Turbo-Chargers/Scavenging and Supercharging Flashcards

1
Q

With reference to main engine turbochargers:
a) Explain their function; (2)
b) State two advantage of fitting them; (2)
c) Explain how they are cooled and lubricated. (4)

A

a.) Turbocharger reuses the exhaust gases in order to increase overall efficiency of the engine. Turbocharger converts the waste energy of exhaust gas into useful work by supercharging the combustion process. They make use of and reduce the amount of waste energy from exhaust gas and provide a high pressure air charge for efficient scavenging.

b.) * By utilising a Turbo charger, it allows the injection of a larger amount of fuel for the cylinder size due to the greater density of air created. Therefore, producing more power.

  • This increased power being produced by an engine will experience far less mechanical power loses compared to a larger naturally aspirated engine (an internal combustion engine in which air intake depends solely on atmospheric pressure so has no T/C), and the Specific fuel consumption will be reduced.

c.) t/c cooling

  • Turbo chargers can be cooled by the engines HT jacket water, or a stand-alone cooling water system or air cooled depending on the engine manufacturer.

t/c lubrication

Most turbochargers don’t have a separate dedicated system. lubrication depends on type of turbo charger bearings used. the two types being metal journal type and ball bearing type. The lube oil is supplied from the main engine lube oil system through a gravity tank. the gravity tank connects through to a pipeline connected to the t/c bearing housing via a non-return valve. the gravity is supplied with oil from the main engine lube oil system through an orifice and one line from the tank goes back to the sump tank, thus maintaining the oil level in the gravity tank at all times.

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2
Q

a) Describe, with the aid of a sketch, the operational principle of a main engine exhaust gas turbocharger. (10)

b) State the function of each of the following turbocharger system components:

(i) Suction filters; (2)
(ii) Exhaust grids; (2)
(iii) Charge air cooler. (2)

A

a.) SEE ORAL/IAMI Sketch Pack for drawing

Exhaust gas directed towards turbine blades using the nozzle and kinetic force of exhaust gas rotates the turbine and compressor wheel. these two wheels turn together and the rapid spinning allows the compressor to suck in large amounts of ambient air and compress it. as a result, the air is very dense and has a higher temperature.

air is sucked in through filter and accelerated to a higher velocity and then slow pressurised using diffuser and volute casing.

This air then passes through a charge air cooler where it is cooled and gains a higher density before going to the engine. Once in the engine the compressed air allows the engine to burn more fuel efficiently and therefore making the engine operation better.

b.) i.) ensure that air entering in doesn’t have harmful debris that would then damage the engine components upon entry to the engine

ii.) protection device used for the front of t/c to prevent t/c blades being damaged from debris or small bits of metal by collecting the metal

iii.) reduce the temperature of the compressed air, increase the density and mass of air available within the cylinder for combustion.

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3
Q

a) State two reasons for fitting an exhaust gas turbocharger to an engine.

b) Describe the effect of dirty or restricted:
(i) Air filters;
(ii) Exhaust gas turbine.

c) Outline how the exhaust gas turbine is cleaned.

A

a.) t/c convert waste energy from exhaust gas into useful energy, by reusing this energy they are increasing air intake and the engine overall efficiency. allow larger amount of fuel to be injected into each cylinder because of the greater density of air created and therefore increasing engine power.

b.) i.) it will cause reduced engine power and combustion efficiency and scavenge pressure. debris matter may be able to enter the engine causing damage to engine parts. If basic filtration methods are not maintained or when the intake air quality is very bad, downfall in the turbocharger performance can be expected along with mechanical problems in compressor blades and nozzles. Moreover, if the air contains abrasive particles, it may even damage or break the turbine blades.

ii.) can lead to back pressure surging and excessive turbine vibration or potential sparks, resulting in breakage of turbine blades. If cleaning is not carried out properly, then the supply of air to engine will be reduced, resulting in lack of of air and improper combustion with black smoke.

c.) two methods can be used water washing and dry washing. When dry cleaning, engine should be running at high load as cleaning is more efficient. If water washing method is used engine speed is reduced until exhaust inlet temperature is below 420 degrees. Fresh water must also be slightly hot to avoid thermal stress. Water is injected through a regulating valve connected to exhaust gas turbine side. Both methods are used when engine is running to remove carbon soot and other exhaust by products.

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4
Q

With respect to main propulsion engine, state the immediate action to be taken as an EOOW in the event of the following, stating one reason for each: (4) marks

a) Excessive vibration from turbocharger at full sea speed;

b) Excessive vibration of air start branch pipe to one cylinder during manoeuvring

c) High Main Bearing Temperatures

A

a.) Contact the bridge and chief engineer, request the engine load to be reduced as much as possible until vibration stops. Caused by propeller being crashed into water in rough weather. often “turbocharger surging” could be an imbalance of exhaust pressure. It could be the engine starting to run on water if the exhaust temperature of the first cylinder starts dropping, followed by the other cylinders as the water replaces the fuel in the lines, find out where the water is coming from. If the worst comes to the worst, the rotor needs removing and sending ashore to check the balance if there’s nothing physically wrong with it.

b.) Inform the bridge and C/E, shut off fuel to the affected unit until manoeuvring is complete or if possible stop engine. this could be caused due to turbulence in the pipe due to irregular running of compressor. inspect compressor drain any oil and water moisture form it then inspect safety devices on air starting system.

c.) Contact the bridge and chief engineer, ask the engine loading to be reduced or stopped. Check lubrication oil flows, pressures and temperature.

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5
Q

With reference to large slow speed diesel engines,
a) State four possible factors leading to a scavenge fire. (4)
b) State four indications of a scavenge fire. (4)

A

a.) 1. if the piston rings have been damaged due to perhaps poor maintenance, this then allows hot combustion gases or sparks to blow past between the piston cylinder liner running surface and through the underside of cylinder liner area and to the scavenge space.

  1. large amount of unburnt carbon from combustion process could have accumulated and blocked the under piston scavenge drain. Due to poor maintenance of scavenge space
  2. over injection of fuel oil and poor combustion due to leaking fuel valves or fuel injectors and improper injection timing
  3. Blocked stuffing box drain or Insufficient or excessive cylinder lubrication.

b.) 1. Under piston scavenge space temperature high alarm goes off and or there’s a rise in cylinder exhaust gas temperatures

  1. turbocharger starts repeatedly surging and there is loss of engine power and reduction in rpm which happens because a back pressure is created under the piston space due to fire
  2. discharging of Sparks and black smoke from the scavenge drains cocks and scavenge air box and potentially the funnel due to incomplete combustion
  3. Paint blisters and hotspots on the scavenge drains, which can be seen on scavenge doors due to high temperature increase but occurs only in large fires
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6
Q

State two dangers of allowing a scavenge fire to exist. (4)

A

Scavenge fires can cause a loss in engine power to one engine cylinder unit which then would lead to irregular running. This puts a lot of strain on the rest of the engine cylinder units due to them having to cope with excessive load and causes various engine components to fail for example the piston and piston rod.

Irregular running will also lead to high temperature and then cause distortion in diaphragm which is sealing the scavenge space from the crankcase. if this happens hot combustion gases could possibly escape between any cracks or distortion in diaphragm and enter the crankcase. the high temperature would have also caused oil droplets to evaporate within the crankcase and mix with air so once the oil vapour reaches range of flammability and comes into contact with hot combustion gases then explosion will occur. explosion occurs when air fuel and heat is present.

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7
Q

State four actions to be taken by the EOOW on discovering:
(i) A scavenge fire in one engine unit only; (8)
ii) A scavenge fire in several engine units at the same time. (8)

A

Action taken in case of a scavenge fire depends on the type of the fire, whether its small or large. You can determine by what kind of fire it is because large fire will have signs easily visible like paint discolouration or blisters generated by the heat from the scavenge space inside the main engine. Also, turbocharger surging and large reduction in rpm and loss of engine power

i.) For Small Fire

  1. Inform the bridge, and start to reduce the speed of the engine & reduce it to slow or dead slow when navigationally safe to do so. This will reduce the amount of heat being generated
  2. Cut off the fuel supply to the affected unit by using fuel isolation valves. Cylinder lubrication of the affected unit should be increased to reduce heat.
  3. Coolant flow through jacket and piston should be maintained to reduce heat. Scavenge drains to be shut to prevent flow of spark and smoke in the engine room.
  4. Then, keep clear of the scavenge space relief valves to prevent human injury. Minor fire should in time burn it itself out.

ii.) For Large Fires

  1. Inform the bridge and C/E immediately to stop the engine immediately and reduce heat being generated.
  2. Stop fuel oil booster pump and use fuel isolation valves to cut off fuel supply. Open indicators cock, engage turning gear and turn the engine to prevent engine seizure.
  3. maintain normal engine cooling and lubrication. careful not to increase fire by having too much lubrication circulate through the cylinder. close Scavenge air duct flap valve to cut off air supply.
  4. Extinguishing the fire with a fixed firefighting system this can either be CO2 or steam used to smother the scavenge fire.
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8
Q

a) Explain the procedure to be carried out before the inspection of the scavenge space on a large 2-stroke diesel engine. (8)

b) State four reasons for carrying out a scavenge space inspection. (8)

