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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 />

ment <strong>of</strong> reed lift is evident, as is the resulting calculation <strong>and</strong> measurement <strong>of</strong> delivery ratio<br />

over the entire speed range <strong>of</strong> the engine, to b6-seen in Fig. 6.26. The timing <strong>of</strong> opening <strong>and</strong><br />

closing <strong>of</strong> the reed petal at the low speed <strong>of</strong> 5430 rpm shows the reed opening at 160° btdc <strong>and</strong><br />

closing at 86° atdc, which is an asymmetrical characteristic about tdc.<br />

At the "high" engine speed <strong>of</strong> 9150 rpm, the reed petal opens at 140° btdc <strong>and</strong> closes at<br />

122° atdc. This confirms the initial view, expressed in Sec. 1.3.4 <strong>and</strong> Figs. 18(c) <strong>and</strong> (d), that<br />

the reed petal times the inlet flow behavior like a disc valve at low engine speeds <strong>and</strong> as a<br />

piston-controlled intake port at high engine speeds. In other words, it is asymmetrically timed<br />

at low speeds <strong>and</strong> symmetrically timed at high speeds.<br />

Within this same paper by Fleck etal. [1.13] there is given a considerable body <strong>of</strong> experimental<br />

<strong>and</strong> theoretical evidence on reed valve characteristics for steel, glass-fiber- <strong>and</strong> carbon-fiber-reinforced<br />

composites when used as reed petal materials. The paper [1.13] gives<br />

the dimensions <strong>of</strong> the engine with its tuned expansion chamber exhaust system <strong>and</strong> associated<br />

measured power data, which you will find instructive as another working example for the<br />

comparison <strong>of</strong> Prog.6.2v2 with experiment.<br />

6.3.2 The use <strong>of</strong> specific time area information in reed valve design<br />

From the experimental <strong>and</strong> theoretical work at QUB on the behavior <strong>of</strong> reed valves, it has<br />

been found possible to model in a satisfactory fashion the reed valve in conjunction with an<br />

engine modeling program. This implies that all <strong>of</strong> the data listed as parameters for the reed<br />

valve block <strong>and</strong> petal in Fig. 5.4 have to be assembled as input data to run an engine simulation.<br />

The input geometrical data set for a reed valve is even more extensive than that for a<br />

piston-controlled intake port, adding to the complexity <strong>of</strong> the data selection task by the designer<br />

before running an engine model. This places further emphasis on the use <strong>of</strong> some<br />

empirical design approach to obtain a first estimate <strong>of</strong> the design parameters for the reed<br />

block <strong>and</strong> petals, before the insertion <strong>of</strong> that data set into an engine modeling calculation. I<br />

propose to pass on to you my data selection experience in the form <strong>of</strong> an empirical design for<br />

reed valves as a pre-modeling exercise.<br />

In Sec. 6.1 there is a discussion on specific time area <strong>and</strong> its relevance for exhaust, transfer<br />

<strong>and</strong> intake systems. The flow through a reed valve has to conform to the same logical<br />

approach. In particular, the value <strong>of</strong> specific time area for the reed petal <strong>and</strong> reed port during<br />

its period <strong>of</strong> opening must provide that same numerical value if the flow <strong>of</strong> air through that<br />

aperture is to be sufficient to provide equality <strong>of</strong> delivery ratio with a piston-controlled intake<br />

port. The aperture through the reed valve assembly is seen in Fig. 5.4 <strong>and</strong>, from the discussion<br />

in Sec. 5.2, is to be composed <strong>of</strong> two segments: the effective reed port area in the flow direction<br />

as if the reed petal is not present; <strong>and</strong> the effective flow area past the reed petal when it<br />

has lifted to its maximum, caused either by the gas flow or as permitted by the stop-plate.<br />

Clearly, there is little point in not having these two areas matched. For example, if the design<br />

incorporates a large reed port area but a stiff reed which will barely lift under the pressure<br />

differential from the intake side to the crankcase, very little fresh charge will enter the engine.<br />

Equally, the design could have a large flexible reed which lifted easily but exposed only a<br />

small reed port, in which case that too would produce an inadequate delivery ratio characteristic.<br />

In a matched design, the effective reed port area should be larger than the effective flow<br />

450

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