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THERMAL MACHINES AND HEAT ENGINES

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THERMAL MACHINES AND HEAT ENGINES ( thermal-machines-and-heat-engines )

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Fig. 17.1. The Carnot cycle in different diagrams. Carnot cycle, and any other conceivable power cycle, is to be run clockwise in both the T-s and p-V thermodynamic diagrams, since the heat engine receives net heat, that in a reversible process is Qnet=TdS (recall the area interpretation of integrals), and delivers net work, that in a reversible process is Wnet=pdV; notice that in a cycle dU=TdSpdV=0. The Carnot cycle is not practical, not only because of unavoidable frictional losses (could be minimised with appropriate lubrication), but because of the heat transfer with negligible temperature jump, that would render the heat transfer rate infinitesimal for a finite size engine with finite thermal transmittance with the heat sources. However, heat transfer rates may be highly increased if the gas moves through a porous media that serves as intermediate heat source, as in the cycles of Stirling and Veuillemier. GAS POWER CYCLES Inside a heat engine, a working fluid cyclically evolves taking heat from a hot source and rejecting heat to the environment, producing some mechanical work in the way (usually shaft work). Gases are the best working substances because of their ease to exchange thermal to mechanical energy by compression or expansion, whereas liquids have little compressibility. We call ‘gas cycles’ those where the working substance stays all the time in the gas phase, and vapour cycles those where the gas condenses to liquid in some part of the cycle (and back again). Although any cycle may in principle be used as a heat engine or as a refrigerator and heat pump by just reversing the direction of the process, in practice there are big difference and the study is split between power cycles and refrigeration cycles. Many gas cycles have been proposed, and several are currently used, to model real heat engines: the Otto cycle (approximates the actual petrol engine), the Diesel cycle (approximates the actual diesel engine), the mixed cycle (an hybrid of the last two that is better than both), the Brayton cycle (approximates very well the actual gas turbine engine), and the Stirling cycle (used in some exotic applications). We restrict the analysis to the so called ‘air standard’ model, which assumes air with temperature-independent properties as the working fluid, neglecting fuel addition effects (the air to fuel mass ratio is around 15:1 in Otto engines, 30:1 in Diesel engines, and 50:1 in Brayton engines), and consider an equivalent heat addition. Otto cycle The Otto cycle is a first approximation to model the operation of a spark-ignition engine, first built by Nikolaus Otto in 1876, and used in many cars, small planes and small power systems (below say 200 kW) down to miniature engines. This is a reciprocating internal combustion gas engine, in contrast to the, at that time master, external combustion steam engine. The Otto engine is sketched in Fig. 17.2, where the typical terms are introduced for engine-geometry characteristics (stroke, bore, displacement and compression ratio); other terms for engine-operation characteristics are shaft speed, mean pressure, power, fuel consumption, torque, volumetric efficiency, energy efficiency, etc.

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