Showing posts with label compression ignition engines ppt. Show all posts
Showing posts with label compression ignition engines ppt. Show all posts

Saturday, 21 November 2015

Compression Ignition Engines PPT

Abnormal Combustion

Delay period:

  Delay period is the time interval (measured in milliseconds) 
between the commencement of fuel injection and the beginning of 
ignition and combustion. The start of combustion is indicated 
by the deviation of point of the pressure curve above the normal 
compression pressure. In practice, this actual time is as low as 
0.006 seconds. The delay period consists of the following:

-  Physical delay period.


-  Chemical delay period

Factors influencing delay period:

 1.  Characteristics of fuel (self-ignition temperature,
        volatility and viscosity).
 2.  Temperature and pressure of compressed air.
 3.  Degree of atomization of injected fuel.
 4.  Air motion / turbulence present in the combustion
       space.

 5.  Engine speed.

 6.  Injection timing.

 7.  Characteristics of the combustion chamber.


Factors affecting knock

Knocking 

   Knocking is violet gas vibration and  audible sound produced by extreme  pressure differentials leading to the very rapid rise during the early part of uncontrolled second phase of combustion.Delay period is directly related to Knocking in CI engine. An extensive delay period can be due to following factors:

    •  A low compression ratio permitting only a 
marginal self -ignition temperature to be 
reached.
   •  A low combustion pressure due to worn out piston, rings and bad valves
   •  Low cetane number of fuel
   •  Poorly atomized fuel spray preventing
      early combustion and
     Coarse droplet formation due to malfunctioning of injector parts like spring
   •  Low intake temperature and pressure of 
      air 

METHODS OF CONTROLING DIESEL KNOCK

    We have discussed the factors which are 
responsible for the detonation in the previous 
sections. If these factors are controlled, then the 
detonation can be avoided.

     Using a better fuel. Higher CN fuel has lower delay 
period and reduces knocking tendency.

     Controlling the Rate of Fuel Supply. By injecting
 less fuel in the beginning andthen more fuel amount
 in the combustion chamber detonation can be 
controlled to a certain extent. Cam shape of suitable
 profile can be designed for this purpose. 

 Knock reducing fuel injector: 
This type of injector avoid the sudden increase in 
pressure inside the combustion chamber because 
of accumulated fuel. This can be done by 
arranging the injector so that only small amount
 of fuel is injected first. This can be achieved by
 using two or more injectors arranging in out of
 phase.

  By using Ignition accelerators : 
C N number can be increased by adding chemical
 called dopes. The two chemical dopes are used 
are ethyl-nitrate andamyle –nitrate in  concentration of 
8.8 gm/Litre and 7.7 gm/Litre. But these two 
increase the NOx emissions.

Increasing Swirl : Knocking can be greatly
 reduced by increasing swirl ( or reducing
 turbulence). Swirl helps in knock free 
combustion.

Injection systems :
Direct – Injection systems:
      In largest size engines, where mixing rate 
requirement are lease stringent, quiescent direct – 
injection systems of the type are used. The momentum 
and energy of the injected fuel jets are sufficient to 
achieve adequate fuel distribution and rates of mixing 
with the air. Additional organized air motion is not 
required. The combustion chamber shape is usually a 
shallow bowl in the crown of the piston, and a 
central multi hole injector is used. 





Advanced IC engines notes PPT



Anna University- Chennai
Department of Mechanical Engineering

Subject : Advanced IC Engines




This post is useful for the students from Mechanical Engineering for the subject of Advanced IC engines as well as for IC Engines if you go to higher study.




The following images covers the Compression ignition engines which is the second unit of Advanced IC engines.



The following contents about the CI engines were discussed from the following images. Make download for your reference which will be more useful for understanding the concepts of Compression Ignition Engines.

UNIT 2


COMPRESSION IGNITION ENGINES



CONTENTS
- Stages of combustion-normal and abnormal combustion
-Direct and Indirect injection systems
-Turbocharger
-Factors afecting knock

-Thermodynamic analysis of CI Engine combustion process.


STAGES OF COMBUSTION:
  •    Stages of combustion can be divided into four stages namely,
  • —  Pre-flame combustion
  • —  Uncontrolled combustion
  • —  Controlled combustion and
  • —  After burning






   Pre-flame combustion
  •    At the beginning of pre-flame combustion, the energy release rate is very less than rate of heat absorption by the fuel because the amount of fuel vapour is small. As a result, the pressure in the cylinder decreases with the progressive fuel vaporization. 
  •     This decrease in pressure attains a maximum value when the energy release due to pre-flame reaction is equal to the rate of heat absorption by the fuel. This process of fuel vaporization and subsequent decrease in pressure in the cylinder is shown on fig by paths ‘ab’.


Uncontrolled combustion:
    A considerable amount of fuel is accumulated in the combustion chamber during the relay period (time between the start of injection of fuel and start of ignition of fuel).


    This accumulated fuel burns very rapidly causing a steep raise in the cylinder pressure. The rate of pressure raise increases with the increase in delay period because of the amount of fuel taking part in this combustion increase with an increasing delay period.

    This phase of combustion causing rapid pressure raise in the cylinder is known as “period of uncontrolled combustion”.
      
Controlled combustion

   All the accumulated fuel during the delay period generally burns during the period of controlled combustion. The fuel injected after this (after point d) burns at the same rate at which it is injected because, the vaporisation of fuel, mixing with the air and burning takes place almost instantaneously as the fuel leaves the nozzle.

   This is because, the temperature and pressure inside the cylinder are sufficiently high and sufficient turbulence is created due to precious burning, thus the delay period for the fuel injected after point “d” is almost zero. This period of combustion is known as “controlled combustion” because the rate of burning can be controlled by controlling the rate of injection. 

  After burning:

   The thermal decomposition of the part of fuel takes place during uncontrolled and controlled combustion. 

  The decomposed fuel molecules contain enough number of hydrocarbons and carbon particles which has lower reaction rates. 

  Some carbon and hydro carbon, decomposed from fuel are left in the combustion product because the rate of decomposition during uncontrolled and controlled combustion is more than the rate of reaction of these molecules during that period. 

   These unburned hydrocarbons and carbon generally burn after stopping the fuel injection during the expansion stroke. This process of combustion of decomposed carbon atoms is known as “after burning”.










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