Master Air Starting Valve Explored written by: Ricky • edited by: Lamar Stonecypher • updated: 7/11/2009 Let us find out what is the function of the air starting valve in the starting air line of a ship.
Introduction We have learnt how compressed air is air is used for various purposes on board ships ships,, and its use in solving starting problems related to main and auxiliary engines. We have seen the full layout of the compressed air starting system. system. Now it is time to take an individual look at the various components of this system and we will study the master air starting valve of a marine engine in this article.
Master Air Admittance Valve If you remember the air starting system from our previous article, you will notice that a main valve is fitted at the entrance to the main air starting line from the air bottles. This valve has to fulfill the following functions
To supply pressurized air from the bottles to the engine cylinder via individual cylinder valves
To ensure that once the engine has started it cuts off the air supply
To ensure that no products of combustion pass over to the bottle side
The last point is very important since once the engine starts firing, the cylinders are full of hot gases and if these gases find their way across to the main air storage tanks or bottles, the result could be anybody’s guess. It could cause a huge explosion and could lead to damage of life and property and might endanger the ship or start an engine room fire. fire.
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In order to ensure this sort of safety, a non-return valve is incorporated inside the starting air valve so that there is only one way passage for the air from the bottle to the engine cylinders but not the other way round. This is all explained in the next section in more detail.
Construction & Working The construction of the master air starting stop valve is shown clearly in the diagram below which shows the cut section of the valve and all the internal parts and passages are clearly shown and legibly marked for the benefit of the readers.
The inlet and outlet for the starting air are shown in the diagram as well as the drain and the control air path. It must be understood that there is a difference between the control air and the starting air. The starting air actually goes inside the
cylinders and makes the engine start, while the control air is used to control the timing of the main starting air and cutting it off at an appropriate time. The arrangement consists of a spring loaded non-return valve which is used for safety purpose and to prevent blow back of the gases to the engine aided with the flame trap which is also provided there. There is also an arrangement to operate this valve manually in case it does not open or close automatically due to some problem. Now suppose the control air line suddenly gets faulty so the starting air pressure could keep the valve open, but because of the stop valve it gets shut when blow back gases try to escape to the other side. It is important to note that the main starting air line is kept in vented position when not in use. This is important to prevent any build up of pressure due and also to remove any condensate in the line which could cause knocking in the line when the compressed air at high pressure whizzes past it. Next to the starting air master valve are the individual cylinder valves which deal with different cylinders, as well shall see in our next article.
Preferential trip
The non-essential circuits or loads on ships are air conditioning, exhaust and ventilation fans, and galley equipments which can be disconnected momentarily and can be connected again after fault finding. The main advantage of preferential trip is that it helps in preventing the operation of main circuit breaker trip and loss of power on essential services and thus prevents blackout and overloading of generator. Construction and Working The preferential trip circuit consists of an electromagnetic coil and a dashpot arrangement to provide some delay to disconnect the non-essential circuits. Along with this, there is also an alarm system provided, which functions as soon as an overload is detected and trips start operating. There are some mechanical linkages also in the circuit which instantaneously operates the circuit and completes the circuit for preferential trips. The dashpot arrangement consists of a small piston with a small orifice and which is placed inside a small cylinder assembly. This piston moves up against the fluid silicon and the time delay is governed by the orifice in the piston. Working of Preferential Trip
The current passes through the electromagnetic coil and the linkages are kept from contacting using a spring arrangement. As soon as the current value increases the limit, the electromagnetic coil pulls the linkage up against the spring force and operates the instantaneous circuit and the alarm system. The lower linkage completes the circuit for the preferential trip circuit. The current passes through the coil in the preferential trip circuit which pulls the piston in the dashpot arrangement. The movement of this piston is governed by the diameter of the orifice and the time delay made by the same. The preferential trip operates at 5, 10 and 15 seconds and the load is removed accordingly. If the overload still persists, then an audible and visual alarm is sounded. The preferential trip is one of those important electrical circuit diagrams which help in removing the excessive load from the main bus bar, thus preventing situation like blackout which is a dangerous incident to ship, especially when the ship is sailing in restricted or congested waters.
