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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:在发动机状条件下快速压缩和膨胀机中的Unsgenged Prechamber燃烧的实验性和数值研究

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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:尽管未接受的PRECHAMBER已被广泛应用于精益预混天然气发动机,但对基本面的了解有限,缺乏预测性建模工具(3D RAN CFD)妨碍PRECHAMBER设计和优化的方式。本研究通过组合光学诊断(高速OH * -Chemil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)中贫甲烷/空气混合物的瘦甲烷/空气混合物的止血剂燃烧。来自前者的数据用于开发和验证特定应用的建模方法,后者旨在提供对实验观察的不可或缺的解释。最初,Schlieren和OH *图像的比较确认了所固有的反应火焰喷射器从预挤压器出口的假设,这证明了水平设定燃烧建模框架适用于调查的操作条件。已经延长了所用的G-arequation燃烧模型以考虑研究的PRECHAMBER配置中存在的火花点火和火焰壁相互作用。通过实验数据验证开发的模型,在(i)喷射出口时序,(ii)主室热释放率(HRR)和(iii)投影的反应火焰区域,证明鼓励预测能力的良好协议建议的建模方法。实验和CFD仿真的综合见解表明了主要腔室热释放速率的两个阶段,分别由喷射穿透和湍流火焰传播。随后使用OH * - 辛升发光和CFD图像对单个火焰射流的分析表明,由于湍流水平较高和较大的涡尺寸,喷射头趋于更具反应性。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(累积热释放的5%)之间的逆相关性。总体而言,这项研究为未来的未来传球设计提供了有用的指导方针。 (c)2019燃烧研究所。由elsevier Inc.出版的所有权利保留。

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:PRECHAMBER;CFD燃烧仿真;湍流火焰喷射;燃烧光学诊断;

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