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Experimental and numerical investigations of the unscavenged prechamber combustion in a rapid compression and expansion machine under engine-like conditions

机译:在类似发动机的条件下,快速压缩和膨胀机中无气室前室燃烧的实验和数值研究

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摘要

Even though the unscavenged prechamber has been extensively applied in lean premixed natural gas engines, the limited understanding of the fundamentals and the lack of predictive modeling tools (3D RANS CFD) place obstacles in the way of prechamber design and optimization. The present study investigates unscavenged prechamber combustion of lean methane/air mixtures in a Rapid Compression Expansion Machine (RCEM) by combining optical diagnostics (high-speed OH*-chemiluminescence and Schlieren imaging) and 3D Computational Fluid Dynamic (CFD) simulations. Data from the former is used to develop and validate the modeling approach for the specific application and the latter aims to provide indispensable interpretation of the experimental observations. Initially, the comparison of the Schlieren and the OH* images confirm the hypothesis that inherent reacting flame jets exit the prechamber, which justifies the applicability of a level set combustion modeling framework for the investigated operating conditions. The employed G-equation combustion model has been extended to account for the specifics of spark ignition and flame wall interaction present in the prechamber configuration studied. Validation of the developed model by means of the experimental data shows good agreements in terms of (i) jet exit timing, (ii) main chamber heat release rate (HRR) and (iii) projected reactive flame area, evidencing encouraging predictive capability of the proposed modeling approach. The combined insights from experiments and CFD simulations suggest two phases of the main chamber heat release rate, dominated by the jet penetration and the turbulent flame propagation respectively. The subsequent analysis on a single flame jet, using OH*-chemiluminescence and CFD images, indicates that the jet head tends to be more reactive due to a higher turbulence levels and larger eddy size. Moreover, the entire dataset reveals an inverse correlation between the initial reactive jet speed and the early phase combustion duration (5% of total cumulative heat release). Overall, this research provides useful guidelines for the future unscavenged prechamber design. (C) 2019 The Combustion Institute. Published by Elsevier Inc. All rights reserved.
机译:尽管无气的预燃室已广泛应用于稀薄的预混天然气发动机中,但对基本原理的了解有限以及缺乏预测建模工具(3D RANS CFD)仍给预燃室的设计和优化带来了障碍。本研究通过结合光学诊断(高速OH *化学发光和Schlieren成像)和3D计算流体动力学(CFD)模拟,研究了快速压缩膨胀机(RCEM)中稀薄的甲烷/空气混合物的未燃室燃烧。前者的数据用于开发和验证针对特定应用的建模方法,而后者的目的是提供对实验观察的必不可少的解释。最初,对Schlieren图像和OH *图像的比较证实了以下假设:固有的反应性火焰喷射流离开了前室,这证明了水平集燃烧模型框架适用于所研究的运行条件的合理性。所采用的G方程燃烧模型已经扩展,可以说明研究的预燃室配置中存在的火花点火和火焰壁相互作用的细节。通过实验数据对开发模型的验证表明,在以下方面,(i)射流出口正时,(ii)主腔室热释放率(HRR)和(iii)预计的反应火焰面积具有良好的一致性,证明了该模型令人鼓舞的预测能力建议的建模方法。来自实验和CFD模拟的综合见解表明主腔室放热率的两个阶段,分别由射流穿透和湍流火焰传播控制。随后使用OH *化学发光和CFD图像对单个火焰喷射器进行的分析表明,由于较高的湍流度和较大的涡流尺寸,喷射头往往具有更高的反应性。此外,整个数据集揭示了初始反应射流速度与早期燃烧持续时间(占总累积热量释放的5%)之间的反相关关系。总体而言,这项研究为将来的未清理前室设计提供了有用的指导。 (C)2019燃烧研究所。由Elsevier Inc.出版。保留所有权利。

著录项

  • 来源
    《Combustion and Flame》 |2019年第6期|68-84|共17页
  • 作者单位

    Swiss Fed Inst Technol, Aerothermochem & Combust Syst Lab, ML L16, Sonneggstr 3, CH-8092 Zurich, Switzerland;

    Swiss Fed Inst Technol, Aerothermochem & Combust Syst Lab, ML L16, Sonneggstr 3, CH-8092 Zurich, Switzerland;

    Swiss Fed Inst Technol, Aerothermochem & Combust Syst Lab, ML L16, Sonneggstr 3, CH-8092 Zurich, Switzerland;

    Swiss Fed Inst Technol, Aerothermochem & Combust Syst Lab, ML L16, Sonneggstr 3, CH-8092 Zurich, Switzerland;

    Swiss Fed Inst Technol, Aerothermochem & Combust Syst Lab, ML L16, Sonneggstr 3, CH-8092 Zurich, Switzerland;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);美国《生物学医学文摘》(MEDLINE);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Prechamber; CFD combustion simulation; Turbulent flame jet; Combustion optical diagnostics;

    机译:前室;CFD燃烧模拟;湍流火焰喷射;燃烧光学诊断;

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