Engine Structure and Power Transmission Systems Flashcards

1
Q

what is the purpose of the thruster
(bow and stern)?

A

The purpose of the thruster units is to turn the vessel when is operating at slow speeds or when is not under way, to keep the ship in position in a cross wind and to move the ship towards or away from a mooring position as required. The thrust is produced by rotation of a propeller unit which is housed in a transverse cylindrical ducting, where the propeller unit is rotated by means of a vertical electric motor via bevel gears. The propeller blade pitch is controllable in order to obtain the desired magnitude and direction of thrust. Power is transmitted from the electric motor through the flexible coupling, input shaft and bevel gears to the propeller shaft, rotating the propeller in a single direction.

The thruster comprises of a number of separate sections:

The electric motor unit with drive shaft and bevel gearing driving the propeller unit hub;

The propeller unit with blades mounted in the hub;

The hydraulic unit which changes the pitch of the propeller blades;

The control system which regulates the blade pitch in accordance with demand from the bridge.

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1
Q

with reference to bow and stern thrusters

what does the propeller unit consist of?

A

The propeller unit, usually consists of four propeller blades and a propeller hub. The propeller hub and gear case house a hydraulic servomotor and sliding block mechanism. The propeller blades are connected to blade carriers by blade bolts, and this ensures easy exchange of blades in the thruster tunnel. The gear case, which carries the propeller parts, is connected to the thruster tube by bolts and this ensures easy overhauling of all parts inside the thruster tube. The power transmission gear is located inside the gear case and consists of the vertical input shaft, the right angle reduction bevel gear and the horizontal propeller shaft, and serves to transfer the power from the prime mover to the propeller. The bevel gear and individual bearings are lubricated by the gravity oil filling the gear case

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2
Q

with reference to bow and stern thrusters

what does the hydraulic unit do?

A

The hydraulic power pack unit provides oil under pressure and this is used to change the pitch of the thruster unit blades. The oil is drawn from the gravity tank, through the suction filter and into the oil service pump. The pressurized oil is pumped to the solenoid valve via the check valve and the flow of oil is controlled by the solenoid valve.
The hydraulically operated solenoid valve is a changeover valve for the distribution of the hydraulic oil to the respective servo cylinders depending on the command entered at the active control panel. When the command is entered on the control panel, the solenoid valve is actuated and pressurized hydraulic oil is supplied to one of the hydraulic circuits down the oil tube, through the feed ring and oil entry tube to the servomotor, causing displacement of the cross head piston. The reciprocating movement of the piston is converted into a turning movement by the sliding block mechanism and this turns the propeller blades. The vent side of the servomotor piston drains to the oil bath in the thruster body via a solenoid valve. From this pressurized oil bath, oil returns to the header tank. The main actuator power pack pump takes oil from the header tank and supplies it to the thruster unit via the solenoid control valves. A shaft sealing mechanism is attached to the gear case in order to prevent leakage of oil out of the system. When a pitch change command is entered, the propeller will tend to move excessively. The pilot check valve prevents any excessive movement of the propeller whilst changing pitch.

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3
Q

with reference to bow and stern thrusters

how is the bevel gear and all the bearings inside the gear case lubricated?

A

The bevel gear and all the bearings inside the gear case are lubricated by the bath lubricating method. The lubrication oil in the gear case is slightly pressurized by the connection with the gravity tank which is positioned above the waterline to prevent sea water from leaking into the oil system.

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4
Q

with reference to bow and stern thrusters

when is the main motor started?

A

The main motor must only be started when the blades are in the neutral position (zero pitch), or in the allowable zone (blade pitch of ±3°). The system is interlocked to prevent the main motor from starting if the blade pitch is outside of the set limits. The interlock switches also prevent the main motor from starting when:
The cooling fan is stopped;
The power pack gravity tank level is low;
The control oil pressure is low

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5
Q

with reference to bow and stern thrusters

explain the operation of the bow thrusters?

