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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 />

(iv) <strong>Two</strong>-stroke engines use ball, roller, <strong>and</strong> needle roller element bearings <strong>and</strong> these<br />

tend to be noisy by comparison with pressure-fed hydrodynamic bearings.<br />

The advantages <strong>of</strong> the two-stroke engine<br />

(i) The engine with the tuned exhaust pipe produces a high specific output, but this is<br />

achieved by choking the final outlet diameter, thereby simplifying the design <strong>of</strong> an<br />

effective exhaust silencer.<br />

(ii) The crankcase pump induces air by pumping with a low compression ratio <strong>and</strong>, as<br />

this reduces the maximum values <strong>of</strong> air intake particle velocity encountered in its<br />

time history, this lowers the higher-frequency content <strong>of</strong> the sound produced.<br />

(iii) The peak combustion pressures are lower in the equivalent two-stroke cycle engine,<br />

so the noise spectrum induced by that lesser combustion pressure is reduced<br />

via all <strong>of</strong> the transmission components <strong>of</strong> the cylinder, cylinder head, piston <strong>and</strong><br />

crankshaft.<br />

8.4 Some fundamentals <strong>of</strong> silencer design<br />

If you study the textbooks or technical papers on acoustics <strong>and</strong> on silencer design, such as<br />

many <strong>of</strong> those referenced below, you will find that the subject is full <strong>of</strong> empirical design<br />

equations for the many basic types <strong>of</strong> silencers used in the field <strong>of</strong> internal combustion engines.<br />

However useful these may be, you will get the feeling that a fundamental underst<strong>and</strong>ing<br />

<strong>of</strong> the subject is not being acquired, particularly as the acoustic theory being applied is<br />

one oriented to the propagation <strong>of</strong> acoustic waves, i.e., waves <strong>of</strong> infinitesimal amplitude,<br />

rather than finite amplitude waves, i.e., waves <strong>of</strong> the very considerable amplitude to be found<br />

in the inlet <strong>and</strong> exhaust systems <strong>of</strong> the internal-combustion engine. The subject matter to be<br />

found in the acoustic treatment <strong>of</strong> the theory is somewhat reminiscent <strong>of</strong> that for the topic <strong>of</strong><br />

heat transfer, producing an almost infinite plethora <strong>of</strong> empirical equations for which the authors<br />

admit rather large error b<strong>and</strong>s for their implementation in practice. This has always<br />

seemed to me as a most unsatisfactory state <strong>of</strong> affairs. Consequently, a research program was<br />

instigated at QUB some years ago to determine if it was possible to predict the noise spectrum<br />

emanating from the exhaust systems <strong>of</strong> internal-combustion engines using the approach <strong>of</strong><br />

the calculation <strong>of</strong> the propagation <strong>of</strong> finite amplitude waves by the method <strong>of</strong> characteristics<br />

as described in Ref. [7.36]. This resulted in the technical publications by Blair, Spechko <strong>and</strong><br />

Coates [8.1-8.3]. A much more complete exposition <strong>of</strong> the work <strong>of</strong> Coates is to be found in his<br />

doctoral thesis [8.17].<br />

8.4.1 The theoretical work <strong>of</strong> Coates [8.3]<br />

In those publications, a theoretical solution is produced [8.3] that shows that the sound<br />

pressure level at any point in space beyond the termination <strong>of</strong> an exhaust system into the<br />

atmosphere is, not empirically but directly, capable <strong>of</strong> being calculated. The amplitude <strong>of</strong> the<br />

nth frequency component <strong>of</strong> the sound pressure, pn, is shown to be primarily a complex<br />

function <strong>of</strong>: (a) the instantaneous mass flow rate leaving the end <strong>of</strong> the pipe system, rh, <strong>and</strong><br />

(b) the location <strong>of</strong> the measuring microphone in both distance <strong>and</strong> directivity from the pipe<br />

end, together with other parameters <strong>of</strong> some lesser significance.<br />

548

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