A

a.) First work permit should be obtained and risk assessment must be carried out. Scavenge space is considered as a enclosed space so you must obtain a enclosed space entry form. This essentially allows you to enter the space and ensures that all entry checks are carried out. Prior to entry the space has to be ventilated for a period of 24 hours in advance. This ventilation can be done by using a portable fan to allow air to enter the space and all the toxic combustion gases and lowers the atmosphere toxicity to an acceptable level for entry as before carrying out this ventilation the oxygen level isn’t survivable. Its possible to use engine auxiliary blowers to ventilate the space. A crew member who is entering scavenge space should wear a atmosphere tester at all times so it can continuously measure the oxygen level and if it falls below 20.9% then alarm will go off to indicate that oxygen is too low and anyone inside should evacuate immediately. Starting air should be isolated by closing main air starting valve to prevent flow of air inside scavenge space as you are going to be entering through scavenge space receiver you cannot have air blowing through whilst your inside cleaning the space or for inspection. Then isolate fuel as well. Engage the turning gear for the main engine and then if possible person who is carrying out inspection after scavenge space cleaning is preformed should have the turning gear controller with them when entering scavenge space that way if an emergency occurs they can stop turning engine immediately also if you have someone outside who is turning the engine they don’t don’t know where the inspector is so an accident could easily occur. Before entry ensure all PPE is worn and before entering you have all equipment you need like hydrometer for checking piston rings, feeler gauge, Vernier calliper and rags. Have someone else outside space to ensure that crew members inside are okay that way they can quickly signal for help in an emergency. 2 people to enter and inspect scavenge space when its clean and use permit to work list to check through all required items like cylinder unit, scavenge air duct flaps, scavenge relief valves.

b.) 1. To check the condition of the piston rings. When the piston is below scavenging ports, inspect the piston crown and cylinder wall. Check for any frictional wear between the sliding surface of cylinder liner and piston. turn the engine, inspect piston rings and piston skirt through the scavenge ports.

  1. To check the condition of the cylinder liner and check for abrasion on the liner surface for remnants of mechanical wear, corrosion, and combustion.
  2. to check that the scavenge drains are clear of blockage and to Check for micro seizures on the piston’s rings and liner surface.
  3. Check the free movement of piston ring springiness by pressing the rings and inspect the piston rod.
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9
Q

with reference to turbochargers;

what is the purpose of U-tube manometer?

A

main engine air coolers and the turbochargers are equipped with U-shaped glass tubes filled with liquid. These tubes are called U-tube manometers, and they are used to measure the pressure difference between two points in a fluid system. A U-tube manometer is a simple device that consists of a U-shaped glass/plastic tube containing liquid, usually water or oil. The liquid level in each leg of the tube depends on the pressure applied to that leg. If both legs are exposed to the same pressure, such as atmospheric pressure, the liquid levels will be equal. However, if one leg is connected to a point of higher pressure, such as the inlet of an air cooler or a turbocharger, and the other leg is connected to a point of lower pressure, such as the outlet of an air cooler or a turbocharger, the liquid level in the high-pressure leg will drop, while the liquid level in the low-pressure leg will rise. The difference in liquid levels indicates the pressure difference between the two points. So, the principle behind their operation is simple: as the differential pressure across the component changes, the liquid level in one arm of the U-tube rises while the other falls, providing a visual indication of the pressure difference.

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10
Q

why are U-tube manometers used instead of pressure gauges?

A

U-tube manometers are used instead of pressure gauges for several reasons:

Direct Reading:One of the primary advantages of U-Tube Manometers is that they provide a direct reading of the differential pressure. Unlike pressure gauges that rely on mechanical elements, U-Tube Manometers offer a clear and instantaneous visual representation of the pressure difference, making them highly reliable. They are accurate and reliable, as they are not affected by temperature changes or mechanical vibrations.

Accuracy:U-Tube Manometers are known for their accuracy and precision in measuring pressure differentials. Pressure gauges may drift or require recalibration over time, while U-Tube Manometers maintain their accuracy as long as the liquid column remains stable. They do not require any external power source or calibration.They can measure both positive and negative pressures, as well as vacuum.

Durability:U-Tube Manometers are robust and durable instruments that can withstand harsh marine environments. They are less prone to damage compared to fragile pressure gauge dials and needles. Also, they are simple, cheap, and easy to install and operate.

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11
Q

why are U-Tube Manometers important?

A

U-tube manometers are important because they provide a visual indication of the pressure difference across the air coolers and the turbochargers. This pressure difference reflects the performance and efficiency of these components, as well as the condition of the engine. For example, the main engine air cooler is a heat exchanger that cools down the compressed air from the turbocharger before it enters the engine cylinders. This increases the density and oxygen content of the air, which improves the combustion process and reduces emissions. The U-tube manometer connected to the air cooler shows the pressure drop across the cooler, which is proportional to the amount of heat transferred from the air to the cooling water. A low pressure drop indicates a low heat transfer rate, which means that either the air cooler is dirty or fouled, or that there is insufficient cooling water flow. A high pressure drop indicates a high heat transfer rate, which means that either the air cooler is clean and efficient, or that there is excessive cooling water flow. U-Tube Manometers act as early warning systems. A sudden change in the pressure differential could indicate a problem with the air cooler or turbocharger, allowing engineers to take corrective actions before the issue escalates, potentially avoiding costly repairs and downtime. By monitoring the U-tube manometers regularly, one can assess the performance and condition of the air coolers and turbochargers, and take appropriate actions to maintain or improve them.

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12
Q

what maintenance is carried out on U-tube manometers

A

Maintenance of U-Tube Manometers

U-tube manometers require little maintenance, but proper maintenance of U-Tube Manometers is essential to ensure their accuracy and reliability:

Liquid Column Inspection:Regularly inspect the liquid column in the U-tube for signs of contamination, evaporation, or air bubbles. Any irregularities can affect the accuracy of the readings and should be addressed promptly.

Leak Checks:They should be checked periodically for any leaks, cracks, clogs, or contamination. Ensure that the connections between the U-tube manometer and the monitored equipment are leak-free. Leaks can lead to false readings and should be sealed immediately.

Calibration:Periodically calibrate the U-Tube Manometer to confirm its accuracy. This calibration process may involve adjusting the liquid column height to a known reference value.

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13
Q

what are some problems that occur with u-tube manometer.

A

When U-Tube Manometers are not functioning correctly, it can lead to inaccurate pressure readings. If there is any discrepancy between the readings of the U-tube manometers and other indicators of the engine performance, such as power output, fuel consumption, exhaust gas temperature, or emissions, one should investigate the possible causes and solutions.

Check for Blockages:Inspect the tubing and connections for any blockages or obstructions that might impede the movement of the liquid in the U-tube. If both legs of the U-tube manometer show equal liquid levels, it means that there is no pressure difference across the component connected to the tube. This could indicate that either the component is blocked or bypassed, or that there is no flow through the component. One should check the valves, pipes, filters, and pumps related to the component, and ensure that they are open, clean, and working properly.

Verify Liquid Integrity:Ensure that the liquid inside the U-tube is in good condition and free from contamination. Replace the liquid if necessary.

Recheck Connections:Confirm that all connections are secure and that there are no leaks. Tighten or replace fittings as needed. If one leg of the U-tube manometer shows a higher liquid level than the other, it means that there is a negative pressure difference across the component connected to the tube. This could indicate that either the component is leaking or damaged, or that there is a backflow or reverse flow through the component. One should check the seals, gaskets, flanges, and clamps related to the component, and ensure that they are tight, intact, and aligned correctly.

Verify Liquid Column Stability:If the liquid column is fluctuating excessively, it could indicate air bubbles or evaporation. Replenish the liquid and remove any trapped air. If the liquid level in the U-tube manometer fluctuates or oscillates rapidly, it means that there is a pulsating or unstable pressure difference across the component connected to the tube. This could indicate that either the component is vibrating or resonating, or that there is a surge or stall in the flow through the component. One should check the mounts, supports, dampers, and silencers related to the component, and ensure that they are rigid, secure, and effective.

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14
Q

what is the purpose of charge air coolers?

A

The turbocharger uses the exhaust gas from the engine to compress new air and charge the engine with a positive pressure higher than ambient conditions. Exhaust gas temperature convection and compression raises the temperature of the air and this cannot be delivered directly into the engine due to operational limitations exceeding.
As a result, the engine is equipped with a cooler that returns the air temperature to ambient relatively close levels.
Because hot air has a lower density, the mass of air charged into the engine is smaller than when the air is cold.
Thus, the charge air cooler increases the density and lowers the temperature of the charge air. The compressed charged air exiting the charge air cooler will have a temperature of around 40 to 50 degrees Celsius, down from approximately 150 degrees Celsius. At cold temperatures, the lower temperature of the air increases the density of the charge air. Increased charge air density increases scavenging efficiency and allows for more air to be compressed inside the engine cylinder, allowing for more fuel to be burnt inside the combustion chamber, resulting in increased power. Additionally, the engine is kept at a safe operating temperature. Compression temperature reduction alleviates stress on the piston, piston rings, cylinder liner, and cylinder head. Additionally, the charge air cooler lowers the exhaust gas temperature. If very cold air reaches the cylinder liner, a severe thermal stress occurs, resulting in cylinder liner failure. Charge air coolers are installed between the turbocharger compressor outlet and the engine intake or scavenging manifold.

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15
Q

What causes fouling of the air coolers?

A

When the air cooler become fouled, the heat transfer between air and cooling agent, which is normally fresh water, is decreasing and this is indicated by the raise in air temperature after cooler and a raise in the pressure drop across the cooler (U-tube manometer). Fouling of the air passages in air cooler, which is part of the engine turbocharging system, is usually due to oil film and oily-water films collected on the sides of the tubes and tube fins. Lint and similar material adheres to these films of oil or emulsion. The presence of oil may be caused by faulty air filters which allow the air to pass by the side of the filter element. Sometimes the oil is drawn from bearing at the blower end. The presence of moisture is usually the result of high humidity, when the engine is operating in warm air temperatures in conjunction with low sea water temperature. So, the signs of air coolers on air side are: higher pressure drop across the cooler, higher air temperature after the cooler, higher cooling water outlet temperature, higher under piston scavenging air temperature, higher exhaust temperature on all cylinders and in worst case scenarioturbocharger surging. If the fouling is on the water side of the cooler the signs are: higher air temperature after the cooler, higher cooling water outlet temperature, higher under piston scavenging air temperature and higher exhaust temperature on all cylinders.

