Operational Theory

The Actual Diesel Engine Cycle

 

 

The ideal cycles are theoretical only, and do not show what actually happens inside the cylinder of a large marine diesel engine.

 

For simplicity and because of its close relationship with the ideal cycles, the following describes a two stroke cycle:

 

 

Starting at bottom dead centre, the exhaust valve is open and the scavenge ports are uncovered. Air is flowing into the cylinder, pushing out or "scavenging" the remaining exhaust gas.

 

As the piston moves up the cylinder, the scavenge ports are closed off by the piston. The angle at which this occurs varies but is about 140 BTDC. (Before Top Dead Centre).

 

The exhaust valve then closes. Again this angle is variable but is about 120 BTDC.

 

Compression now starts. However it is not adiabatic, where no heat is gained and lost to the liner, piston and cylinder head but polytropic (literally, many temperatures). The index of compression, 'n' is variable but for this example is taken as 1.35.

 

Although the air inlet to the engine is maintained at about 45 -50, The air inside the cylinder will have gained heat from the surroundings when the engine is at operating temperature, and at the start of compression is about 75.

 

At about 6 BTDC, fuel injection will commence, and will continue through untill about 10 ATDC (After Top Dead Centre), depending on engine load..

 

The fuel will heat up and start to burn just as the piston comes over TDC (Top Dead Centre). Pressure will rise in the cylinder quickly, reaching a maximum at between 12 and 15 ATDC. The piston is driven down by the rapidly expanding gases, converting the energy in the burning fuel into work.

 

The length of time the fuel burns for again is variable. For this model it is until 33 ATDC when expansion again follows a polytropic curve with the index 'n' here set at 1.23.

 

The pressure then drops in the cylinder as the piston moves down the cylinder until the exhaust valve opens (120ATDC), when the pressure is about 9 bar.

 

During exhaust blowdown, pressure drops rapidly in the cylinder until the scavenge ports open (140 ATDC) and the pressure drops to scavenge pressure.

 

Note pressures quoted are absolute: i.e gauge pressure + atmospheric pressure (1bar).

 

It is possible to model the cycle on a spreadsheet, and to calculate the Mean Indicated Pressure (MIP), Indicated Work and Indicated Power (IP).

 

Because the diagram is a pV curve, the area  enclosed by the diagram is indicative of the work done during the cycle. To calculate the area of the diagram, I subtracted the area under the compression line (i.e BDC - TDC) from the area under the epansion line (i.e TDC - BDC). The area under the polytropic compression and expansion curve are easily calculated because they follow the law pVn=C. Although there is no set equation for the fuel burning curve or the exhaust blowdown curve, the Exel spreadsheet calculated equations which gave a good representation. By integrating the equation between the required values it was possible to calculate the area (and therefore the work done) under those curves. The results can be seen in the table on the diagram.

 

If the work done per cycle (revolution) is divided by the swept volume then the Mean Indicated Pressure is obtained. In this case it is just over 16.3 bar. When calculating the Indicated Power for a cylinder on an actual engine, it is the Mean Indicated Pressure that needs to be obtained from the indicator diagram. If the Mean Indicated Pressure is multiplied by the swept volume of the cylinder (a known quantity), then the work done/cycle is obtained.

 

As stated earlier, the air in the cylinder is about 75C at start of compression. The temperature at the start of fuel injection can be calculated using PV/T = Constant. This gives a temperature of 593 at 6 BTDC and 611 at TDC. The temperature rises rapidly during combustion to about 1500C depending on the type of fuel.

 

Because the piston displacement is very small per degree of crank angle around BDC and TDC, and largest at about 70ATDC (see Piston displacement page) the indicator diagram is different from the one obtained when using crank angle on the x axis

The crank angle/pressure diagram is often used by computer packages which calculate the MIP and IP by measuring the pressure in the engine cylinders using a pressure transducer, whilst at the same time measuring the crank angle using a pick up on the flywheel. However these diagrams tend to measure the crank angle from 0 - 360 and so look like the diagram below.

 

For examples of these computer drawn indicator cards go to the members section.

 

 

Because the computer program will have been programmed with the engine bore, stroke and conrod length, it can calculate the MIP and IP from the pressure recorded for each crank angle, which it measures every 0.25.

 

 

Another diagram which can be drawn is the out of phase diagram. In this the crank angle is offset by 90

 

 

If the volume on the x axis is moved 90 out of phase with the pressure, (so that at the pressure reached at TDC, the volume is recorded as that at 90 ATDC, when the piston has reached 90ATDC the volume is recorded as that at BDC, and when the piston has reached BDC the volume is recorded as that of 90ABDC etc), this will amplify in a horizontal plane what is happening to the pressure in the cylinder allowing faults to be diagnosed.

 

IN THE MEMBERS SECTION:

 

Power Cards: What they are and how to interpret them.

Out of phase and draw cards: What they are, and how to take them.

Procedure for taking indicator cards.

Computer derived indicator cards.

The light spring diagram: What it is, and faults that it shows.

Faults with indicator diagrams

The difference between Mean Indicated Pressure (MIP) and Mean Effective Pressure (MEP).

How to balance an engine using peak pressures.

Other methods of assessing engine power: Manufacturers Graph,Water Brake, Torsionmeter

Downloadable spreadsheets for piston position, velocity and acceleration.

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