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THERMODYNAMIC PERFORMANCE OPTIMIZATION OF RECIPROCATING INTERNAL COMBUSTION (IC) ENGINES

机译:往复式内燃机(IC)发动机的热力学性能优化

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Reciprocating IC engines are traditionally modeled as operating on air standard cycles that approximate indicator diagrams obtained in experiments on real engines. These indicator diagrams can best be approximated by the dual cycle for both gasoline and diesel engines. Analysis of air standard cycles unfortunately fails to capture second law effects such as exergy destruction due to the irreversibility of combustion. Indeed, a complete thermodynamic study of any process requires application of both the first and second laws of thermodynamics. This article gives a combined first and second law analysis of reciprocating IC engines in general with optimization of performance as primary goal. A practical dual-like cycle is assumed for the operation of a typical reciprocating IC engine and process efficiencies are assigned to allow for irreversibilities in the compression and expansion processes. The combustion process is modeled instead of being replaced simply by a heat input process to air as is common in air standard cycle analysis. The study shows that performance of the engine can indeed be optimized on the basis of geometrical design parameters such as the compression ratio as well as the air-fuel ratio used for the combustion.
机译:往复式IC发动机传统上是在空气标准循环上进行操作的,该航空标准循环是在真正的发动机实验中获得的指示图。这些指示图最能由汽油和柴油发动机的双循环近似。遗憾的是,空气标准循环的分析未能捕获由于燃烧不可逆转而导致的第二律效应,例如暴力破坏。实际上,对任何过程的完整热力学研究需要应用热力学的第一和第二定律。本文一般提供了往复IC发动机的往复式IC发动机的组合和第二律分析,以优化作为主要目标。假设用于操作典型往复IC发动机的操作的实用的双循环,并且分配过程效率以允许压缩和扩展过程中的不缩小。燃烧过程被建模而不是仅通过热输入过程更换为空气,而在空气标准循环分析中是常见的。该研究表明,发动机的性能实际上可以基于几何设计参数,例如压缩比以及用于燃烧的空燃比。

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