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16
Q

how can fouling of air coolers be prevented?

A

As a remedy, fouling can be prevented through proper plan maintenance by cleaning the coolers at regular intervals. The air side of the cooler can be water washed and/or chemically cleaned. On most of the 2 stroke main engines there is a possibility of periodically cleaning the air coolers even during engine operation at low load. On some of the vessel there is designated tank available where a mixture of water and Air Cooler Cleaner chemical are mixed and recirculated through the air cooler for a certain period of time. It is very important to rinse with fresh water the air cooler very well after cleaning and blow with air if possible in order to prevent chemical corrosion of the cooler parts. For the water side a soft brush can be used to clean inside tubes and in case of hard deposits a long drill bit can be used, but with caution in order not to damage the tubes. However, if there is no improvement after cleaning then the cooler needs to be removed from the engine and dipped into a chemical bath for several hours. Usually this procedure, especially for main engines are performed during every vessel special survey (dry docking), when the coolers are dismantled and taken into yard facilities for proper cleaning into chemical ultrasonic bath.

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17
Q

explain why turbocharger surging occurs?

A

Turbochargers are designed to match the engine and balance the rate of air consumption over the whole working range and it should not fall into the surging limit area. Therefore when various engine part do not perform in synchronization with the turbocharger, this will lead to surging . Surging can have a multitude of reasons with which most of the engineers are more or less familiar, but sometimes finding the cause of surging can be troublesome and time consuming. Surging must be avoided as much possible as it reduces the turbocharger’s efficiency and performance and continuous surging can cause damage of its bearings and compressor failure.

The most common causes can be:

Rapid change of engine load – this often happens during bad weather when the vessel is pitching heavily and propeller comes out of the water and in this case the engine rpm must be reduced concomitantly with changing of vessel course in order to slow down the vessel pitching. Most of the engine governors have a rough sea mode that will slow the governor response in such cases in order to prevent turbo surging. Another reason of change in load can be a defective engine governor or high wear and lag in governor command link to the engine. This can be easily observed especially during good weather if sudden and frequent rpm change occurs in the engine.

Improper power distribution between engine cylinders. In this case one unit is producing more or less power than the others, thus leading to engine unbalance and variation on exhaust gas pressure. This is affecting mainly the impulse type turbochargers as the exhaust is pumped directly into the turbine. In order to remedy this issue a power card must be taken on the engine to determine and remedy the faulty cylinder. The fault in the cylinder may be: excessive wear of the cylinder, unit misfiring, leaking exhaust valve, improper adjusted valve timing and leaking injectors.

Fouled turbocharger parts like: dirty filters (can be observed visually or by checking the U-tube manometer installed on the compressor silencer), damaged silencer, dirty and clogged nozzle ring, dirty turbine impeller, worn out turbocharger’s bearings etc.

Dirty and clogged scavenging air cooler and/or water mist catcher prevents the air flow and creates back pressure into the compressor. This can be observed on the U-tube manometer installed on each scavenge air cooler. The value must be compared with the one’s from the engine shop trial at different loads. Hence the importance of having a fully functional U-tube manometer, although you can find plenty vessel where nobody pays attention to this. As a remedy the air cooler must be chemically cleaned, although this must be a frequent activity and part of the engine plan maintenance system.

Damaged or blocked scavenging air flaps.

Restriction in exhaust gas flow due fouling of economizer, nozzle ring dirty, obstruction of exhaust manifold, damage gratings inside exhaust manifold. As a remedy U-tube manometer readings on economizer must be checked and compared with the shop trial and economizer cleaned if necessary. Due nowadays engine slow steaming it is a good practice to soot blow the economizer twice a day using soot remover despite engine load, as long as the engine runs at constant rpm. Similarly, exhaust manifold must be inspected for any obstructions and gratings checked and repaired as found necessary.

Problems in engine fuel supply system like: leaking injectors, cold fuel which leads to improper injection, engine fuel starvation, seized or defective fuel injection pump etc. As a remedy fuel temperature must be checked and monitored and power card must be taken in order to check the performance of engine cylinders.

In the worst case scenario scavenge or exhaust fire.

These are the most common causes, but sometimes there is some unexpected reason for turbocharger surging. Few years back I’ve been on a vessel with prolonged turbocharger surging issue. The support from the office was really disappointing as they kept told vessel to open and inspect the air coolers for cleanliness. However, after several inspecting and cleaning of air coolers (although Δp was in very good range compared with shop trial), we continued our own investigation by checking the scavenging flaps, water trap, ME exhaust valves, ME performance and compression pressures, exhaust gas economizer Δp, exhaust gas manifold for any obstructions and everything found in good order. After presenting a full report to the office with our investigation and where we explained that something is wrong with the turbocharger (even though as per our records they have been overhauled by a third party company in close relations with superintendents) they decided to send a ME maker representative onboard as they didn’t trust our investigation. I don’t want to blame anyone but it seems that many of the superintendents are simply clerks with no deep engineering knowledge but good at office politics. However, the attending engineer have done the same investigation as we have and in their report specified that everything is in order with ME and the turbocharger have to be opened and inspected (imagine the reaction from the office). However, after long debates the office decided to sent someone else to investigate the turbochargers and we discovered that the nozzle ring’s fin blades were heavily worn (change in thickness and shape) and some of them with hard soot deposits. It seems that the nozzle rings were not replaced at last overhaul as we found few sheared bolts and most probably to remove it would have taken quite a lot of time and would have delayed the vessel. The wear and deposits on nozzle ring’s fins had a negative impact on turbocharger’s efficiency and functioning, as restricted the gas flow and changed the flow pattern, thus leading to turbocharger‘s continuous “barking” and surging.

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18
Q

How is maximum engine performance achieved?

A

For maximum performance to be maintained its essential that during the gas exchange process the cylinder is completely purged of residual gases at the completion of the exhaust phase of the cycle and a fresh charge of air introduced into the cylinder ready for the following compression stroke. However, even the most efficient systems still leave behind unburnt hydrocarbons from the previous cycle, the most fuel efficient engines are using techniques such as exhaust gas recirculation (EGR) which is an attempt to burn some of the unburnt gasses and reduce harmful emissions from the engine. In the case of four-stroke engines, purging the cylinder of the gasses from the previous cycle is carried out by careful timing of inlet and exhaust valves where, because of the time required to fully open the valves from the closed position and conversely to return to the closed position from fully open, it becomes necessary for opening and closing to begin before and after dead centre positions if maximum gas flow is to be ensured during exhaust and induction periods.

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19
Q

What’s the purpose of a valve overlap in 4 stroke engines?

A

Basic object of overlap, that is, exhaust and inlet valves opening together, is to assist in final removal of any exhaust gases from that cylinder so that contamination of charge air is minimal.

The overlap in the case of pressure-charged engines serves to:

further increase this scavenge effect,
provide a pronounced cooling effect which either reduces or maintains mean cycle temperature to within acceptable limits even though loading may be considerably increased. Consequent upon (b) it becomes clear that thermal stressing of engine parts is relieved and with exhaust gas turbo-charger operation prolonged running at excessively high temperatures is avoided. This latter process would have an adverse effect on materials used in turbo-charger construction and could also contribute towards increased contamination.

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20
Q

explain and compare the scavenging arrangement of 2 stroke engines?

A

The scavenging arrangement of two-stroke engines is either uniflow or longitudinal scavenge and loop and cross scavenge

All the latest large two-stroke marine engines currently under construction have been designed to work with the uniflow system that employs a poppet-style exhaust valve situated at the cylinder head. Very early versions of the uniflow system were opposed piston engines where the exhaust (upper piston) uncovered the exhaust port while at the top of its travel. The uniflow system is the most efficient system which is why it has been adopted for new engines.

In the uniflow system the charge air is admitted through ports at the lower end of the cylinder and as it sweeps upwards towards the exhaust discharge area, almost complete evacuation of residual gases is obtained. By suitable design of the scavenge ports or the provision of special air deflectors the incoming charge air can be given a swirling motion which intensifies the purging effect and also promotes a degree of turbulence within the charge which is required for good combustion when fuel injection takes place.

Both cross and loop scavenge systems have exhaust and scavenge ports arranged around the periphery of the lower end of the liner and in so doing eliminate the need for cylinder head exhaust valves or upper exhaust ports and the associated operating gear. This simplifies the engine construction considerably and, in the past, it might also have led to a reduction of maintenance. Due to a simplified cylinder head construction the cylinder combustion space can be designed for optimum combustion conditions. However, the scavenging efficiency is now so much lower than with the uniflow system due to the more complex gas–air interchange and the possibility of charge air passing straight to exhaust with little or no scavenging effect. Careful attention to port design did reduce this problem but not enough to stop its fall from favour.

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21
Q

explain the gas exchange process?

A

The gas exchange process itself may be divided into three separate phases:

  • blowdown
  • scavenge
  • post-scavenge.