A

Operation of the bow thrusters requires starting a large induction motor and the power requirement of this electric motor is high, requiring that additional generators are started in order to avoid the risk of a vessel blackout. It is important to note that, on modern vessels if there is insufficient power capacity available at the switchboard an additional generator is started by the power management system. The thruster drive motor cannot be started until sufficient power is available at the switchboard. Usually, the main switchboard includes a bow thruster control panel, which includes a control position selection switch, lock-out relay trip reset, motor control and an ammeter. A series of status indicators are also included for monitoring the condition of the VCB, gravity tank, pump pressure etc. If any warning lamp is illuminated, the cause of the fault should be determined and remedied before operation of the bow thruster. Feeder protection for the bow thrusters is achieved by means of the protection and monitoring panel located on the main switchboard bow thruster panel and offers both measurement and protection for the bow thruster drive motor. To ensure safe, reliable operation of the bow thrusters, limits are imposed on the vessel’s speed and draught. If there is insufficient draught, the thruster will suffer a reduction in performance along with cavitation and the possibility of air drawing. The result of this will be increased vibration which may cause damage. Similarly, at speeds greater than 5 knots there is a risk of drawing air into the thruster, particularly when operating at shallow waters. This will degrade the performance and can cause cavitation damage and it can be detected by hunting of the main motor ammeter and should be avoided. If the vessel’s speed is below 5 knots and air drawing is occurring, reducing the propeller pitch will prevent further air drawing from taking place. Under normal circumstances the main power supply is activated by the engineering department and after that the thruster operation and control is undertaken by the deck department from the bridge panels. The main switch at the local thruster control panel should be set at REMOTE in order to allow for this. Control of the thruster on the bridge is either at the wheelhouse control stand or the control stands on the bridge wings. It is important to note that, especially on bow thruster, when the hydraulic pump is started the fan is also started and the FAN RUN indicator in the panel will be illuminated. The main motor is interlocked with the fan and oil pump and will not start unless they are running. Also is important to remember that there are EMERGENCY STOP push-buttons in the wheelhouse panel, forward mooring station and in the bridge wing panels. The thruster unit includes a feedback system for transmitting the angle of the propeller blades to the remote control panel located on the bridge. As the oil entry varies, the stroke of the oil entry tube also varies. The movement of the oil entry tube causes movement of the feedback lever. This movement is transmitted via the feedback chain to the blade angle transmitter located outside the thruster gear casing. This mechanical movement is then converted to an electrical signal by the blade angle transmitter and transmitted to the angle indicator on the bridge and local control panels.

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6
Q

difference between medium and slow speed diesel engines

A

Medium-speed diesels, e.g. 250 to 750 rev/min, and slow-speed diesels, e.g. 100 to 120 rev/min, each have their various advantages and disadvantages for various duties on board ship. The slow-speed two-stroke cycle diesel is used for main propulsion units since it can be directly coupled to the propeller and shafting. It provides high powers, can burn low-grade fuels and has a high thermal efficiency. The cylinders and crankcase are isolated, which reduces contamination and permits the use of specialised lubricating oils in each area. The use of the two-stroke cycle usually means there are no inlet and exhaust valves. This reduces maintenance and simplifies engine construction. Medium-speed four-stroke engines provide a better power-to-weight ratio and power-to-size ratio and there is also a lower initial cost for equivalent power. The higher speed, however, requires the use of a gearbox and flexible couplings for main propulsion use. Cylinder sizes are smaller, requiring more units and therefore more maintenance, but the increased speed partly offsets this. Cylinder liners are of simple construction since there are no ports, but cylinder heads are more complicated and valve operating gear is required. Scavenging is a positive operation without use of scavenge trunking, thus there can be no scavenge Fires. Better quality fuel is necessary because of the higher engine speed, and lubricating oil consumption is higher than for a slow-speed diesel. Engine height is reduced with trunk piston design and there are fewer moving parts per cylinder. There are, however, in total more parts for maintenance, although they are smaller and more manageable. The Vee engine configuration is used with some medium-speed engine designs to further reduce the size and weight for a particular power.

