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An experimental and analytical investigation into the combustion characteristics of HCCI and dual fuel engines with pilot injection.

机译:对HCCI和先导喷射双燃料发动机的燃烧特性进行实验和分析研究。

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摘要

The combustion processes within Homogeneous Charge Compression Ignition (HCCI) and dual fuel engines with pilot liquid fuel injection were investigated both experimentally and analytically. An ISUZU 3KC1 engine with a swirl chamber was suitably modified, fitted with the developed necessary instrumentation and supporting data acquisition and calculation software systems. Also, a fully instrumented variable compression ratio single cylinder CFR engine made capable of operation on gaseous and liquid fuels mixtures was used for HCCI operation. In parallel with the experimental investigation, 3D predictive computational models were developed and applied to both the HCCI and dual fuel engine combustion systems. The models, based on the KIVA3 software, incorporate detailed chemical kinetics for the oxidation of hydrogen, n-heptane, and diesel fuel while accounting for the turbulence-chemistry interactions during combustion. Much of the results of the predictive models were validated against the corresponding experimental behavior.; The combustion characteristics and cyclic variation of an n-heptane and n-pentane fuelled HCCI CFR engine were examined. The effects of changes in compression and equivalence ratios, and the additions of nitrogen, carbon dioxide, and different gaseous fuels on n-heptane fuelled HCCI engine were investigated. The optimum values for the addition of N2, CO 2, and CH4 to produce higher power and reduce cyclic variation and the intensity of energy release in HCCI combustion were determined and found to depend on the intake mixture strength, the extent of any non-homogeneity, and the specific operational conditions.; The combustion characteristics of the modified ISUZU 3KC1 engine with a swirl chamber when operating as diesel or dual fuel engine were investigated. This included determining the effects of factors such as engine speed and the quantities of the pilot and gaseous fuels on engine performance, emissions, cyclic variation, and combustion noise. It was found that a minimum absolute quantity of diesel fuel is needed to achieve steady combustion and obtain high fuel conversion efficiency for a specific operational condition.; The results of the simulation of the combustion characteristics of n-heptane fuelled HCCI-CFR engine were in good qualitative and fair quantitative agreement with the corresponding experimental values. It was found, for example, that changes in the values of the combustion chamber wall surface temperature influence greatly the autoignition timing and its location within the chamber. For high chamber wall temperatures, autoignition takes place first at regions near to the cylinder surface and the quenching distance is reduced. The effects of the initial intake swirl, temperature and pressure, engine speed, compression and equivalence ratios, and the addition of diluents and gaseous fuels on the combustion characteristics of a hydrogen fuelled HCCI engine were examined. Also, the effects of injection timing and the quantity of hydrogen admitted on the combustion of a diesel/hydrogen direct injection Gardner dual fuel engine with a hemispheric piston crown were investigated through a series of simulations. Furthermore, the corresponding processes within the ISUZU 3KC1 diesel and diesel/methane dual fuel engines with a swirl chamber were examined in detail, and the influence of changes in engine speed, injection timing, and the quantity of diesel and gaseous fuels on combustion and performance were investigated. It was observed that an earlier autoignition can be obtained through injecting the pilot fuel into the small prechamber compared to the corresponding swirl chamber operation. Furthermore, through the early injection of a small pilot liquid fuel into the swirl chamber of the dual fuel engine, a two-stage HCCI combustion can be achieved which may reduce engine emissions and improve thermal efficiency.
机译:通过实验和分析研究了均质充气压缩点火(HCCI)和带有先导液体燃料喷射的双燃料发动机内的燃烧过程。对具有涡旋室的五十铃3KC1发动机进行了适当的改装,以配备已开发的必要仪表并支持数据采集和计算软件系统。同样,将能够对气体和液体燃料混合物进行操作的,装备齐全的可变压缩比单缸CFR发动机用于HCCI操作。在进行实验研究的同时,还开发了3D预测计算模型并将其应用于HCCI和双燃料发动机燃烧系统。这些模型基于KIVA3软件,结合了氢,正庚烷和柴油燃料氧化的详细化学动力学,同时考虑了燃烧过程中的湍流-化学相互作用。预测模型的大部分结果已针对相应的实验行为进行了验证。研究了正庚烷和正戊烷燃料的HCCI CFR发动机的燃烧特性和循环变化。研究了压缩和当量比的变化以及氮,二氧化碳和不同气态燃料的添加对正庚烷燃烧的HCCI发动机的影响。确定了添加N2,CO 2和CH4以产生更高功率并减少循环变化的最佳值,并确定了HCCI燃烧中的能量释放强度,并取决于进气混合物强度,任何非均匀性的程度,以及具体的操作条件。研究了装有涡流室的改良五十铃3KC1发动机作为柴油或双燃料发动机时的燃烧特性。这包括确定诸如发动机转速以及引燃和气态燃料量等因素对发动机性能,排放,循环变化和燃烧噪声的影响。已经发现,对于特定的运行条件,需要最少的绝对数量的柴油以实现稳定的燃烧并获得高的燃料转化效率。对正庚烷燃料HCCI-CFR发动机燃烧特性的仿真结果与相应的实验值在定性和定量方面吻合良好。例如,已经发现,燃烧室壁表面温度的值的变化极大地影响了自燃正时及其在燃烧室内的位置。对于较高的燃烧室壁温度,自燃首先发生在靠近气缸表面的区域,并缩短了淬火距离。研究了初始进气涡流,温度和压力,发动机转速,压缩比和当量比以及添加稀释剂和气态燃料对以氢为燃料的HCCI发动机燃烧特性的影响。此外,还通过一系列模拟研究了喷射正时和氢吸收量对带有半球形活塞顶的柴油/氢直喷加德纳双燃料发动机燃烧的影响。此外,详细研究了具有涡旋室的五十铃3KC1柴油和柴油/甲烷双燃料发动机的相应过程,以及发动机转速,喷射正时以及柴油和气态燃料量的变化对燃烧和性能的影响。被调查了。已经观察到,与相应的涡流室操作相比,通过将引燃燃料喷射到小预燃室中可以获得较早的自燃。此外,通过将少量的先导液体燃料尽早喷射到双燃料发动机的涡流室中,可以实现两级HCCI燃烧,这可以减少发动机排放并提高热效率。

著录项

  • 作者

    Liu, Chengke.;

  • 作者单位

    University of Calgary (Canada).;

  • 授予单位 University of Calgary (Canada).;
  • 学科 Engineering Mechanical.
  • 学位 Ph.D.
  • 年度 2006
  • 页码 475 p.
  • 总页数 475
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 机械、仪表工业;
  • 关键词

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