During ‘blowdown’ the exhaust gases are expelled rapidly – the process being assisted by generously dimensioned exhaust ports or valves arranged to open rapidly. At the end of this ‘blowdown’ period when the scavenge ports begin to uncover, the cylinder pressure should be at or below the charge air pressure so that the scavenge process which follows effectively sweeps out the residual gases without any resistance from a pressurised charge in the cylinder. With scavenge ports closed again the post-scavenge period allows completion of the gas exchange process. The engine design should ensure that the exhaust discharge mechanisms close as quickly as possible to prevent undue loss of charge air and maximise the trapped air ready for the beginning of compression, giving the highest possible density of charge ready for combustion. Although some loss of charge air is unavoidable it should be borne in mind that the air supply is in excess of that required for combustion and the cooling effect of the air passing through the system has the result of keeping mean cycle temperatures down so that service conditions are less exacting. The production of NOx during combustion, happens at the peak temperatures during the process. Therefore, if these peak temperatures are reduced then so is the volume of environmentally harmful NOx gasses. In the latest engines this is accomplished by using the ‘Miller’ cycle, which modifies the timing of the inlet and exhaust valves to ensure that there are no peak temperatures produced during the combustion process. This can only be done with an engine that has full control over the inlet, exhaust and the start and stop of the fuel injection. Also with this system the pressure charging is increased with the use of two-stage turbo-charging. The increased cylinder pressures encountered with modern turbo-charged machinery may result in exhaust opening being advanced so that sufficient time is given for cylinder pressure to fall to or below charge air pressure when the scavenge ports uncover. A complementary aspect of earlier opening to exhaust is the increased pulse energy obtainable from the exhaust gas which can be utilised to improve turbocharger performance. In many cases this is the main criterion which influences exhaust opening, since the loss of expansive working is more than offset by the gain in turbo-charger output. Obviously in the case of reversing engines there may be some slight penalty incurred if prolonged operation in the astern direction is considered.

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22
Q

explain what is pressure charging?

A

By increasing the density of the air, and therefore the mass of oxygen present in the cylinder at the beginning of compression a corresponding greater mass of fuel can be burned giving a substantial increase in power developed. The degree of pressure charging required, which determines the increase in air density, is achieved by the use of free-running turbo-chargers which are driven by the energy left in the exhaust gases expelled from the main engine. About 20% of the energy available in the exhaust gas is utilised in this way. In the past it was usual practice to employ some form of scavenge assistance either in series or in parallel with the turbo-chargers. This was accomplished by engine-driven reciprocating scavenge pumps, under piston effect or independently driven auxiliary blowers. Only the under-piston effect and auxiliary blowers would still be used on the engines of ships still in service today. The turbo-charger provides charge air at 70–95% of required pressure with underpiston effect or series pump making up the balance. There is an increase in temperature of air delivered to the engine since air cooling is carried out after the turbo-charger only. With parallel operation air supply to engine is increased by air delivery from pumps with proportionate increase in output resulting in greater exhaust gas supply to turbo-charger and improved turbo-charger performance

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23
Q

what are the advantages of pressure charging?

A
  • substantial increase in power for a given speed and size
  • better mass power ratio, that is, reduced engine mass for given output
  • improved mechanical efficiency with reduction in specific fuel consumption
  • reduction in cost per unit of power developed
  • an increase in air supply has a considerable cooling effect leading to less exacting working conditions and improved reliability.
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24
Q

the manner in which the energy contained within the exhaust gases is utilised to drive the turbo-charger may be described in two ways:

1.The pulse system of operation
2. Constant pressure operation.

explain both of these systems?

A

Pulse operation

This makes full use of the higher pressures and temperatures of the exhaust gas during the blow-down period and with rapidly opening exhaust valves or ports the gases leave the cylinder at high velocity as pressure energy is converted into kinetic energy to create a pressure wave or pulse in the exhaust leading to the turbo-charger. For pulse operation it is essential that the exhaust leading from the cylinder to the turbine entry are short and direct without unnecessary bends so that volume is kept to a minimum. This ensures optimum use of available pulse energy and avoids the substantial losses that could otherwise occur with a corresponding reduction in turbo-charger performance. Of necessity, exhaust ducting must be arranged so that the gas exchange processes of cylinders serving the same turbo-charger do not interfere with each other to cause pressure disturbances that would affect purging and recharging with an adverse effect upon engine performance. With two-stroke engines the optimum arrangement is three-cylinder grouping with 120° phasing which gives up to 10% better utilisation of available energy than cylinder groupings other than multiples of three. Due to the small volume of the exhaust ducting and direct leading of exhaust to turbine inlet the pulse system is highly responsive to changing engine conditions giving good performance at all speeds. Theoretically, turbo-charging on the pulse system does not require any form of scavenge assistance at low speeds or when starting. In practice however the use of an auxiliary blower or some other means of assistance is employed to ensure optimum conditions and good acceleration from rest.

Constant pressure operation

In this system the exhaust gases are discharged from the engine into a common manifold or receiver where the pulse energy is largely dissipated. Although the pulse energy is lost, the gas supply to the turbine is at almost constant pressure so that optimum design conditions prevail since, under normal conditions, gas flow will be steady rather than intermittent. Furthermore, as the engine ratings increase, the constant pressure energy contained in the exhaust gas becomes increasingly dominant so that sacrifice of pulse energy in a large volume receiver is of less consequence. Figure 4.5 shows the results of tests carried out on a Wärtsilä two-stroke engine which indicates that up to a BMEP of around 7 bar the advantage lies with the pulse system but as the BMEP increases beyond this figure the constant pressure system becomes more efficient giving greater air throughout and some slight reduction in the fuel rate. Due to the much larger volume of the exhaust system associated with constant pressure operation the release of exhaust gas is rapid and earlier opening to exhaust is generally only necessary to ensure that cylinder pressure has fallen to or below the charge air pressure when the scavenge ports begin to uncover. With a possible reduction in exhaust lead expansive working can be increased which is a further contributory factor in reducing the fuel rate. A major drawback to constant pressure operation is that the large capacity of the exhaust system gives poor response at the turbo-charger to changing engine conditions with the energy supply at slow speeds being insufficient to maintain turbo-charger performance at a level consistent with efficient engine operation. Some form of scavenge assistance such as under-piston scavenging is often utilised. To offset this however the number of turbo-chargers required as compared to pulse operation can be reduced, a greater flexibility exists in the case of turbo-charger location and exhaust arrangement and no de-rating of engine need to be considered for cylinder groupings other than multiples of three. For this reason most large slow-speed two-stroke engines tend to be of the constant pressure configuration. Figure 4.6 shows the diagrammatic arrangement of the Wärtsilä RTA scavenge engine which operates with constant pressure supercharge. In normal operation air is drawn into under-piston space B from common receiver A and compressed on downstroke of piston to be delivered into space C so that when scavenge ports uncover purging is initiated with a strong pressure pulse. As soon as pressure in spaces B/C falls to common receiver pressure in space A scavenge continues at normal charge air pressure. For part load operation the auxiliary fan is arranged to cut in when charging pressure falls below a pre-set value. Air is drawn from space A and delivered into space F and this together with under-piston effect ensures good combustion and trouble-free operation under transient conditions. See figure 4.7 for the MAN arrangement.

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25
Q

Under conditions of high humidity precipitation at the air cooler can occur how is this prevented and why?

A

Carryover of this water to the engine can have a number of detrimental effects. Water contamination of cylinder lubricating oil may reduce its viscosity and hence its ability to withstand the imposed loads leading to increased cylinder and piston ring wear. Water contamination may also lead to corrosion of engine components. To prevent the carryover of water a water separator is fitted.

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26
Q

with the aid of a sketch explain the working principle of a water seperator?

A

see EK reed motor book scavenging/supercharging figure 4.8 for sketch

Figure 4.8 shows a water separator fitted on the outlet side of an air cooler. This separator utilises the difference in the mass of water and air. As the moist air flows into the vanes its direction is changed. Due to its lower mass the air is able to change direction easily to flow around the vanes. The water, however, because of its greater mass and, therefore momentum, is not able to change direction so easily and flows into the water trap to be removed at the drain. The water separator should also be sprayed with cleaning solvent when cleaning the air cooler. It must be noted that the vapour given off by cleaning solvents is harmful and by spraying into air coolers may contaminate the atmosphere throughout the engine. The air coolers should not be cleaned when personnel are working within the engine

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27
Q

Some engine manufacturers are introducing water injection into the combustion process. how is this different from water contamination?

A

This is different from the water contamination because it is a carefully designed system that has been developed following an extensive research and development programme where the effect on all the engine components and fluids will have been considered and any adverse effect will have been removed as part of the engine’s design. The reason for the water injection is to reduce the peak temperatures of combustion thus reducing the harmful NOx.

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28
Q

what’s the reason for not overcooling the charge air?

A

The temperatures of the inlet air, combustion and exhaust have all been calculated carefully by the engine’s designers. This is not only done so that the correct density of air can be achieved but also that the gasses do not fall to their ‘dew point’ where water will be formed from any steam in the system. The water of course will combine with any oxide of sulphur to form sulphuric acid which in turn will damage the engine or other components.

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29
Q

explain the importance of air cooling

A

air must be passed through a cooler on its passage to the engine in order to reduce its temperature and restore the density of the charge air to optimum conditions. Correct functioning of the cooler is therefore extremely important in relation to efficient engine operation. Any fouling which occurs will reduce heat transfer from air to cooling medium and it is estimated that the 1°C rise in temperature of air delivered to the engine will increase exhaust temperature by 2°C. Reduction in air pressure at cooler outlet due to increased resistance is also a direct result of fouling. It is therefore imperative that air coolers are kept in a clean condition. It is preferable that this is accomplished on a regular basis rather than changing a dirty cooler since progressive fouling will have an adverse effect on engine performance. Regular cleaning should be included into the ship’s routines and can be carried out by spraying with a commercial air cooler cleaning solvent.

