of hot surfaces
·
Pipe work supports and retaining
devices to be checked every 6 months
·
Flexible pipes to be closely examined,
and care taken when tightening to avoid twisting. Recommends that these pipes
are pressure tested every five years or even renewed.
·
Engine builders to limit the pressure
pulses to under 16 bar. Only pressure
accumulators fitted to the fuel pump have proved effective in limiting the
pressure pulses.
·
All copper and aluminium-brass piping
should be heat treated to reduce work hardening effects
·
Spray and defector plates to be
correctly fitted after dis-assembly
·
Change in pipe design to eliminate
compression fittings and copper/brass pipework
·
Remote isolation valves should be
fitted in the event of fuel leakage as suggested in M Notice 1456
·
Knowledge of the fuel systems and the
problems of pressure pulses should be included in the training and examination
of Engineering Officers.
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