Lecture-18 Prepared under QIP-CD Cell Project Internal Combustion Engines Ujjwal K Saha, Ph.D. Department of Mechanical Engineering Indian Institute of Technology Guwahati 1
Combustion in CI Engine Combustion in a CI engine is quite different from that of an SI engine. While combustion in an SI engine is essentially a flame front moving through a homogeneous mixture, combustion in a CI engine is an unsteady process occurring simultaneously in many spots in a very non-homogeneous mixture controlled by fuel injection. Air intake into the engine is unthrottled, with engine torque and power output controlled by the amount of fuel injected per cycle. 2
Only air is contained in the cylinder during compression stroke, and a much higher compression ratios (12 to 24) are used in CI engines. In addition to swirl and turbulence of the air, a high injection velocity is needed to spread the fuel throughout the cylinder and cause it to mix with the air. Fuel is injected into the cylinders late in the compression stroke by one or more injectors located in each cylinders. Injection time is usually about 20 0 of crankshaft rotation (15 0 btdc and 5 0 atdc). 3
Cylinder pressure as a function of crank angle for a CI engine. A : point of fuel injection B : point of ignition C : end of fuel injection AB : delay period 4
Combustion in CI Engine In a CI engine the fuel is sprayed directly into the cylinder and the fuel-air mixture ignites spontaneously. These photos are taken in a RCM under CI engine conditions with swirl air flow 1 cm 0.4 ms after ignition 3.2 ms after ignition 3.2 ms after ignition Late in combustion process 5
In Cylinder Measurements This graph shows the fuel injection flow rate, net heat release rate and cylinder pressure for a direct injection CI engine. Start of injection Start of combustion End of injection 6
Four Stages of Combustion in CI Engines Start of injection End of injecction -20-10 TC 10 20 30 7
Combustion in CI Engine The combustion process proceeds by the following stages: Ignition delay (ab) - fuel is injected directly into the cylinder towards the end of the compression stroke. The liquid fuel atomizes into small drops and penetrates into the combustion chamber. The fuel vaporizes and mixes with the hightemperature high-pressure air. Premixed combustion phase (bc) combustion of the fuel which has mixed with the air to within the flammability limits (air at high-temperature and high-pressure) during the ignition delay period occurs rapidly in a few crank angles. 8
Combustion in CI Engine contd. Mixing controlled combustion phase (cd) after premixed gas consumed, the burning rate is controlled by the rate at which mixture becomes available for burning. The rate of burning is controlled in this phase primarily by the fuel-air mixing process. Late combustion phase (de) heat release may proceed at a lower rate well into the expansion stroke (no additional fuel injected during this phase). Combustion of any unburned liquid fuel and soot is responsible for this. 9
CI Engine Types Two basic categories of CI engines: i) Direct-injection have a single open combustion chamber into which fuel is injected directly ii) Indirect-injection chamber is divided into two regions and the fuel is injected into the pre-chamber which is connected to the main chamber via a nozzle, or one or more orifices. 10
CI Engine Types contd. For very-large engines (stationary power generation) which operate at low engine speeds the time available for mixing is long so a direct injection quiescent chamber type is used (open or shallow bowl in piston). As engine size decreases and engine speed increases, increasing amounts of swirl are used to achieve fuel-air mixing (deep bowl in piston). For small high-speed engines used in automobiles chamber swirl is not sufficient, indirect injection is used where high swirl or turbulence is generated in the pre-chamber during compression and products/fuel blowdown and mix with main chamber air. 11
Types of CI Engines Glow plug Orifice -plate Direct injection: quiescent chamber Direct injection: swirl in chamber Indirect injection: turbulent and swirl pre-chamber 12
Direct Injection quiescent chamber Direct Injection multi-hole nozzle swirl in chamber Direct Injection single-hole nozzle swirl in chamber Indirect injection swirl pre-chamber 13
Combustion occurs throughout the chamber over a range of equivalence ratios dictated by the fuel-air mixing before and during the combustion phase. In general most of the combustion occurs under very rich conditions within the head of the jet, this produces a considerable amount of solid carbon (soot). Combustion Characteristics 14