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7
Q

purpose Couplings, clutches and gearboxes

A

Where the shaft speed of a medium-speed diesel is not suitable for its application, e.g. where a low speed drive for a propeller is required, a gearbox must be provided. Between the engine and gearbox it is usual to fit some form of flexible coupling to dampen out vibrations. Elastic or flexible couplings allow slight misalignment and damp out or remove torque variations from the engine. The coupling may in addition function as a clutch or disconnecting device. Couplings may be mechanical, electrical, hydraulic or pneumatic in operation. It is usual to combine the function of clutch with a coupling and this is not readily possible with the mechanical coupling. There is also often a need for a clutch to disconnect the engine from the gearbox. A clutch is a device to connect or separate a driving unit from the unit it drives. With two engines connected to a gearbox a clutch enables one or both engines to be run, and facilitates reversing of the engine.

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8
Q

with the aid of a sketch describe the operation of a hydraulic coupling?

A

The hydraulic or fluid coupling uses oil to connect the driving section or impeller with the driven section or runner (Figure 2.25). No wear will thus take place between these two, and the clutch operates smoothly. The runner and impeller have pockets that face each other which are filled with oil as they rotate. The engine driven impeller provides kinetic energy to the oil which transmits the drive to the runner. Thrust bearings must be provided on either side of the coupling because of the axial thrust developed by this coupling.

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9
Q

with the aid of a sketch describe the operation of a plate type clutch

A

A plate-type clutch consists of pressure plates and clutch plates arranged in a clutch spider (Figure 2.26). A forward and an aft clutch assembly are provided, and an externally mounted selector valve assembly is the control device which hydraulically engages the desired clutch. The forward clutch assembly is made up of the input shaft and the forward clutch spider. The input shaft includes the forward driven gear and, at its extreme end, a hub with the steel pressure plates of the forward clutch assembly spline-connected, i.e. free to slide. Thus when the input shaft turns, the forward driven gear and the forward clutch pressure plates will rotate. The forward clutch plates are positioned between the pressure plates and are spline-connected to the forward clutch spider or housing. This forward clutch spider forms part of the forward pinion assembly which surrounds but does not touch the input shaft. The construction of the reverse clutch spider is similar. Both the forward and reverse pinions are in constant mesh with the output gear wheel which rotates the output shaft. In the neutral position the engine is rotating the input shaft and both driven gear wheels, but not the output shaft. When the clutch selector valve is moved to the ahead position, a piston assembly moves the clutch plates and pressure plates into contact. A friction grip is created between the smooth pressure plate and the clutch plate linings and the forward pinion rotates. The forward pinion drives the output shaft and forward propulsion will occur. The procedure when the selector valve is moved to the astern position is similar but now the reverse pinion drives the output shaft in the opposite direction.

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10
Q

explain how an engine can be reversed

A

Where a gearbox is used with a diesel engine, reversing gears may be incorporated so that the engine itself is not reversed. Where a controllable pitch propeller is in use there is no requirement to reverse the main engine. However, when it is necessary to run the engine in reverse it must be started in reverse and the fuel injection timing must be changed. Where exhaust timing or poppet valves are used they also must be re-timed. With jerk-type fuel pumps the fuel cams on the camshaft must be repositioned. This can be done by having a separate reversing cam and moving the camshaft axially to bring it into position. Alternatively a lost-motion clutch may be used in conjunction with the ahead pump-timing cam. The shaping of the cam results in a period of pumping first then about 10° of fuel injection before top dead centre and about 5° after top dead centre. A period of dwell then occurs when the fuel pump plunger does not move. A fully reversible cam will be symmetrical about this point, as shown. The angular period between the top dead centre points for ahead and astern running will be the ‘lost motion’ required for astern running. The lost-motion clutch or servo motor uses a rotating vane which is attached to the camshaft but can move in relation to the camshaft drive from the crankshaft. The vane is shown held in the ahead operating position by oil pressure. When oil is supplied under pressure through the drain, the vane will rotate through the lost-motion angular distance to change the fuel timing for astern operation. The starting air system is re-timed, either by this camshaft movement or by a directional air supply being admitted to the starting air distributor, to reposition the cams. Exhaust timing or poppet valves will have their own lost-motion clutch or servo motor for astern timing. Medium- and slow-speed diesel engines will follow a fairly similar procedure for starting and manoeuvring. Where reversing gearboxes or controllable-pitch propellers are used then engine reversing is not necessary. A general procedure is now given for engine operation which details the main points in their correct sequence.

