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Simulation of n-heptane and Fuels for Advanced Combustion Engines (FACE) surrogates in a single-cylinder compression ignition engine.

机译:在单缸压缩点火发动机中模拟正庚烷和高级燃烧发动机(FACE)的燃料。

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摘要

A CFD model of a HATZ diesel engine was developed for the purpose of simulating low temperature combustion (LTC) of surrogate diesel fuels for the Fuels for Advanced Combustion Engines (FACE). Initial validation of the model was performed using n-heptane data from a single cylinder HATZ diesel engine. N-heptane was initially chosen for several reasons: (1) several well validated mechanisms are available, (2) there is a wealth of data for n-heptane ranging from constant volume to engine experiments, (3) n-heptane is also used as the simplest representative of diesel fuel, because of the similarity in cetane numbers resulting in ignition characteristics (e.g. ignition delay) that are representative of diesel fuel without the added complexity of modeling several hundred components. Simulations were run with both a detailed n-heptane mechanism and several reduced mechanisms to determine the suitability of using a reduced mechanism and ensure that the main ignition characteristics were captured. Due to the computational time, CFD combustion models are limited to using a reduced version of the detailed mechanism. It was found that a 173 species n-heptane mechanism predicts start of combustion (SOC) within 0.5 crank angle degrees of the detailed 561 species mechanism. The 173 species mechanism required 27 hours of computational time to reach the end of the simulation whereas the 561 species detailed mechanism required 41 hours of computational time under the same conditions. There were two additional reduced mechanisms that were used which contained 85 species and 35 species and were used with reasonable accuracy with a computational time of 8 hours and 2 hours, respectively. Due to the varying physical and chemical properties of the FACE surrogates, a sensitivity analysis of the effects of the physical properties was conducted by changing the n-heptane physical properties to n-hexadecane physical properties while keeping the chemistry the same. As expected, when the fuel properties of n-hexadecane (which is less volatile than n-heptane) were assigned to the n-heptane chemistry, SOC was delayed and the net heat release rate was reduced. This is mainly due to the droplets requiring more time for evaporation and less of a premixed combustion phase along with combustion occurring later in the cycle.;The FACE fuels were developed to fulfill the need for research grade fuels that are able to represent common refinery stream fuels. Due to the FACE fuels consisting of hundreds of fuel components and the lack of availability of a chemical mechanism for some of the fuel components make it extremely difficult to model these fuels in a fullscale engine model. Thus, surrogates are required for the FACE fuels as well as a reduced mechanism capable of capturing the chemical reactions of each individual fuel component. A detailed diesel mechanism was reduced from 4016 species to a single chemical mechanism with 1046 species to match the characteristics of the surrogates for the FACE fuels 1, 3, 5, 8, and 9. The surrogates were used in simulation because they experimentally behave the same as the FACE fuels, and they only contain 4-7 species, compared to the hundreds of species found in the FACE fuels. Using the single chemical mechanism to represent the five surrogates FACE fuels it was found that 200°C of air preheat was required to achieve autoignition in the HATZ model compared to the 100°C of air preheat required experimentally. Initial runs have found that there were similar trends between the FACE fuel surrogate experiments and simulations for the respective fuels. Future work will require improvements on the single chemical mechanism to represent the five surrogate FACE fuels.
机译:开发了HATZ柴油机的CFD模型,目的是模拟高级燃烧发动机燃料(FACE)的替代柴油的低温燃烧(LTC)。使用来自单缸HATZ柴油发动机的正庚烷数据对模型进行了初步验证。最初选择正庚烷的原因有几个:(1)有几种经过充分验证的机理,(2)从恒定体积到发动机实验,正庚烷的数据很多,(3)也使用正庚烷作为十六烷值的最简单代表,因为十六烷值的相似性会导致代表柴油的点火特性(例如点火延迟),而不会增加对数百个零件建模的复杂性。使用详细的正庚烷机制和几种简化的机制进行模拟,以确定使用简化的机制的适用性,并确保捕获了主要的点火特性。由于计算时间长,CFD燃烧模型仅限于使用详细机制的简化版本。发现一种173种正庚烷机理可预测详细561种机理的0.5曲轴转角内的燃烧开始(SOC)。 173个物种的机制需要27小时的计算时间才能达到模拟结束,而561个物种的详细机制在相同条件下需要41个小时的计算时间。使用了另外两个简化的机制,分别包含85种和35种,并且以合理的准确度使用,计算时间分别为8小时和2小时。由于FACE替代物的物理和化学性质各不相同,因此通过将正庚烷物理性质更改为正十六烷物理性质,同时保持化学性质相同,可以对物理性质的影响进行敏感性分析。不出所料,当将正十六烷(挥发性比正庚烷低)的燃料属性分配给正庚烷化学物质时,SOC会延迟,净放热率会降低。这主要是由于液滴需要更多​​的时间进行蒸发,而较少的预混燃烧阶段以及随后在循环中发生的燃烧。FACE燃料的开发是为了满足能够代表普通炼厂物流的研究级燃料的需求。燃料。由于FACE燃料由数百种燃料成分组成,并且某些燃料成分缺乏化学机制,因此很难在全尺寸发动机模型中对这些燃料进行建模。因此,FACE燃料需要替代物,并且需要能够捕获每种燃料组分的化学反应的简化机构。详细的柴油机机理已从4016种减少为1046种的单一化学机理,以匹配FACE燃料1、3、5、8和9的替代物的特性。模拟中使用了替代物,因为它们在实验上表现出与FACE燃料相同,与FACE燃料中发现的数百种物质相比,它们仅包含4-7种。使用单一的化学机理表示五种替代FACE燃料,发现在HATZ模型中实现自燃需要200°C的空气预热,而实验所需的空气预热为100°C。初步运行发现,在FACE燃料替代实验和相应燃料的模拟之间存在相似的趋势。未来的工作将需要改善代表五种替代FACE燃料的单一化学机理。

著录项

  • 作者单位

    Colorado School of Mines.;

  • 授予单位 Colorado School of Mines.;
  • 学科 Engineering Mechanical.
  • 学位 M.S.
  • 年度 2013
  • 页码 134 p.
  • 总页数 134
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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