What is Lambda Control in Ships? MARCH 25, 2011 BY ANISH1 COMMENT
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With new stringent regulations against pollution being introduced, it is important for the manufacturers to build marine engine that satisfy these norms and do not hamper the normal operation of the engine. To achieve this, engines are provided with several automation systems, which not only reduce the pollution level but also increase the efficiency of the engine and reduce other operational cost. One such introduced automation is lambda control which controls the fuel injection system of themarine engine according to the variation in the load on the same. Purpose of Lambda Controller The main function of any engine is to supply enough power so that it can handle the load put on it. The load may increase or reduce during the operation and to accompany this, some excess fuel may be given to keep up the performance. Lambda controller is used to control the excess fuel injection in the combustion chamber of a marine engine when there is a change in the engine load i.e. during a momentary increase in the engine load. This is done by controlling the two main elements which are responsible for combustion- fuel and air. This controller senses the relation between the charge air pressure and fuel index of the engine at that load. Principle of Working The working of Lambda controller can be understood with the help of the following diagram:
When there is a sudden momentary increase in the engine load, the lambda control will regulate the fuel through injection pump using the regulator arm. For this, (1) is turned on which in-turn commands the switch (2) to touch the Piston arm (3) and be pushed downward, where in the electric circuit will be closed. Hence, solenoid valve (4) will open which will then actuate the jet system to accelerate the turbocharger resulting in increase in charged air pressure. This will result in pressing the piston (3) back in the lambda cylinder (5). When the lambda value or lambda ratio is satisfactory, then the solenoid valve will get closed, deactivating the jet system. When the system is activated for more than 10 seconds, then the solenoid valve is signaled to shut off and there is an alarm for system failure Fuel oil limiting during start During the start procedure, the lambda controller is used as an index limiter. Hereby heavy smoke formation is prevented during start procedure and the regulating device cannot over-react. Advantages
It reduces the emission of excess visible smoke when there is a sudden increase in engine load.
The overall load efficiency of engine increases.
The exhaust side of the engine .i.e. exhaust valve, exhaust gas way, exhaust uptake etc are less fouled due to carbon deposits.
The maintenance work reduces due to less fouling of parts.
"Normal" lifting of the relief valve can occur in the following situation, and should give no cause for concern;
When too much fuel is supplied by the engineer when on starting the engine; I have done this a few times!
If air is being used to stop engine in “emergency stop” situation.
Running engine full astern for a prolonged period, in this case the bridge should be informed that astern running is at its limit.
However, there are situations that could lead to a relief valve lifting while engine is operating under normal load and conditions and warrant a full inspection.
Faulty fuel pump or incorrectly set fuel injector delivering excessive fuel.
Badly leaking fuel injector; through loose nozzle or enlarged injection holes.
Water leaking into the combustion chamber.
Scavenge fire.
Slow turning
A slow turning valve is fitted. This will open instead of the main automatic valve if the engine has been stopped for more than 30 minutes during manoeuvering. It will only supply enough air to turn the engine over very slowly; This is a precaution in case a cylinder has had oil or water leak into it which would cause damage to the engine when starting. If the engine completes a full revolution on the slow turn, then the main automatic valve opens and the engine will start. (note: The operating system for the slow turning has been omitted for simplicity).
Boiler Starting Failure – Troubleshooting NOVEMBER 12, 2010 BY ANISH1 COMMENT
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Failure in boiler starting is a common phenomenon on ship. There can be several reasons for the failure in staring of a boiler. In this article we will learn about the most common reasons for not starting of boiler. 1)
Fuel inlet valve to the burner is in close position:
The fuel line for boiler’s burner consists of several valves located at fuel tank, pumps
suction, discharge valve, or valve before the boiler burner. Any of these can be in closed position resulting in starvation of fuel. 2) Line filter at the inlet of the fuel line for burner is choked: If the system runs in heavy oil then there are chances of filters in the line getting choke. To avoid this, boiler system are normally built for changeover from diesel to heavy oil during starting and heavy to diesel during stopping. This keeps the filter and the fuel line clean.
3)
Boiler fuel supply pump is not running:
There are two main reasons for fuel pump not running. Normally when the pumps are in pairs, the change over auto system is kept in manual position, and if the operating pump trips, the stand by pump will not start automatically. Another reason is tripping of pump due to short circuit in the system etc. 4)
Solenoid valve in the fuel supply line is malfunctioning
Nowadays most of the system adopts advance automation, but their can be a possibility wherein the solenoid in the fuel supply line is malfunctioning and not opening. 5)
Flame eye is malfunctioning:
A Flame eye is a photocell operated flame sensor fitted directly on the refractory to detect weather the burner is firing or not. If the flame eye unit is malfunctioning, then it will give a trip signal even before the burner starts firing. 6)
Air or Steam ratio setting is not proper
For proper and efficient combustion, air fuel ration is very important, if the supply of air is excess then there will be excess of smoke, and if it exceeds more than normal level the combustion will burn off causing flame failure. 7)
Forced draft fan flaps malfunctioning
For removing excess gases trapped inside the combustion chamber forced draft fan (FDF) are used for pre purging and post purging operation and are connected with a timer to shut the fan flaps. If the flaps are malfunctioning then continuous forced air will go inside the chamber, preventing the burner to produce flame causing flame failure of the boiler. 8) Any contactor switch inside Control panel is malfunctioning Boiler control panel consist of several contactors and PLC cards. Even one contactor malfunctioning may result in trouble for boiler starting. 9)
Trip not reset
If any previous trips like low water level, flame failure, emergency stop etc. has not been reset than boiler will not start. 10) Main Burner atomiser is clogged Main burners consist of atomizer for efficient burning of fuel. If the atomizer is clogged by sludge and fuel deposits then burner may not produce flame and trip the boiler..