Ignition Delay Ignition delay is defined as the time (or crank angle interval) from when the fuel injection starts to the onset of combustion. Both physical and chemical processes must take place before a significant fraction of the chemical energy of the injected liquid is released. Physical processes are fuel spray atomization, evaporation and mixing of fuel vapour with cylinder air. Good atomization requires high fuel-injection pressure, small injector hole diameter, optimum fuel viscosity, high cylinder pressure (large divergence angle). Rate of vaporization of the fuel droplets depends on droplet diameter, velocity, fuel volatility, pressure and temperature of the air. 15
Ignition Delay Physical processes are fuel spray atomization, evaporation and mixing of fuel vapour with cylinder air. Chemical processes similar to that described for auto-ignition phenomenon in premixed fuelair, only more complex since heterogeneous reactions (reactions occurring on the liquid fuel drop surface) also occur. 16
Fuel Ignition Quality The ignition characteristics of the fuel affect the ignition delay. The ignition quality of a fuel is defined by its cetane number CN. For low cetane fuels the ignition delay is long and most of the fuel is injected before autoignition and rapidly burns, under extreme cases this produces an audible knocking sound referred to as diesel knock. 17
Fuel Ignition Quality For high cetane fuels the ignition delay is short and very little fuel is injected before auto-ignition, the heat release rate is controlled by the rate of fuel injection and fuel-air mixing smoother engine operation. 18
Cetane Number The method used to determine the ignition quality in terms of CN is analogous to that used for determining the antiknock quality using the ON. The cetane number scale is defined by blends of two pure hydrocarbon reference fuels. By definition, isocetane (heptamethylnonane, HMN) has a cetane number of 15 and cetane (n-hexadecane, C 16 H 34 ) has a value of 100. 19
Cetane Number In the original procedures a- methylnaphtalene (C 11 H 10 ) with a cetane number of zero represented the bottom of the scale. This has since been replaced by HMN which is a more stable compound. The higher the CN the better the ignition quality, i.e., shorter ignition delay. 20
Cetane Number Measurement The method developed to measure CN uses a standardized single-cylinder engine with variable compression ratio The operating condition is: Inlet temperature ( o C) 65.6 Speed (rpm) 900 Spark advance ( o BTC) 13 Coolant temperature ( o C) 100 Injection pressure (MPa) 10.3 21
Cetane Number Measurement contd. With the engine running at these conditions on the test fuel, the compression ratio is varied until combustion starts at TC, ignition delay period of 13 o. The above procedure is repeated using blends of cetane and HMN. The blend that gives a 13 o ignition delay with the same compression ratio is used to calculate the test fuel cetane number. 22
Cetane vs Octane Number The octane number and cetane number of a fuel are inversely correlated. Gasoline is a poor diesel fuel and vice versa. 23
Factors Affecting Ignition Delay Injection timing At normal engine conditions the minimum delay occurs with the start of injection at about 10-15 BTC. The increase in the delay time with earlier or later injection timing occurs because of the air temperature and pressure during the delay period. Injection quantity For a CI engine the air is not throttled so the load is varied by changing the amount of fuel injected. 24
Factors Affecting Ignition Delay contd. Increasing the load (bmep) increases the residual gas and wall temperature which results in a higher charge temperature at injection which translates to a decrease in the ignition delay. Intake air temperature and pressure an increase in ether will result in a decrease in the ignition delay, an increase in the compression ratio has the same effect. 25
Factors Affecting Ignition Delay (gauge) 26
Factors Affecting Delay Period (DP) 1. Compression Ratio: DP decreases with increase of CR. 2. Engine Speed: DP decreases with increase of engine speed. 3. Power Output: DP decreases with increase of power output. 4. Fuel Atomization: DP decreases with fineness of atomization. 5. Fuel Quality: DP decreases with higher cetane number. 6. Intake Temp. & Pressure: DP decreases with increase of Temperature and pressure. 27
Effect of Ignition Delay 28
Knock in CI Engines Knock in SI and CI engines are fundamentally similar. In SI engines, it occurs near the end of combustion; whereas in CI engines, it occurs near the beginning of combustion. Knock in CI engines is related to delay period. When DP is longer, there will be more and more accumulation of fuel droplets in combustion chamber. This leads to a too rapid a pressure rise due to ignition, resulting in jamming of forces against the piston and rough engine operation. When the DP is too long, the rate of pressure rise is almost instantaneous with more accumulation of fuel. 29
Knock in SI and CI Engines 30
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