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11
Q

what is the transmission system on a ship?

A

The transmission system on a ship transmits power from the engine to the propeller. It is made up of shafts, bearings, and the propeller itself. The thrust from the propeller is transferred to the ship through the transmission system. The different items in the system include the thrust shaft, one or more intermediate shafts and the tail shaft. These shafts are supported by the thrust block, intermediate bearings and the stern tube bearing. A sealing arrangement is provided at either end of the tail shaft with the propeller and cone completing the arrangement.

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12
Q

explain what a thrust block is?

A

The thrust block transfers the thrust from the propeller to the hull of the ship. It must therefore be solidly constructed and mounted onto a rigid seating or framework to perform its task. It may be an independent unit or an integral part of the main propulsion engine. Both ahead and astern thrusts must be catered for and the construction must be strong enough to withstand normal and shock loads. The casing of the independent thrust block is in two halves which are joined by fitted bolts. The thrust loading is carried by bearing pads which are arranged to pivot or tilt. The pads are mounted in holders or carriers and faced with white metal. In the arrangement shown the thrust pads extend three-quarters of the distance around the collar and transmit all thrust to the lower half of the casing. Other designs employ a complete ring of pads. An oil scraper deflects the oil lifted by the thrust collar and directs it onto the pad stops. From here it cascades over the thrust pads and bearings. The thrust shaft is manufactured with integral flanges for bolting to the engine or gearbox shaft and the intermediate shafting, and a thrust collar for absorbing the thrust. Where the thrust shaft is an integral part of the engine, the casing is usually fabricated in a similar manner to the engine bedplate to which it is bolted. Pressurised lubrication from the engine lubricating oil system is provided and most other details of construction are similar to the independent type of thrust block.

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13
Q

what are shaft bearings?

A

Shaft bearings are of two types, the aftermost tunnel bearing and all others. The aftermost tunnel bearing has a top and bottom bearing shell because it must counteract the propeller mass and take a vertical upward thrust at the forward end of the tail-shaft. The other shaft bearings only support the shaft weight and thus have only lower half bearing shells. The tilting pad is better able to carry high overloads and retain a thick oil lubrication film. Lubrication is from a bath in the lower half of the casing, and an oil thrower ring dips into the oil and carries it round the shaft as it rotates. Cooling of the bearing is by water circulating through a tube cooler in the bottom of the casing.

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14
Q

explain what a stern tube bearing does?

A

The stern tube bearing serves two important purposes. It supports the tail shaft and a considerable proportion of the propeller weight. It also acts as a gland to prevent the entry of sea water to the machinery space. Early arrangements used bearing materials such as lignum vitae (a very dense form of timber) which were lubricated by sea water. Most modern designs use an oil lubrication arrangement for a white metal lined stern tube bearing. Oil is pumped to the bush through external axial grooves and passes through holes on each side into internal axial passages. The oil leaves from the ends of the bush and circulates back to the pump and the cooler. One of two header tanks will provide a back pressure in the system and a period of oil supply in the event of pump failure. A low-level alarm will be fitted to each header tank. Oil pressure in the lubrication system is higher than the static sea water head to ensure that sea water cannot enter the stern tube in the event of seal failure.

