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Design and Simulation of Two Stroke Engines

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<strong>Design</strong> <strong>and</strong> <strong>Simulation</strong> <strong>of</strong> <strong>Two</strong>-<strong>Stroke</strong> <strong>Engines</strong><br />

The terms for bore, stroke, con-rod length <strong>and</strong> engine speed, i.e., BO, ST, CRL <strong>and</strong> RPM<br />

are self-explanatory <strong>and</strong>, as with all <strong>of</strong> the units in the programs, they are in mm dimensions<br />

unless otherwise stated.<br />

The trapped compression ratio is TCR; the number <strong>of</strong> cylinders <strong>of</strong> the engine is NC Y; the<br />

bmep expected at the RPM is BMEP in bar units.<br />

The exhaust ports <strong>and</strong> transfer ports open at EPO <strong>and</strong> TPO °atdc, respectively; the subtended<br />

port angles, 9p, <strong>of</strong> the exhaust ports is EXANG; the radial thickness <strong>of</strong> the cylinder<br />

liner in the scavenge port belt is LINER.<br />

The chordal values <strong>of</strong> the bars <strong>of</strong> the exhaust <strong>and</strong> scavenge (transfer) ports, Xb, are EBAR<br />

<strong>and</strong> TB AR, while that for the bar between the last exhaust port <strong>and</strong> the first scavenge port is<br />

coded as ETBAR, respectively. The value <strong>of</strong> FOCUS is the proportion <strong>of</strong> the cylinder radius,<br />

from the cylinder center to the edge <strong>of</strong> the bore on the scavenge side, where the guiding edges<br />

<strong>of</strong> the main scavenge ports index the centerline. The guiding edges in question are the trailing<br />

edges <strong>of</strong> the first port, <strong>and</strong> the leading edge <strong>of</strong> the second backswept port. This is shown even<br />

more clearly in Fig. 3.40, where they are reproduced in the same manner as the screen display<br />

<strong>of</strong> the computer program. The side port is at right angles to the line <strong>of</strong> symmetry <strong>and</strong> the back<br />

ports are aligned with it, facing the exhaust port. Naturally, it is essential in this design configuration<br />

to elevate the back ports, usually by 50-60°. To allow the designer this flexibility,<br />

both the side <strong>and</strong> the back ports can be elevated by setting angles SUP <strong>and</strong> BUP between 0<br />

<strong>and</strong> (a maximum <strong>of</strong>) 60°.<br />

The plan radius <strong>of</strong> a recessed cylinder bowl in the fashion <strong>of</strong> a DI diesel engine is RBOWL;<br />

the corner radius <strong>of</strong> that bowl is RCV; the squish clearance, the piston lengths to crown <strong>and</strong><br />

skirt, <strong>and</strong> the gudgeon pin <strong>of</strong>fset (+ in direction <strong>of</strong> rotation) are shown coded as SQCL, GPC,<br />

GPS <strong>and</strong> GPOFF, respectively.<br />

The port corner radii, rc, are presented as RTE, RBE, RTT <strong>and</strong> RBT, the top <strong>and</strong> bottom<br />

corner radii <strong>of</strong> the exhaust <strong>and</strong> scavenge (transfer) ports, respectively.<br />

The output data are also fairly self-explanatory. However, each line shows: the engine<br />

total swept volume (cm 3 ) <strong>and</strong> power (kW); the mean widths <strong>of</strong> all <strong>of</strong> the exhaust <strong>and</strong> scavenge<br />

ports; the port width ratio CA; the areas Axp <strong>and</strong> Asp <strong>of</strong> the exhaust ports <strong>and</strong> scavenge<br />

ports, respectively; the exhaust pipe area <strong>and</strong> its diameter; the blowdown, exhaust <strong>and</strong> transfer<br />

port time areas <strong>of</strong> those ports (vide Sec. 6.1); the blowdown, exhaust <strong>and</strong> transfer port time<br />

areas <strong>of</strong> those ports (vide Sec. 6.1); the combustion chamber clearance volume (cm 3 ) <strong>and</strong> the<br />

depth <strong>of</strong> that chamber; the heights, hx <strong>and</strong> hs, <strong>of</strong> the exhaust ports <strong>and</strong> scavenge ports, respectively;<br />

the subtended port angles, 6p, <strong>of</strong> each <strong>of</strong> the scavenge ports for they are specifically<br />

designed to be identical; the subtended angles, 0b, <strong>of</strong> each <strong>of</strong> the bars <strong>of</strong> the exhaust ports,<br />

between the exhaust <strong>and</strong> the scavenge ports, <strong>and</strong> between each <strong>of</strong> the scavenge ports, respectively;<br />

the slopes (deg) <strong>of</strong> each <strong>of</strong> the focusing edges <strong>of</strong> the main scavenge ports with respect<br />

to the "horizontal" centerline <strong>of</strong> scavenge symmetry.<br />

A change <strong>of</strong> data is invited by the program for any or all <strong>of</strong> the input data, as is their<br />

recomputation. The code for that data change is the name <strong>of</strong> that particular input data parameter,<br />

to be typed in by the user. A hard copy, i.e., a printout, is available <strong>of</strong> the entire screen<br />

display, <strong>and</strong> this is drawn to scale from the input <strong>and</strong> output data. The "by eye" design process<br />

is aided by the computer program immediately drawing the sketch <strong>of</strong> the piston <strong>and</strong> the porting<br />

to scale on the computer screen as a function <strong>of</strong> the input data.<br />

272

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