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30
Q

what is the most common turbo charger used?

A

The majority of marine turbo-chargers is still single-stage axial flow turbine wheel driving a single-stage centrifugal air compressor via a common rotor shaft to form a self-contained free running unit.

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31
Q

State 2 important key turbo charger constructional features and characteristics?

A

Due to the high rotational speeds perfect dynamic balance is essential if vibrations are to be reduced. This is done by mounting the bearings in resilient housings incorporating laminar spring assemblies to give both axial and radial damping effects.

Another aspect to be prevented flutter or chatter at bearing surfaces when they are stopped so that incidental bearing damage is prevented. Lubrication of the bearings may be by separate or integral oil feed, but whatever arrangement is adopted it must be fully effective at a steady axial tilt of up to 15° and support a temporary tilt of 22½° as may occur in a heavy sea. The bearings themselves may be a combination of ball and roller bearings or separate sleeve (journal)-type bearings.

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32
Q

periodic replacement of ball and roller assemblies is essential if trouble-free service is to be maintained what is is the resons for this?

A

this is due to the fact that rapid and repeated deformation with resultant stressing causes surface metal fatigue of contact surfaces with the result that failure will occur. The effects of vibration, overloading, corrosion or possible abrasive wear, lead to premature failure which emphasises the need for isolation of bearings from external vibrations together with use of correct grade of lubricant and effective filtration. Plain bearings should however have a life equal to that of the blower provided that normal operating conditions are not exceeded. Ball bearings can end up with tiny indentations in the rolling surface caused by vibrations from the vessel when the turbo-charger is at rest for longer lengths of time.

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33
Q

what cooling media is used for turbo chargers?

A

Cooling media for cooled exhaust gas casings is generally from the engine jacket water cooling system although in some cases seawater has been employed. In both cases anti-corrosion plugs are fitted to prevent or inhibit corrosion on the water-side.

With water-cooled casings under light load conditions when low exhaust temperatures are encountered it is possible that precipitation of corrosive forming products – mainly sulphuric – will occur on the gas side of the casing. This results in serious corrosive attack which is more marked at the outlet casing because of lower temperatures. Methods of prevention such as enamelling and plastic coatings, etc. have been tried to alleviate this problem with varying degrees of success. A particularly effective approach to the problem is the use of air as the cooling media with the result that this particular instance of corrosive attack is virtually eliminated.

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34
Q

What’s the material used for the components in the high temperature gas stream and why?

A

The components in the high-temperature gas stream, that is, the nozzle ring, turbine wheel, blades and rotor shaft are manufactured from heat resisting nickel-chrome alloy steel to withstand continuous operation at temperatures in excess of 450°C. Some degree of cooling may be given by controlled air leak-off past the labyrinth seal, between the back of the impeller and volute casing, which flows along the shaft towards the turbine end.

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35
Q

What’s the function of the diffuser?

A

The diffuser functions to direct air smoothly into the volute casing which continues the deceleration process with further increase in air pressure. From here the air passes to the charge air receiver via the air cooler. The turbine end of the turbo-charger consist of casings which house the nozzle-ring turbine wheel and blading.

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36
Q

What does the blower end of a turbo charger consist of?

A

the blower end of the turbo-charger consists of a volute casing of light aluminium alloy construction which houses the inducer, impeller and diffuser which are also of light alloy construction.

37
Q

What’s the function of the inducer?

A

The function of the inducer is to guide the air smoothly into the eye of the impeller where it is collected and flung radially outward at ever-increasing velocity due to the centrifugal effect at high rotational speed. At discharge from the impeller it passes to the diffuser where its velocity is reduced in the divergent passages thus converting its kinetic energy into pressure energy.

38
Q

Some manufactures utilising sleeve-type bearings mount them inboard of the compressor and turbine. what advantages does this have?

A

1.A short, rigid shaft is possible.

2.It allows large volume turbine and compressor inlet casings, free of bearing housings.

3.The main casing, bearing housings and turbo-machinery form one module allowing the rotor to be withdrawn from the turbine casing without disconnecting engine ductwork.

39
Q

With the aid of a system drawing describe how turbochargers are lubricated?

A

see motor sketch pack for drawing

The oil for the bearings is supplied from the main engine lubricating oil system or a separate oil feed as shown in figure 4.11. The oil level in the high-level tank should be maintained about 6 m above the turbo-chargers. This will ensure that the oil pressure reaching the bearings should never fall below a pressure of around 1.6 bar. If level of oil falls below the mouth of the inner drain pipe it is quickly emptied and an alarm condition is initiated. After an alarm it takes about 10 min to empty the high-level tank which is sufficient to ensure adequate lubrication of the turbo-chargers as they run down after the engine is stopped.

40
Q

Recent developments have increased the overall efficiency of turbo-chargers by improving the aerodynamic performance and increases in pressure ratio. state one of theses improvements

A

One improvement attained is as a result of the general adoption of constant pressure charging for large slow-speed two-stroke engines. This eliminates the excitation of blade vibration by exhaust gas pulses. Excitation of blade vibration is still possible but with careful attention to the choice of nozzle vane number and natural frequencies of vibration of blades it is possible to dispense with the need for rotor blade damping wire. Not only does this give greater turbine aerodynamic efficiency, but greater resistance to contamination by heavy fuel combustion products.

41
Q

With the aid of sketches briefly describe the two Types Of Turbochargers In Marine Diesel Engines

A

Based on the exhaust gas flow, there are two type of turbochargers, Axial- flow turbo chargers and Radial flow turbo chargers.

Axial- Flow Turbochargers

Exhaust gas in and out of the turbine blade along the axis of the shaft are called axial- flow turbochargers.

Radial- Flow Turbochargers

Exhaust gas enters the turbine blades along the radial direction and leaves the turbine along the trailing edge of the blade. these type of turbo chargers are called Radial- Flow turbochargers

For smaller higher-speed diesel applications (690–6,700 kW range)
the use of radial flow turbo-chargers is common. The casings are uncooled but require insulation. Bearings are of the sleeve type and are lubricated from the engine lubricating oil system. The turbine wheel is a one-piece casting of a design which gives acceptable efficiencies over the entire operation range. The compressor is also of a one-piece design of backswept vane giving stable operating characteristics. At high airflows the efficiency tends to decrease due to losses at the turbine exit.

42
Q

Explain what to do in the event of Turbo-charger breakdown?

A

Correct operating and shut down procedures, depending upon engine type, will be found in the engine builders and/or turbo-charger manufacturers’ recommended practice. As a general rule however, in the event of damage to the turbo-chargers, the engine should be stopped immediately so that the damage is limited and broken fragments do not cause further damage elsewhere within the engine. Under conditions where the engine cannot be stopped, without endangering the ship, engine speed must be reduced to a point where the turbo-charger speed has dropped to a level where any vibration that is usually associated with a malfunction is no longer perceptible. If the engine can be stopped but lack of time does not permit in repair or possible replacement of defective charger it is essential that the rotor of the damaged unit is locked and completely immobilised. If exhaust gas still flows through the affected unit once the engine is restarted, the coolant flow through the turbine casing needs to be maintained but due to the lack of sealing air at shaft labyrinth glands the lubricating oil supply to the bearings will need to be cut off – with integral pumps mounted on the rotor shaft, the act of locking the shaft ensures this – otherwise contamination of lubricant together with increase in fouling will occur. For rotor and blade cooling a restricted air supply is required and can be achieved by closing a damper or flap valve in the air delivery line from the charger, to a position which gives limited flow from scavenge receiver back to the damaged blower. Alternatively a bank flange incorporating an orifice of fixed diameter can be fitted at the outlet flange of the blower. Where only a single turbo-charger has been affected, out of a number associated with the engine, the power developed by the engine will obviously depend upon charge air pressure attainable. At the same time a careful watch must be kept upon exhaust condition and temperature to ensure efficient engine operation with good fuel combustion. In the event of all turbo-chargers becoming defective it is possible to remove blank covers from the scavenge air receiver so that natural aspiration supplemented by any under-piston effect, or parallel auxiliary blower operation is possible – if this method of emergency operation is carried out protective gratings must be fitted in place of blind covers at the scavenge air receiver. In all cases when running at reduced power special care must be taken to ensure any out-of-balance forces, due to variation in output from affected units, do not bring about any undue engine vibration.

43
Q

what is turbocharger fouling?

A

Turbo-charger fouling

Turbo-chargers that have contaminated turbines and compressors will have less efficiency and lower performance than their design specification, which results in higher exhaust temperatures. In four-stroke applications the charging pressure can increase due to the constriction of the flow area through the turbine resulting in unacceptable high ignition pressures. To maintain turbo-charger efficiency it is important to ensure that all operating parameters are maintained according to the manufacturer’s recommendations. If the compressor draws its air from the machinery spaces then steps must be taken to maintain as clean an atmosphere as possible since leaking exhaust gas and/or oil vapour will accelerate the deterioration of efficiency. In some installations the turbo-chargers draw air through ducts from outside the engine room.

44
Q

describe how to preform water washing on the blower side of turbocharger?

A

Water washing – blower side

On the air side of the turbo-charger, dry or oily dust mixed with soot and possibly salt from a salt-laden marine atmosphere can lead to deposits which are relatively easy to remove with a water jet, usually injected at full load with the engine warm. A fixed quantity of liquid (1–2½ | depending upon blower size) is injected for a period of from 4 to 10 s after which an improvement should be noted. If unsuccessful the treatment can be repeated but a minimum of 10 min should be allowed between wash procedures. Since a layer of a few tenths of a millimetre on impeller and diffuser surfaces can seriously affect blower efficiency the importance of regular water washing becomes obvious. It is essential that the water used for wash purposes comes from a container of fixed capacity – under no circumstances should a connection be made to the fresh water system because of the possibility of uncontrolled amounts of water passing through to the engine. A cup full of water could be mixed with a general cleaning agent and carefully poured into the air filter as the turbo-charger is running.