11) Pilot Burner nozzle is choked : A Pilot burner nozzle is very small and can be blocked by carbon deposits and sludge resulting in flame failure. Some pilot burner consists of small filter which can be clogged after continuous operation resulting in flame failure because of carbon accumulation. 12) Electrodes are not generating spark Initial spark for generating a flame is produced by electrode which may be due to carbon deposits on them or fault in the circuit of electrodes etc.
The fuel pump cam on the MAN B&W MC series engine is designed to raise the plunger on the injection stroke and then keep the plunger at the top of its stroke while the follower stays on the peak of the cam until just before the next delivery stroke when the follower returns to the base circle of the cam, and the fuel pump plunger moves down on its suction stroke. The animation on the left shows the cam follower just beginning to move up the slope of the cam with the camshaft rotating in anticlockwise direction. (i.e. start of injection) If the engine direction is reversed at this point, then air will enter the pneumatic cylinder as shown and will move the piston to the right. The cam follower will be moved across and would finish in the position shown which would be at the correct fuel pump timing for running astern. It should be noted that the reversal of the follower only takes place while the engine is rotating. If the engine had been stopped from running ahead, and then started astern, the fuel pump followers would move across as the engine starts to rotate, and before the fuel is admitted by venting the fuel pump puncture valves. A micro switch shown on the LHS detects whether the follower has moved across. If not, an indicator light is lit in the control room, However the engine will still start if a
follower fails to move, perhaps due to corrosion in the servo cylinder. A high exhaust temperature deviation alarm would operate within a short time. Allowing the engine to start in this situation could be useful during manoeuvring in confined waters .
The video clip opposite shows a cam follower moving from astern to
ahead on a MAN B&W MC engine.
Indicator Lights for Camsha
Reversing Servomotor on MAN B&W 2 Stroke Engine
On a two stroke engine, the fuel pumps must be retimed when the engine is required to reverse direction (i.e. run astern). This is done by moving the fuel pump cams or fuel pump cam follower positions relative to the crankshaft.
If one cylinder of the engine is considered (left), the piston is just before TDC with the engine running ahead and the crankshaft rotating clockwise. The piston is moving up towards TDC. The picture on the right shows the fuel cam at this point; where the cam follower is rising up the lift of the cam as it rotates clockwise. This point can be considered as the start of injection.
The fuel pump cam foll up the rise of the cam stroke. The cam is corre the engin
If, at this point the engine is stopped, and is started in the reverse direction (astern), the crankshaft now moves in an anticlockwise direction. Then the piston in this particular unit is now moving down the cylinder and is just after TDC. At this point fuel injection should have just finished. However, by studying the picture of the cam (right) it can be seen that the camshaft has reversed direction (because it is directly driven from the crankshaft), and is also rotating anticlockwise. In the picture the follower is moving down the cam which means the fuel pump plunger is just finishing the suction stroke; i.e completely out of time with the engine.
Here the fuel pump ca position. When the pis TDC, fuel delivery shou and the follower should the peak of th
So that the Fuel Pump cam is timed correctly with the crankshaft when the engine is reversed, the fuel pump cams are rotated by a hydraulic servomotor which changes the position of the cams relative to the crankshaft. The angle through which the cams are turned is known as the Lost Motion angle. Although this can be made to happen when the engine is still rotating, it is probably easier to think of the engine stopped as shown left and the camshaft moving as shown on the animation below. Once the fuel cams have moved, the engine can then start running in the reverse direction (anticlockwise).
The angle that the cams the lost motion
Because the engine is started using compressed air admitted through the air start valves, the operating mechanism for these must also be retimed. More details on the operation of the reversing servomotor as used on the Sulzer RTA engine can be found in themembers section
This is not the only method of reversing a two stroke engine. Other methods include moving the whole camshaft axially so that a different set of cams are used, and a rather clever method used by MAN-B&W which alters the position of the cam followers.