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15
Q

explain the purpose of stern tube seals?

A

Special seals are fitted at the outboard and inboard ends of the tail shaft. They are arranged to prevent the entry of sea water and also the loss of lubricating oil from the stern bearing. Older designs, usually associated with sea water lubricated stern bearings, made use of a conventional stuffing box and gland at the after bulkhead. Oil-lubricated stern bearings use either lip or radial face seals or a combination of the two. Lip seals are shaped rings of material with a projecting lip or edge which is held in contact with a shaft to prevent oil leakage or water entry. A number of lip seals are usually fitted depending upon the particular application. Face seals use a pair of mating radial faces to seal against leakage. One face is stationary and the other rotates. The rotating face of the after seal is usually secured to the propeller boss. The stationary face of the forward or inboard seal is the after bulkhead. A spring arrangement forces the stationary and rotating faces together.

16
Q

draw and label all the parts of a solid propeller?

A

The propeller consists of a boss with several blades of helicoidal form attached to it. When rotated it ‘screws’ or thrusts its way through the water by giving momentum to the column of water passing through it. A solid fixed-pitch propeller is shown in Figure 11.5. Although usually described as fixed, the pitch does vary with increasing radius from the boss. The pitch at any point is fixed, however, and for calculation purposes a mean or average value is used. A propeller which turns clockwise when viewed from aft is considered right-handed and most single-screw ships have right-handed propellers.

17
Q

Describe the construction and assembly of a propeller?

A

The propeller is fitted onto a taper on the tail shaft and a key may be inserted between the two: alternatively a key less arrangement may be used. A large nut is fastened and locked in place on the end of the tail shaft: a cone is then bolted over the end of the tail shaft to provide a smooth flow of water from the propeller. One method of key less propeller fitting is the oil injection system. The propeller bore has a series of axial and circumferential grooves machined into it. High-pressure oil is injected between the tapered section of the tail shaft and the propeller. This reduces the friction between the two parts and the propeller is pushed up the shaft taper by a hydraulic jacking ring. Once the propeller is positioned the oil pressure is released and the oil runs back, leaving the shaft and propeller securely fastened together. The Pilgrim Nut is a patented device which provides a predetermined frictional grip between the propeller and its shaft. With this arrangement the engine torque may be transmitted without loading the key, where it is fitted. The Pilgrim Nut is, in effect, a threaded hydraulic jack which is screwed onto the tail shaft. A steel ring receives thrust from a hydraulically pressurised Nitrile rubber tyre. This thrust is applied to the propeller to force it onto the tapered tail shaft. Propeller removal is achieved by reversing the Pilgrim Nut and using a withdrawal plate which is fastened to the propeller boss by studs. When the tyre is pressurised the propeller is drawn off the taper.

18
Q

What is a Controllable-pitch propeller ?

A

A controllable-pitch propeller is made up of a boss with separate blades mounted into it. An internal mechanism enables the blades to be moved simultaneously through an arc to change the pitch angle and therefore the pitch. When a pitch demand signal is received a spool valve is operated which controls the supply of low-pressure oil to the auxiliary servo motor. The auxiliary servo motor moves the sliding thrust block assembly to position the valve rod which extends into the propeller hub. The valve rod admits high-pressure oil into one side or the other of the main servo motor cylinder. The cylinder movement is transferred by a crank pin and ring to the propeller blades. The propeller blades all rotate together until the feedback signal balances the demand signal and the low-pressure oil to the auxiliary servo motor is cut off. To enable emergency control of propeller pitch in the event of loss of power the spool valves can be operated by hand. The oil pumps are shaft driven. The control mechanism, which is usually hydraulic, passes through the tail shaft and operation is usually from the bridge. Varying the pitch will vary the thrust provided, and since a zero pitch position exists the engine shaft may turn continuously. The blades may rotate to provide astern thrust and therefore the engine does not require to be reversed.