45
Q

describe how to do water washing on turbine side?

A

Water wash – turbine side

This must be carried out at reduced speed by rigging a portable connection to the domestic fresh water system and injecting water, via a spray orifice before the protective grating at turbine inlet, for a period of 15–20 min with drains open to discharge excessive moisture and or deposits which do not evaporate off. Since water washing may not completely remove all deposits, and can interact with sulphur, causing a resultant corrosive attack, chemical cleaning may be used in preference. This effectively removes deposits at the turbine and moreover is still active within the exhaust gases passing to the waste heat system, so that further removal of deposits occurs which maintains heat transfer at optimum condition and keeps back-pressure of exhaust system well within the limits required for efficient engine operation.

46
Q

describe how to do dry cleaning on turbine side?

A

Dry cleaning – turbine side

Instead of water, dry solid bodies in the form of granules are used for cleaning. About 1.5–2 kg of granules is blown by compressed air into the exhaust gas lines before the gas inlet casing or protection grid. Agents particularly suited to blasting are natural kernel granules, or broken or artificially shaped activated carbon particles with a grain size of 1.2–2.0 mm. The blasting agents have a mechanical cleaning effect, but it is not possible to remove fairly thick deposits with the comparatively small quantity used. For this reason this method must be adopted more frequently than for cleaning with water. Dry cleaning is carried out every 24–50 h. The main advantage of this type of turbine cleaning is that it can be carried out at full or only slightly reduced load. The cleaning equipment configuration is shown in figure 4.15. Turbo-charger manufacturers recommend that heavily contaminated machines, which have not been cleaned regularly from the very beginning or after overhaul, should not be cleaned by water washing or granulate injection. This is because the dangers of incomplete removal of deposits may cause rotor imbalance. These turbo-chargers need careful dismantling and cleaning with the machine apart is recommended.

47
Q

explain what is surging?

A

Surging may occur in heavy weather when the propeller comes out of the water and the governor shuts the fuel off almost instantaneously. To obtain efficient and stable operation of the charging system it is essential that the combined characteristic of the engine and blower are carefully matched.

Apart from fouling of turbo-charger other contributory factors to surging are contamination of exhaust and scavenge ducting, ports and filters. Since faulty fuel injection leads to poor combustion and greater release of contaminants the need to maintain fuel injection equipment at optimum conditions is essential. Other related causes are variation in gas supply to turbo-chargers due to unbalanced output from cylinder units and mechanical damage to turbine blading, nozzles or bearings, etc.During normal service the build-up of contaminants at the turbo-charger can be attributed to deposition of air-borne contaminants at the compressor which in general are easily removed by water washing on a regular basis. At the turbine however, more active contaminants resulting from vanadium and sodium in the fuel together with the products of incomplete combustion deposit at a higher rate which increases with rising temperature. A further problem arises with the use of alkaline cylinder lubricants with the formation of calcium sulphate deposits originating from the alkaline additives in the lubricant. Again water washing on a regular basis is beneficial in removing and controlling deposits but particular care needs to be taken to ensure complete drying out after the washing sequence since any remaining moisture will interact with sulphurous compounds in exhaust gas stream with damaging corrosive effect but this effect should only be slight as the turbine dries out quite quickly after the water is removed.

48
Q

The reduction in the turbocharger performance and hence reduced engine output after turbocharger overhaul is a clear evidence of improper overhauling procedure and assembly.

what are the possible causes and how to rectify?

A

Possible faults during overhauling are following:

The compressor axial clearances set during the bearing reassembly are notcorrect and the rotor could be fouling the casing, hence the rotational speedwould fall. If the turbocharger rotates at a slower rate, then there will be less airdelivered and hence lower pressure.

The turbocharger casings have not been correctly reassembled, causing airleakage. This leakage would reduce the pressure generated at the turbocharger outlet

The turbocharger filters were not cleaned, and the restriction would cause anair flow restriction. The pressure ratio is known across the turbocharger atcertain operating speeds, would cause the discharge pressure to fall if theintake or suction pressure is low.

The following engine operational information should be gathered inorder to detect the possible cause of the problem with turbocharger overhaul:

Engine power
Scavenge and exhaust manifold pressures
turbocharger speed
Inlet/outlet gas, air and water temperatures
Differential pressures of the air filter, air cooler, and exhaust gas boiler (iffitted)

Once these readings were taken, they could be checked against previous data frombefore the overhaul, or even datum readings when the engine and turbocharger were new.Abnormalities would be noted, and this would hopefully indicate the possible defect.Specific faults such as the air filter fouling would be indicated by the measurement ofthe pressure differential across the filters.
The defects stated would arise due to an incorrect procedure during turbocharger overhaul, and lackof suitable checks to ensure correct reassembly.A new procedure detailing the areas to be checked would be drawn up.
Thisprocedure would list the specific checks and measurements that must be taken duringreassembly. If a specific fault has previously occurred, then a method to overcomethis defect would be recorded in the new procedure.

49
Q

what’s the procedure for turbocharger overhauling?

A

1.Lock off the engine staring mechanism.
2.Remove the turbocharger air filter.
3.Drain off the oil from both drain plugs.
4.Remove the bearing covers from both sides.
5.Remove the locking wires.
6.Unscrew the hexagon screws and remove oil suction pipes.
7.Tighten again the hexagon screws of the bearing boxes.
8.Check the deflection of the divergent nozzle by using pick tester and magnet stand.
9.Remove the divergent nozzle by screw driver.
10.Measure the K value at the blower side by using depth micrometer or caliper and straightedge.
11.Lock the rotor with special tool.
12.Extract the lubricating disc.
13.Extract the both bearings by bearing extractor.
14.The various parts should be warped in waxed paper to protect them against dirt andmoisture.

Checks on Turbocharger while Overhauling

1.Check the deflection of divergent nozzle.
2.Measure the K value at blower side.
3.Change the bearing on both sides with the new one (because bearing service life is same as turbochargeroverhauling time).
4.Clean blower and turbine side with chemical and inspect carefully.
5.Check the labyrinth seal.
6.Made clear the labyrinth seal air line
7.Check the casing for crack & wear
8.Blade condition
9.After reassembled, check Static Balance
10.Check Impeller and Casing clearance

50
Q

What is the main purpose of turbocharger water washing ?

A

To ensure efficient functioning of turbocharger.
To protect the compressor and turbine from contamination (Deposits).

51
Q

What are Disadvantages of turbocharger water washing to turbine side ?

A

Engine speed has to lower.
Thermal stress and corrosion usually occurred.
Longer cleaning time.
Very fine hard deposits and residues cannot be removed easily with water washing.

52
Q

What are Advantages of solid (crystal) cleaning or grit washing ?

A

Not required to reduce engine rpm, thus not affect on scheduled voyage
No used of water, so no corrosion and thermal stress.
Cleaning time is short.
Not wear turbine blade.
Effectively remove combustion residues and hard particle.

53
Q

how to do blower side water washing procedure?

A

Blower side water washing procedure

1.It can be done when M/E on full load.
2.Fill up the warm fresh water to hopper and closed the cover.
3.Open the valve and water will flow into the blower casing and mechanically attack theblower blades and clean the deposit.
4.Close the valve, open the cover and check the cleaning water must be empty.

54
Q

what’s the procedure for turbine side water washing?

A

Turbine side water washing procedure
1.Turbine side water washing can be made with hot fresh water.
2.Inform to the bridge
3.Reduce the M/E rpm to recommended speed and hence turbocharger rpm.
4.Check the water washing injection nozzle if fitted. (directly aim to the exhaust grips beforeentering to the turbocharger)
5.Open turbocharger drain valve.
6.Open the water supply about 1 bar to turbine side.
7.Water washing must be made until the clean water comes out.
8.Close the water supply and remove the nozzle.
9.Exhaust side drain can be closed after all water is drained out and dried.
10.Inform to the bridge and increase the M/E rpm gradually to sea speed.
11.The turbine side water washing is usually at departure after manoeuvring time.
12.For usual practice cleaning is done at every 500 hr, running hour depending on thecleanliness of the turbocharger .

55
Q

what’s the procedure for grit washing or dry cleaning of a turbocharger?

A

Grit Washing or Dry Cleaning of Turbocharger

1.Turbine side cleaning is superseded by walnut shell, with grain size of 12 to 34mesh
2.No speed reduction required and cleaning can be done at full speed, once every day
3.Compressed air of (3 -5 bar) is used to help the grains strike the deposited Turbine Bladesand Nozzles, giving effective cleaning of hard particles
4.Air supply pipe is fitted to solid grain container, and grains are injected into exhaust system byair pressure, at the same point (as in water washing ) just after exhaust grids
5.Turbine casing drain kept open during cleaning time (about 2 minutes only)

56
Q

What measurements are taken during auxiliary engine turbocharger overhaul ?

A

K value, it is a distance between the rotor shaft end and the flange of bearing covermeasure at blower side (axial clearance).
Check radial clearance (at plane bearing), by placing clock gauge on the shaft from the topand clamp by screw driver from bottom, record the clearance.
Rotor and Casing clearance (for new casing or new rotor) (L & M values)

57
Q

How to measure turbocharger axial and radial clearance ?

