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Compare the below SI vs CI tutorials and list down differences Both the cases are ran at 1800 RPM SL. No. Characteristics SI engine CI engine 1 Thermodynamic cycle OTTO cycle Diesel and duel combustion cycle 2 Combustion Spark ignition Compression ignition 3 Governing (Load and speed control) Quantity governed by throttling;…
Tilak S
updated on 19 Nov 2019
Compare the below SI vs CI tutorials and list down differences
Both the cases are ran at 1800 RPM
SL. No. |
Characteristics |
SI engine |
CI engine |
1 |
Thermodynamic cycle |
OTTO cycle |
Diesel and duel combustion cycle |
2 |
Combustion |
Spark ignition |
Compression ignition |
3 |
Governing (Load and speed control) |
Quantity governed by throttling; Almost constant A/F ratio. |
By rack, quality governing, air
|
4 |
Compression ratio |
6-11, restricted by detonation (average 7-9) |
13-22 (average 15-18) Higher CR reduces knocking. Restricted by mechanical and thermal stresses. |
5 |
Operating pressures
(a) Compression pressure (b) Max. pressure (c) Operating speed |
7 to 15 bar 45 to 50 bar Max. 10 bar |
30 to 50 bar 60 to 70 bar Max. 20 bar |
6 |
(a)Operating Speed
(b) Piston speed |
High speed (2000-6000 rpm)
High 16 m/s |
Low sped (4000 rpm) medium speed (400-1200), high speed (1200-3500) up to 11 m/s |
7 |
Distribution of fuel |
A/F ratio is not optimum in multicylinder engines |
Excellent distribution of fuel in multicylinder engines |
8 |
Supercharging |
Limited by detonation, used only in aircraft engine |
Inherently suitable, widely used. Limited by blower power and mechanical and thermal stresses. |
9 |
Exhaust gas temperature |
High, due to low thermal efficiency |
Low, due to high thermal efficiency |
10 |
Starting |
Easy, low cranking effort |
Difficult, high cranking effort |
11 |
Weight per unit power |
Low (0.5 to 4.5 kg/kW) |
High (3.3 to 13.5 kg/kW) |
12 |
Power per unit displacement |
High (30 kW/liter) |
Low (15 kW/liter) |
13 |
Acceleration |
Not so good, but compensated by acceleration pump |
Good |
14 |
Reliability |
Good, normal troubles in carburetor and ignition system |
Good, greater reserve of power, rated by smoke, not max. power, normal trouble in injection and generating systems |
15 |
(a) Specific fuel consumption
(b) Fuel economy
@Full load @Part load |
Full load low, worse at part load and idling Costly fuel, density low, a calorific value slightly higher, fewer calories per liter
Medium Poor |
Full load better, part load much better than SI as no throttling Cheaper fuel, density high„ calorific value slightly low, more calories per liter
Good Good |
16 |
Fuel safety. (fire hazard) |
Volatile fuel, more fire hazard |
Less volatile, less fire hazard |
17 |
(a) Initial, capital cost
(b) Running cost |
Low
High |
High due to heavyweight and sturdy construction, costly construction, 1.25 - 1.5 times.
Low
|
18 |
Operating life |
Less |
More due to sturdy construction. Rating lower than maxi-mum power |
19 |
Maintenance cost |
Minor maintenance compared to CI |
Major overall maintenance required less frequently |
20 |
Noise and vibration |
Less |
More idle noise is a major problem |
21 |
Odour and smoke |
Less objectionable
|
More objectionable |
22 |
Two-stroke operation |
Less suitable, fuel loss in scavenging |
More suitable, no fuel loss in scavenging |
23 |
Applications |
Passenger cars, small mobile applications aircrafts. Two stroke engine scooters, motorcycle mopeds due to cheaper and simpler engine. |
Buses, trucks, locomotives, stationary generating plants. Heavy duty equipment like tractors, earthmoving machinery; ships |
24 |
Combustion problem |
Knock in unburnt mixture. |
Diesel knock caused by long delay. |
25 |
Fuel |
Petrol high octane number, high self-ignition temperature |
High cetane number, low self-ignition temperature |
26 |
Air-fuel ratio |
10 to 17 |
18 to 100 |
27 |
Fuel supply method |
Carburettor(cheap), Port fuel injection and direct injection. |
Expensive; fuel pump and fuel injectors. |
28 |
Very high power |
NO |
Yes |
The SI engine tutorial was run at 1800 RPM. Hence in order to compare the important parameters, the CI engine tutorial is also run at 1800 RPM as shown below
In-cylinder pressure:
Cylinder Pressure is the pressure in the engine cylinder during the 4 strokes of engine operation (intake, compression, combustion and expansion, and exhaust). Pressure during expansion is the most important because that is the cylinder pressure pushing on the piston to produce power.
in cylinder pressure vs crank angle degree plot:
For SI engine
For CI engine
The Diesel engines always generate high cylinder pressure due to the high compression ratio.
