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Wankel Engines Project Report edited .pdf - 123SeminarsOnly

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vicinity of top dead center in the compression stroke, and affect the quantity of mixture<br />

existing in the direction of flame propagation. The higher combustion speed is preferable, in<br />

principle, from the viewpoints of output performance and thermal efficiency. On the other<br />

hand, however, if it is made excessively higher, problems such as misfiring in light-load<br />

operation, and knocking in heavyload operation, etc. will occur. For automobile engines to be<br />

operated over a wide range of loads and revolutions, the rotor recess is selected for a<br />

maximum possible combustion speed without disturbing driveability.<br />

LOCATION AND CONFIGURATION OF ROTOR RECESS<br />

(1) LOCATION OF ROTOR RECESS<br />

The location of the rotor recess closer to the leading side can provide a higher burning<br />

speed when the configuration and volume of the rotor recess are the same. This is because<br />

of the geometrical effect of a greater amount of mixture existing in the leading side where<br />

flame propagation is faster and the squish flow more intensive. The squish flow will become<br />

more intensive when a greater pressure difference is caused between the trailing side in<br />

higher pressure under high compression and the leading side in relatively reduced pressure.<br />

(2) CONFIGURATION OF ROTOR RECESS<br />

When the volume and location of the rotor recess are the same, the squish flow will be more<br />

intensive for the rotor with a shallower recess near the minor axis when the rotor is in the<br />

vicinity of top dead center. This is because the passage area becomes smaller and the<br />

pressure difference between the trailing and leading sides becomes greater.<br />

The cross-section of the rotor recess in an adequate depth to the flame surface profile is<br />

preferred to that in smaller depth and wider width to provide a greater flame surface area.<br />

Further, for efficient burning inside the rotor recess, a configuration that provides a smooth<br />

squish flow is required. The above concept is called the LDR (Leading Deep Recess) rotor<br />

which provides a rotor recess that is deeper on the leading side. Fig. 30 shows a comparison<br />

of burning speeds between the LDR rotor and the MDR (Medium Deep Recess) rotor that<br />

has a volumetric center on its center. Fig. 31 through 32 show comparisons of specific fuel<br />

consumption, performance at W.O.T. and emission of exhaust gas.<br />

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