19
Q

What is Cavitation?

A

Cavitation, is the forming and bursting of vapour-filled cavities or bubbles, can occur as a result of pressure variations on the back of a propeller blade. The results are a loss of thrust, erosion of the blade surface, vibrations in the after body of the ship and noise. It is usually limited to high-speed heavily loaded propellers and is not a problem under normal operating conditions with a well designed propeller.

20
Q

Describe what maintenance must be carried out on a propeller?

A

When a ship is in dry dock the opportunity should be taken to thoroughly examine the propeller, and any repairs necessary should be carried out by skilled dockyard staff. A careful examination should be made around the blade edges for signs of cracks. Even the smallest of cracks should not be ignored as they act to increase stresses locally and can result in the loss of a blade if the propeller receives a sharp blow. Edge cracks should be welded up with suitable electrodes. Bent blades, particularly at the tips, should receive attention as soon as possible. Except for slight deformation the application of heat will be required. This must be followed by more general heating in order to stress relieve the area around the repair. Surface roughness caused by slight pitting can be lightly ground out and the area polished. More serious damage should be made good by welding and subsequent heat treatment. A temporary repair for deep pits or holes could be done with a suitable resin filler.

21
Q

draw a transmission system?

A

see Sketch pack

22
Q

how many exhaust valves does a four stroke typically have?

A

The arrangement for four-stroke medium-speed diesels is to incorporate two exhaust valves per cylinder

23
Q

with reference to 4 strokes with the aid of a sketch explain what the rotocap is?

A

This simple device when fitted to exhaust valves causes rotation of the valve spindle during valve opening, wear of the valve seat is reduced, seat deposits are loosened, valve operation life is extended. Figure 8.7 shows the Rotocap which operates as follows: an increase in spring force on the valve as it opens flattens the Belleville washer so that it no longer bears on the bearing housing B at A. This removes the frictional holding force between B and C, the spring cover. Further increase in spring force causes the balls to move down the ramps in the retainer imparting as they move a torque which rotates the valve spindle. As the valve closes, and load from the Belleville washer is removed from the balls and they return to the position shown in section D–D.

24
Q

what is load controlled cylinder cooling and what are the advantages?

A

Load-controlled cylinder cooling

In an effort to reduce the danger of local liner corrosion over the whole engine load some manufacturers are employing cooling systems that are load dependant. In such a system, the cooling flow is split into a primary circuit, bypassing the liner, for cylinder head cooling. In the secondary circuit uncooled water from engine outlet is directed to cool the liner. To avoid vapour formation as a result of maintaining higher cooling temperatures the system is pressurised to 4–6 bar.

The advantages claimed for such a system include:

1.Possible savings in cylinder lubrication oil feed rate.
2.Omission of cylinder bore insulation.
3. Reduced cylinder liner corrosion.

25
Q

Some engines may use completely separate systems for oil cooling of pistons and bearing lubrication. what are the advantages of this?

what are the disadvantages of having two separate systems?

A

The advantages gained by this method are as follows:

1.Different oils can be used for lubrication and cooling, a very low viscosity mineral oil would be better suited to cooling than lubrication.

2.Additives can be used in the lubricating oil that would be beneficial to lubrication, for example, oiliness agents, e.p. agents and V.I. improvers, etc.

3.Improved control over piston temperatures.

4.If oil loss occurs, then with separate systems the problem of detection is simplified and in the case of total oil loss in either system, the quality to be replaced would not be as great as for a common system.

5.Contamination of the oil in either system may take place. In the event the problem of cleaning or renewal of the oil is not so great.

  1. Oxidation of lubricating oil in contact with hot piston surfaces leads to rapid reduction in lubrication properties

Disadvantages of having two separate systems are: greater initial cost due to separate storage, additional pipework and pumps. A sealing problem to prevent mixing of the two different oils is created and due to the increased complexity more maintenance would have to be carried out