A

Axial Clearance
Push the shaft by screw jack and measure by Depth Gauge (0.2 – 0.3 mm)

Radial Clearance
Lift the shaft radially and measure by Dial Gauge (0.15 – .02 mm)

58
Q

Why turbocharger exhaust outlet lower than inlet temperature ?

A

Some exhaust gas heat and pressure energy is transferred to mechanical rotating energy for turbocharger,thus pressure become decrease and temperature lower.

59
Q

What will occur if oil leak in turbocharger system ?

A

If oil is leaked into the air system the cooling surface are covered with oil which are insulated& cooling efficiency will be reduce (ie. Scavenge temperature drop; Exhaust temperature high)
Also there will be deposits on the blower and blower efficiency will be reduced
If oil leaked into exhaust side, Carbon deposits on the nozzle & turbine blade. It causesurging, reduces blower efficiency and fire in the exhaust piping (uptake fire)

60
Q

with reference to turbocharger over run;

what are the causes,
effects and how to prevent it from happening?

A

Turbocharger Over Run

Causes

Happens in constant pressure turbo charged engine
Caused due to fire and or detonation of scavenge space
Exhaust trunk fire due to accumulation of leaked or excess lube oil and unburned fuel

Effects

Turbocharger bearings, casing damage
E/R fire

Prevention

Scavenge space regular cleaning
Exhaust gas pipe regular cleaning
Maintain complete combustion of fuel
Liner, piston and rings, fuel vales, cylinder lubrication, maintained in good order
Avoid operating M/E under reduced load for long term

61
Q

what are the causes of turbocharger vibration?

A

Unbalancing
Bearing defects
Deposits in nozzle ring
Impingement
Surging, Scavenge Fire, Overloading

62
Q

In the event that a vessel is operating at steady speed, and a turbocharger vibrates, what are the reasons for this and can you minimise these vibrations?

A

When operating at steady speed, turbocharger vibrations could occur when:

Rotor imbalance due to rotor damage from an object displaced from the cylinder,such as a broken piston ring or exhaust valve
Imbalance of the rotor from breaking of the lacing or binding wire
Bearing failure, which would reduce the support of the rotor
Slack foundation mounting of the turbocharger casing
Rotor imbalance following inadequate in-service cleaning
Surging of the turbocharger, when the unit is operated close to the surge linepossibly due to a fouled hull
Vibration transmitted to the turbocharger unit from an adjacent machinery unit.

Turbocharger vibrations can minimized by the following:

Fitting of a protective grid between the engine and the turbocharger, andregular overhaul of the exhaust valve/piston rings
Regular changing of the lacing wire at the inspection stage
Regular changing of the bearings and the sump oil
Regular checks of the foundation bolts

63
Q

in the event that a turbocharger is damaged what actions should you take?

A

1.Stop engine
2.Remove bearing end covers and fit rotor locking devices at both ends
3.Close in the compressor outlet to ensure that scavenge air does not leak out, but at thesame time prevent rotor warping
4.Maintain freshwatercirculation
5.When the engine is operating, then the engine power must be reduced to avoidthermal overload of the engine. The amount of engine power that can be developedcould be limited by one of the following:Excess exhaust gas temperatures,Excess exhaust smoke,Engine vibration,Excess speed of the remaining turbocharger.
6.The time taken for engine speed up would be extended and thus manual engine speedup should be used.

64
Q

what kind of maintenance must be carried out on a turbocharger?

A

Regular maintenance must be carried out to prevent unwanted turbocharger vibrations.
The gas side of turbocharger refers to the nozzle ring and turbine blading. The fall off in performanceof these components would be mainly due to fouling, which would also cause the inletgas temperature and pressure to rise, and hence these should be monitored.
The compressor performance would be reduced by fouling of the compressor wheeland diffuser. This fouling would also cause the delivery pressure to fall, whilst the turbocharger was maintaining a stable speed and all other parameters were normal. Hence thedelivery pressure of the compressor would be monitored.
The suction filter performance would reduce when fouling is present. This would bemonitored by measuring the pressure drop across the filter.The after cooler performance would reduce when fouling is present. This would bemonitored by measuring the air pressure drop across the cooler, and the temperatureof the cooling water.
The performance of the turbine is maintained by regular in-service cleaning,supplemented by manual cleaning of the turbocharger on a yearly operational runninghour routine. The in-service cleaning can be carried out using either dry cleaninginvolving dry particle cleaning, and/or water washing of the turbocharger using warmwater and air blast (only when the engine and turbocharger speed has been reduced). The in-servicecleaning should be carried out twice weekly, or at any stage the performanceof the turbine indicates a high rate of fouling.
The performance of the compressor is maintained by regular in-service cleaning,supplemented by manual cleaning of the compressor and diffuser on a yearlyoperational running hour routine. The in-service cleaning can be carried out using asmall quantity of warm water injected into the turbocharger suction housing at full turbocharger speed. This cleaning can be carried out twice weekly.

65
Q

what is supercharging?

A

Superchargingis the process of the increasing of the weight of the charged air by increasing the density of thecharged air. Turbochargingis one kind of supercharging by using exhaust gas turbocharger. In which the energy inthe exhaust gas expelled from the engine cylinder is utilized in driven in gas turbine, which isconnected to a centrifugal air blower and air is supplied to scavenge air trunk.

66
Q

what are the advantages and disadvantages of a constant pressure turbocharger system

A

Advantages and Disadvantages forConstant Pressure System

Advantages

1.Good performance in high load (Efficient when Bmep is above 8 bar)
2.More suitable for high output engine.
3.There is no need to group the cylinders exhaust into multiple of three. (Simple piping system)
4.No exhaust grouping
5.High turbine efficiency due to steady flow of exhaust.
6.The work transfer at the turbine wheel is smooth.
7.Reduction in SFOC (Specific Fuel Oil Consumption) of 5% – 7%

Disadvantages

1.When running at reduced speed and starting up low available energy at turbine. Thus itsupplies inadequately air quantity of the scavenge pressure necessary for efficientscavenging and combustion.
2.It require scavenge assistant (Auxiliary Blowers).
3.Poor response in changing load.

67
Q

describe the turbocharger pulse system?

A

Pulse System of Turbocharging
Makes full use of the higher pressure and temperature of the exhaust gas during the blowdown period
While rapidly opening the exhaust valves,exhaust gas leave the cylinder at high velocity as pressure energy is converted into kineticenergy to create the pressure wave or pulse in exhaust
These pressure waves or pulses are lead directly to the turbocharger
Exhaust pipe, so constructed in small diameter, is quickly pressurized and boosted up to formpressure pulse or wave
Pressure waves reach to turbine nozzles and further expansion takes place.

68
Q

what are the advantages and disadvantages of the turbocharger pulse system?

A

Advantages and Disadvantages of Pulse System

Advantages

1.At low load and low speed it is more efficient (Still efficient when Bmep is < 8 bar)
2.No need assistant of scavenge pump and blower at any load change.
3.It is highly response to change engine condition giving good performance of all speed ofengines.
4.High available energy at turbine
5.Good turbocharger acceleration

Disadvantages

1.The exhaust grouping is complicated.
2.Different sizes of exhaust pipes are needed for spare.
3.High pressure exhaust from one cylinder would pass back into another cylinder during thelow pressure scavenging period thus adversely effecting the combustion efficiency.

69
Q

how does turbocharger surging occur and what are the reason/causes?

A

Turbocharger Surging

When the discharge volute pressure exceed the pressure built up in the diffuser and theimpeller, it produces a back flow of air from discharge to suction and it is characterized by noise andvibration of turbocharger.

Causes of Turbocharger Surging
1.Suddenly load change by heavy sea
2.Scavenge space fire / Exhaust trunking fire
3.Poor power balance
4.Dirty nozzle and blades
5.Individual cylinder misfire
6.Chocked scavenge /exhaust ports
7.Incorrect matching of turbocharger to engine.
8.Poor scavenging or leaky exhaust valve

70
Q

types of turbocharger bearings?

A

Types of Turbocharger Bearings

Ball type bearing (rolling type)
These are used in turbocharger lube oil from the sumps onboth air and exhaust sides is sprayed onto the bearing by means of attached rotor drivengear type pumps.

Sleeve type bearings
These are lubricated by external L.O supply system.
By gravity from independent header tank situated about six meters above thebearings. The tank capacity must supply for about 15 minutes after engine is stopped or
From a main L.O pump lead to the bearings with a separate L.O pipe line. It has alsogravity tank in case of failure of L.O supply. (Under main engine L.O system)

71
Q

types of turbocharger lube oil system?

A

1.Own sump
2.External lube oil supply system

72
Q

Function of Labyrinth Seals?

A

The bearings are separated from the blower and turbine by labyrinth seals.
These seals aresealed by air supply from the discharge of blower to prevent oil entering the blower and to preventcontamination of the oil by the exhaust gas.
In case of defective labyrinth seals on blower side, oil is leaked into the air system the cooling surfaces are covered with oil which areinsulators and the cooling efficiency will be reduced.Also there will be deposits on the blower and the blower efficiency will be reduced.
In case of defective labyrinth seals on turbine side,the oil is leaked into the exhaust side and there will be carbon deposits on the nozzle andturbine blades.Reduce blower efficiency and fire in the exhaust piping. It will cause turbocharger surging.Oil will contaminate with exhaust gas.

73
Q

How will you know turbocharger air filter chocked ?

A

It can be known by comparing the manometer difference. If manometer difference is greaterthan normal, turbocharger air filter may be choke.
It can cause reduced engine power
Black smoke will emit from the funnel
Scavenge pressure will reduce

74
Q

Function of nozzle ring inturbocharger?

