combustion process in si engines - National Institute of Technology
combustion process in si engines - National Institute of Technology
combustion process in si engines - National Institute of Technology
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INTERNAL COMBUSTION ENGINES (ELECTIVE) (ME667)<br />
SIXTH SEMESTER<br />
EFFECT OF DETONATION (VTU Jan 2006)<br />
The harmful effects <strong>of</strong> detonation are as follows:<br />
1. Noise and Roughness. Knock<strong>in</strong>g produces a loud pulsat<strong>in</strong>g noise and pressure<br />
waves. These waves which vibrates back and forth across the cyl<strong>in</strong>der. The presence <strong>of</strong><br />
vibratory motion causes crankshaft vibrations and the eng<strong>in</strong>e runs rough.<br />
2. Mechanical Damage.<br />
(a)High pressure waves generated dur<strong>in</strong>g knock<strong>in</strong>g can <strong>in</strong>crease rate <strong>of</strong> wear <strong>of</strong> parts<br />
<strong>of</strong> <strong>combustion</strong> chamber. Sever ero<strong>si</strong>on <strong>of</strong> piston crown( <strong>in</strong> a manner <strong>si</strong>milar to that <strong>of</strong><br />
mar<strong>in</strong>e propeller blades by cavitation),<br />
cyl<strong>in</strong>der head and pitt<strong>in</strong>g <strong>of</strong> <strong>in</strong>let and outlet<br />
valves may result <strong>in</strong> complete wreckage <strong>of</strong> the eng<strong>in</strong>e.<br />
(b) Detonation is very dangerous <strong>in</strong> eng<strong>in</strong>es hav<strong>in</strong>g high noise level. In small eng<strong>in</strong>es<br />
the knock<strong>in</strong>g noise is ea<strong>si</strong>ly detected and the corrective measures can be taken but <strong>in</strong><br />
aero-eng<strong>in</strong>es eng<strong>in</strong>es it is difficult to detect knock<strong>in</strong>g noise and hence corrective measures<br />
cannot be taken. Hence severe detonation may per<strong>si</strong>st for a long time which may<br />
ultimately result <strong>in</strong> complete wreckage <strong>of</strong> the piston.<br />
3. . Carbon depo<strong>si</strong>ts. . Detonation results <strong>in</strong> <strong>in</strong>creased carbon depo<strong>si</strong>ts.<br />
4. Increase <strong>in</strong> heat transfer. . Knock<strong>in</strong>g is accompanied by an <strong>in</strong>crease <strong>in</strong> the rate <strong>of</strong> heat<br />
transfer to the <strong>combustion</strong> chamber walls.<br />
The <strong>in</strong>crease <strong>in</strong> heat transfer is due to two reasons.<br />
• The m<strong>in</strong>or reason is that the maximum temperature <strong>in</strong> a detonat<strong>in</strong>g eng<strong>in</strong>e is<br />
about 150°C higher than <strong>in</strong> a non-detonat<strong>in</strong>g eng<strong>in</strong>e, due to rapid completion <strong>of</strong><br />
<strong>combustion</strong><br />
• The major reason for <strong>in</strong>creased heat transfer is the t<br />
scour<strong>in</strong>g away <strong>of</strong> protective<br />
layer <strong>of</strong> <strong>in</strong>active stagnant gas on the cyl<strong>in</strong>der walls due to pressure waves. The<br />
<strong>in</strong>active layer <strong>of</strong> gas normally reduces the heat transfer by protect<strong>in</strong>g the<br />
<strong>combustion</strong> and piston crown from direct contact with flame.<br />
5. Decrease <strong>in</strong> power output and efficiency. . Due to <strong>in</strong>crease <strong>in</strong> the rate <strong>of</strong> heat transfer<br />
the power output as well as efficiency <strong>of</strong> a detonat<strong>in</strong>g eng<strong>in</strong>e decreases.<br />
Jagadeesha T, As<strong>si</strong>stant Pr<strong>of</strong>essor, Department <strong>of</strong> Mechanical Eng<strong>in</strong>eer<strong>in</strong>g, Adichunchanagiri <strong>Institute</strong> <strong>of</strong> <strong>Technology</strong>, Chikmagalur