Small-scale energy conversion devices are being developed for a variety of applications; these includepropulsion units for MAV (micro aerial vehicles). The high specific energy of hydrocarbon and hydrogenfuels, as compared to other energy storing means, like, batteries, elastic elements, flywheels, pneumatics,and fuel cells, appears to be an important advantage, and favors the ICE as a candidate. In addition, thespecific power (power per mass of unit) of the ICE seems to be much higher than that of other candidates.However, micro ICE engines are not simply smaller versions of full-size engines. Physical processes suchas combustion, and gas exchange, are performed in regimes different from those occur in full-size engines.Consequently, engine design principles are different at a fundamental level, and have to be re-consideredbefore they are applied to micro-engines. When a Spark-Ignition (SI) cycle is considered, part of theenergy that is released during combustion is used to heat-up the mixture in the quenching volume, andtherefore the flame-zone temperature is lower and in some cases can theoretically fall below the selfsustainedcombustion temperature. The flame quenching thus seems to limit the minimum dimensions of aSI engine. This limit becomes irrelevant when a Homogeneous-Charge Compression-Ignition (HCCI)cycle is considered. In this case friction losses and charge leakage through the cylinder-piston gap becomedominant, constrain the engine size, and impose minimum engine speed limits.In the present work a phenomenological model has been developed to consider the relevant procuressesinside the cylinder of a Homogeneous-Charge Compression-Ignition (HCCI) engine. An approximatedanalytical solution is proposed to yield the lower possible limits of scaling-down HCCI cycle engines. Thepresent work presents simple algebraic equation that shows the inter-relationships between the pertinentparameters, and constitutes the lower possible miniaturization limits of IC engines.
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