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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 />

where the parameter, I, is the second moment <strong>of</strong> area given in Eq. 5.2.16. The maximum tip<br />

lift ratio, CrCjt, for this empirical calculation is then:<br />

r - Xti P<br />

c rdt - — (6.3.7)<br />

Consequently, for implementation in Eq. 6.3.1, the time area <strong>of</strong> the reeds, for a number <strong>of</strong><br />

reeds, nr, is given by:<br />

j A d e ^ " ^ ^ m 2 deg (6.3.8)<br />

where 6p can been assigned a value <strong>of</strong> 200° for the isosceles triangle <strong>of</strong> lift to xtjp.<br />

The above equations, referring to a combination <strong>of</strong> time areas <strong>and</strong> the mechanics <strong>of</strong> reed<br />

lift, i.e., Eqs. 6.3.1-6.3.8, should be strictly carried out in SI units, or arithmetic inaccuracies<br />

will be the inevitable consequence.<br />

The last geometrical dimension to be calculated is the stop-plate radius which should not<br />

permit the tip <strong>of</strong> the reed to move past a Crcjt value <strong>of</strong> 0.3, but should allow the reed petal to be<br />

tangential to it should that lift actually occur. That a lift limit for Crcjt <strong>of</strong> 0.3 is realistic is seen<br />

in Fig. 5.35 for a racing engine. This relationship is represented by the following trigonometrical<br />

analysis, where the normal limit criterion is for a tip lift ratio <strong>of</strong> 0.3:<br />

(l-C?dt)Lr<br />

r sP = 9r (6-3.9)<br />

6.3.3 The design process programmed into a package, Prog.6.4<br />

This calculation is not as convenient to carry out with an electronic calculator as that for<br />

the expansion chamber, as a considerable number <strong>of</strong> cycles <strong>of</strong> estimation <strong>and</strong> recalculation<br />

are required before a matched design emerges. Therefore, a computer program has been added<br />

to those presented <strong>and</strong> available from SAE, Prog.6.4, REED VALVE DESIGN. This interactive<br />

program has a screen output which shows a plan <strong>and</strong> elevation view to scale <strong>of</strong> the reed<br />

block <strong>and</strong> reed petal under design consideration. A typical example is that illustrated in Fig.<br />

6.27, which is also a design <strong>of</strong> a reed block <strong>and</strong> petals for a 125 racing engine which has<br />

already been discussed in Chapter 5 as a design example. The top part <strong>of</strong> the sketch on the<br />

computer screen shows an elevation section through one-half <strong>of</strong> the reed block, although it<br />

could just as well represent a complete block if that were the design goal. The lower half <strong>of</strong><br />

the sketch shows a projected view looking normally onto the reed port <strong>and</strong> the petal as if it<br />

were transparent, with the darkened area showing the clamping <strong>of</strong> the reed by the stop-plate.<br />

The scaled dimension to note here is the left-h<strong>and</strong> edge <strong>of</strong> the dark area, for that is positioned<br />

accurately, while some artistic license has been used to portray the extent <strong>of</strong> the clamped area<br />

rightward <strong>of</strong> that position!

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