Airflow rate:
The airflow rate is the mass of the air entering into the engine cylinder during the intake process. The airflow rate of our engine is shown in the tabular column below:
For SI engine: For CI engine
A/F ratio of SI engine: Stoichimoteric mixture(14.5 )
A/F ratio of CI engine: Lean mixture(19.18)
Since CI engine operates lean the airflow rate is high (82.8 kg/h) for CI engine when compared to SI engine.
Mean Effective Pressures(MEP):
It is an average pressure acting on the piston during the complete thermodynamic cycle in a Reciprocating internal combustion engine.
The different Mean Effective Pressures of our engines are listed below and the values are tabulated.
For SI engine:
For CI engine:
It can be clearly seen from the above two tables that Ci engines are high power engines thus generating more BMEP and torque
Brake Specific Fuel Consumption(BFSC):
Brake-specific fuel consumption (BSFC) is a measure of the fuel efficiency of any prime mover that burns fuel and produces rotational or shaft power. It is typically used for comparing the efficiency of internal combustion engines with a shaft output. It is the rate of fuel consumption divided by the power produced.
For SI engine: For CI engine
Since CI engines are leanly burned less fuel is consumed for combustion thus resulting in low BSFC(221.3 g/kW-hr) when compared with the SI engine (244.2 g/kW-hr).
SI Engine CI engine
Exhaust Temperature:
Exhaust temperature is the temperature transferred to the engine's exhaust components by the burnt gases escaping from the engine.
Gasoline's chemical structure is not as heavy as diesel's structure, resulting in a fuel that burns at a lower temperature range. In the end, the exhaust temperature from gasoline combustion is only between 700 and 1,100 degrees Fahrenheit.
In contrast, the heavy molecular structure of diesel fuel requires more heat to trigger combustion within the engine chamber. As a result, the exhaust temperatures emitted are particularly higher than gasoline, ranging from 1,000 to 1,200 degrees Fahrenheit.
Diesel engine exhaust gases vary with speed and load. High loads and high speeds result in the highest temperatures. Generally, temperatures of 500 to 700 °C (932 to 1,293 °F) are produced in the exhaust gases from diesel-cycle engines at 100 percent load, to 200 to 300 °C (392 to 572 °F) with no load.
Below contour map shows the exhaust system temperatures in degree celsius
A/F ratios
Air–fuel ratio (AFR) is the mass ratio of air to a solid, liquid, or gaseous fuel present in a combustion process.
In petrol engines, the air-fuel ratio varies from 8 to 15. At slow speeds, rich mixtures will be formed around 7 to 9 AFR. in the economy range, the stoichiometric air-fuel ratio will be around 15 which is the highest for forming a lean mixture. That's why we get more mileage in the economy range. Again if we increase speed, the AFR ranges about 9–12 for running the engine at high speed.
In diesel engines, due to direct injection, only air will be entering the cylinder in the first stroke. So we always get leaner mixtures compared to the SI engine. Generally, it will be around 14–15 for rich mixtures and goes up to 70 for lean mixtures. This depends on our throttle input.
For SI engine: For CI engine
A/F ratio of SI engine: Stoichimoteric mixture(14.5 )
A/F ratio of CI engine: Lean mixture(19.18)
Change MFB 50 and observe the impact on performance:
Combustion control has always been a key factor in modern Internal Combustion Engines management systems, being even more crucial nowadays to improve drivability and reduce pollutant emissions. The position where 50% of fuel mass burned over an engine cycle is reached (MFB50) provides very important information about the effectiveness of combustion, such as the kind of combustion that is taking place.
Three cases were run for different percentages of the main duration in the combustion.
Case 1: MFB50 = 30 CAD
Case 2: MFB50 = 35 CAD
Case 3: MFB50 = 40 CAD
Case 1:
Case 2:
Case 3:
From the above tables following conclusions are drawn:
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