A

To change pressure energy to velocity (kinetic energy)

75
Q

Function of shroud ring inturbocharger?

A

Shroud ring is a component in turbochargers which forms a part of the inner exhaust gas casing adjacent to the turbine.
The area around the turbine is always in contact with highly corrosive exhaust gases. If no shroud ring is
fitted, the turbine inner casing will be slowly wasted and complete housing to be renewed for repair. Otherwise only shroud ring can be replaced with new one.
Minimize maintenance cost.
The radial clearance between turbine blades and shroud ring to be maintained within manufacture tolerance limits. This is very difficult in absence of shroud ring since casing can go for uneven wear.

76
Q

Purpose of inducer in turbochargers ?

A

To feed the shock less air flow to the impeller or
To guide the air smoothly into the eye of impeller

77
Q

Function of Diffuser inturbochargers?

A

To direct the air smoothly into volute casing
Convert kinetic energy to pressure energy inlet air

78
Q

What is K valueinturbochargers?

A

It is a distance between the rotor shaft end and the flange of bearing cover measured byblower side.

79
Q

Purpose of K valueinturbochargers?

A

To ensure that rotating impeller does not to touch the stationary blower casing cover in caseof thrust bearing worn out.

80
Q

How will you run engine in case ofturbocharger failure ?

A

Rotor to be blocked
Exhaust gas to be by-passed theturbocharger
Run engine with reduced speed with remainingturbocharger
Use Auxiliary Blower
Maintain all temperature and pressure of fuel, cooling water and lubrication within limit

81
Q

describe the scavenge port inspection procedure?

A

Scavenge inspection or scavenge port inspection refers to inspection of piston, piston rings, cylinder liner, etc. of the main propulsion engine through scavenge ports. This helps for detecting leakages from the piston and cylinder cover, if any. Jacket cooling water and lubricating oil pumps should be running during the scavenge port inspection. Scavenge inspection is carried out partly from under piston area and partly from scavenge air receiver.

Inspection procedure is following.

Make sure that vessel has necessary permission from port authorities or bridge for main engine immobilization.
Engage turning gear to main engine.
Remove scavenge port inspection covers and scavenge air receiver covers.

Scavenge Space Inspection

Ventilate and clean the area.
Turn the engine to bring the piston of the unit under inspection to BDC (Bottom Dead Centre).
Check for presence of any water or fuel on top of the piston, which indicate leakages.

Inspection of Piston Rings and Grooves

Check condition of cylinder liner wall through scavenge ports using mirror.
Slowly bring the piston up from BDC.
Inspect piston top land and piston skirt.
When piston rings are visible through scavenge ports, move piston up and down several times to ensure that rings are freely moving in the piston grooves.
Use a wooden stick and press the rings to ensure free movement of piston rings. Any broken piston rings can also be found by this way.
The first piston ring is normally CPR (Controlled Pressure Relief) type. In that case check that the CPR grooves are not clogged and gap is not enlarged.

CPR Piston Ring

Clearance between ring groove and rings can be measured and recorded.
Move the piston further upwards and check condition of piston rod.
Visually inspect the condition of stuffing box.

Flaps

Depend on the amount of sludge accumulated at the under piston area, the frequency of scavenge port inspection can be varied.

Air Cooler Mist Catcher

In the scavenge air receiver area, check for free movement of flap valves, auxiliary blower impeller, scavenge manifold relief valve, water accumulation near air cooler mist catcher, etc.

82
Q

what is a scavenge fire?

A

Carbonized lube oil, unburnt fuel oil and carbon from the residualproductsof the combustion spaces are accumulated in the scavenge spaces with the running of the engine. Under certain faulty running condition of the engine, these may ignite causing a fire in the enclosed scavenge space, known as scavenge fire.

83
Q

what are the causes of scavenge fire?

A

Causes of Scavenge Fire

1.Blow past of combustion productscaused by leaky, sticky or broken piston rings, worn out liner, faulty cylinder lubrication, or insufficient axial clearance of the piston rings.
2.Overheated piston dissipates heat to the under piston areacaused by faulty atomization and injection pressure, faulty fuel pump timing, loss of compression, engine overload, failure of coolant circulation or insufficient cooling due to formation of scale.
3.Blow back of exhaust gasescaused by exhaust back pressure or deposits on exhaust ports, fouling of grid before turbine inlet, fouling of turbine blades, choking of EGB or economiser gas outlet.
4.Presence of fuel oil in the scavenge spacesdue to defective fuel injectors, incorrect pressure setting of injectors or fuel particles landing on the cylinder liner due to excessive penetration.
5.Excessive cylinder lubrication which is drained down to scavenge spaces.
6.Oxygen is plenty during engine operation.
7.Fouled scavenge manifold.

84
Q

what are some indication of a scavenge fire?

A

Indication of Scavenge Fire

1.Engine revolution drops as the power generation in the affected cylinder is reduced.
2.Unstable operation of Turbo charger and may cause surging.
3.Exhaust temperature of the affected cylinder increases, as the cylinder is not receiving fresh air.
4.Black smoke with exhaust due to incomplete combustion in that unit.
5.Discharging of spark, flame or smokes through drain cocks from scavenge air boxes.
6.Rise of pressure and temperature of air in the air box below the piston.
7.Visible evidence of fire if a transparent window is fitted.
8.Cooling water outlet temperature of the affected unit is increased.

85
Q

what are some inspections made after a scavenge fire?

A

Inspection after Scavenge Fire
1.Intense fire can cause distortion and may upset piston alignment
2.Check by turning the engine and watch movement of piston in the liner, check for anyoccurrenceof binding at part of stroke (Binding indicates misalignment of piston)
3.Check spring on scavenge space relief device, if the device was near the set of fire
4.Piston rod packing spring also should be checked, which may have become weakened by overheating
5.Check piston rings and liner for any distortion or reddish burning mark
6.Checkdiaphragmand frame near affected part
7.Check guides and guide shoes
8.Check tension of tie bolts

86
Q

how to prevent scavenge fire?

A

Prevention of Scavenge Fire
1.Clean scavenge space and drain at regular intervals
2.Keep scavenge space drain open at regularintervals
3.Excess cylinder lubrication must be avoided
4.In case of timed lubrication, the time has to be checked as per PMS
5.Piston rings must be properly maintained and lubricatedadequately
6.Piston rod stuffing box must be maintained to prevent oil ingress in the scavenge space.
7.Prolong engine or any cylinder over loading to be avoided
8.Cylinder liner wear must be within admissible limits

87
Q

what are some scavenge space protection devices?

A

Scavenge Space Protection Devices

Electrical temperature sensing device fitted within the trunking, which will automatically sound an alarm in the event of excessive rise in local temperature.
Pressure relief valves consisting of self closing spring loaded valves are fitted and should be examined and tested periodically.
Fixed fire extinguishing system may be CO2, Dry Powder or Steam.

88
Q

what are common causes of why T/C is surging

A

The most common causes can be:

Rapid change of engine load – this often happens during bad weather when the vessel is pitching heavily and propeller comes out of the water and in this case the engine rpm must be reduced concomitantly with changing of vessel course in order to slow down the vessel pitching. Most of the engine governors have a rough sea mode that will slow the governor response in such cases in order to prevent turbo surging. Another reason of change in load can be a defective engine governor or high wear and lag in governor command link to the engine. This can be easily observed especially during good weather if sudden and frequent rpm change occurs in the engine.

Improper power distribution between engine cylinders. In this case one unit is producing more or less power than the others, thus leading to engine unbalance and variation on exhaust gas pressure. This is affecting mainly the impulse type turbochargers as the exhaust is pumped directly into the turbine. In order to remedy this issue a power card must be taken on the engine to determine and remedy the faulty cylinder. The fault in the cylinder may be: excessive wear of the cylinder, unit misfiring, leaking exhaust valve, improper adjusted valve timing and leaking injectors.

Fouled turbocharger parts like: dirty filters (can be observed visually or by checking the U-tube manometer installed on the compressor silencer), damaged silencer, dirty and clogged nozzle ring, dirty turbine impeller, worn out turbocharger’s bearings etc.

Dirty and clogged scavenging air cooler and/or water mist catcher prevents the air flow and creates back pressure into the compressor. This can be observed on the U-tube manometer installed on each scavenge air cooler. The value must be compared with the one’s from the engine shop trial at different loads. Hence the importance of having a fully functional U-tube manometer, although you can find plenty vessel where nobody pays attention to this. As a remedy the air cooler must be chemically cleaned, although this must be a frequent activity and part of the engine plan maintenance system.

Damaged or blocked scavenging air flaps.

Restriction in exhaust gas flow due fouling of economizer, nozzle ring dirty, obstruction of exhaust manifold, damage gratings inside exhaust manifold. As a remedy U-tube manometer readings on economizer must be checked and compared with the shop trial and economizer cleaned if necessary. Due nowadays engine slow steaming it is a good practice to soot blow the economizer twice a day using soot remover despite engine load, as long as the engine runs at constant rpm. Similarly, exhaust manifold must be inspected for any obstructions and gratings checked and repaired as found necessary.

Problems in engine fuel supply system like: leaking injectors, cold fuel which leads to improper injection, engine fuel starvation, seized or defective fuel injection pump etc. As a remedy fuel temperature must be checked and monitored and power card must be taken in order to check the performance of engine cylinders.

In the worst case scenario scavenge or exhaust fire.

in order to prevent turbocharger’s surging you need to follow the specific plan maintenance, to keep your filters clean, regularly chemically clean the scavenge air coolers, check the engine performance, clean and/or water wash the economizer regularly and inspect main engine units, scavenging space and exhaust manifold regularly.