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Design and Simulation of Two Stroke Engines

Design and Simulation of Two Stroke Engines

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Chapter 6 - Empirical Assistance for the <strong>Design</strong>er<br />

This equation applies to all ports <strong>and</strong> to all gas flow through the engine. Within the engine<br />

<strong>and</strong> gas-dynamic models <strong>of</strong> Chapters 2 <strong>and</strong> 5, this summation exercise is carried out at each<br />

calculation step so that the values <strong>of</strong> delivery ratio, scavenge ratio, etc., are ultimately determined.<br />

The term, Ae, which is the instantaneous area <strong>of</strong> the port at any instant, employed in<br />

Eq. 6.1.3, is determined using the theoretical approach detailed in Sec. 5.2.<br />

As most two-stroke engines have the symmetrical porting geometry shown in Fig. 6.1,<br />

<strong>and</strong> as the variations <strong>of</strong> density <strong>and</strong> gas velocity with time are somewhat similar from engine<br />

to engine, there might exist some mathematical function linking the remaining terms to the<br />

gas flow transmitted. Perhaps more importantly, as the gas flow which is transmitted is related<br />

to that which is trapped <strong>and</strong> burned with fuel to produce power, the relationship could<br />

extend to a more direct linkage to engine performance.<br />

For example, the application <strong>of</strong> Eq. 6.1.3 to the inlet port within an engine model predicts<br />

the total air mass ingested into the engine on each cycle. The point has already been made<br />

above that this must have a direct relationship to the work output from that cycle when that air<br />

is burned with fuel in the correct proportions. As already pointed out, this can be seen in Figs.<br />

5.9 <strong>and</strong> 5.10 from the close correspondence between the delivery ratio <strong>and</strong> bmep with engine<br />

speed for the chainsaw engine.<br />

The net work output per cycle, from Fig. 1.16, is given by:<br />

Work/cycle = Vsv bmep (6.1.4)<br />

If the relationship is linear, then the division <strong>of</strong> air mass ingested by work output should<br />

be "a constant":<br />

i Jpe A e c e dt<br />

airingested = ^ = a constant (6-1 -5)<br />

Vsvbmep Vsvbmep<br />

On the assumption that the temporal variations <strong>of</strong> density, pe, <strong>and</strong> particle velocity, CQ,<br />

are somewhat similar, even for different engines, incorporating these so-called constants into<br />

the right-h<strong>and</strong> side <strong>of</strong> Eq. 6.1.5 reduces it to:<br />

This can also be written as:<br />

9=0<br />

,=t P<br />

|A0dt<br />

m oc bmep (6.1.6)<br />

V<br />

v sv<br />

jAe-de<br />

3 - - bmep (6-1-7)<br />

6=0<br />

v Ysv<br />

419

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