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OPEN CHAMBER SPARK IGNITED COMBUSTION SYSTEM DEVELOPMENT FOR HIGH POWER DENSITY AND LOW EMISSIONS

机译:开放式腔室火花点燃了高功率密度和低排放的燃烧系统开发

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High power density and thermal efficiency combined with very low NOx exhaust emissions are main challenges in today's gas engine development programmes. Until recently open chamber combustion systems using traditional spark ignition were considered to be limited by knock and misfire in their potential to achieve the above mentioned goals. The main task of the work reported here was to achieve a stable, knock-free combustion using a knock-prone gas fuel of 70 methane number for a specific power density of 25 kW/L at 250 mg/m_N~3 NO_x emission according to the TA Luft. The combustion system development was carried out on a single cylinder engine (SCE), thus, a special aspect of the work was to ensure transferability of the single cylinder engine combustion system development results to the targeted V12 multi-cylinder engine. Prior to engine testing, intensive simulation work was undertaken to specify the most promising engine hardware configurations. The main emphasis was on the 3D CFD analysis of the in-cylinder charge motion and its interaction with carefully chosen combustion chamber geometry variants. The ultimate scope was to generate high local turbulence levels during combustion, enabling a short combustion duration with low variation coefficients. The experimental phase included engine tests for several combustion relevant parameters and the detailed combustion analysis with respect to flame propagation and knock centre location using the optical combustion diagnosis system AVL VISIOLUTION. This paper describes the overall work procedure as well as the analytical and experimental methods and tools employed in the combustion system development programme. It also gives information on engine test results, the value and contribution of combustion visualisation, as well as on the engine performance which could be finally reached.
机译:高功率密度和热效率与极低的NOx排气相结合,是当今燃气发动机开发计划中的主要挑战。直到最近开放式室内燃烧系统,使用传统的火花点火被认为受到爆炸和失火的限制,以实现上述目标。这里报告的工作的主要任务是使用70甲烷编号的敲击易燃气燃料,其特定功率密度为25 kW / L的特定功率密度,根据如此的250mg / m_n〜3的NO_X排放。 ta luft。燃烧系统开发是在单个汽缸发动机(SCE)上进行的,因此,该工作的特殊方面是确保单缸发动机燃烧系统开发结果的可转换性对目标V12多缸发动机。在发动机测试之前,进行了密集的仿真工作,以指定最有前途的发动机硬件配置。主要重点是缸内电荷运动的3D CFD分析及其与精心燃烧室几何变体的相互作用。最终范围是在燃烧期间产生高局部湍流水平,从而实现具有低变化系数的短燃烧持续时间。实验相包括用于多种燃烧相关参数的发动机测试和使用光学燃烧诊断系统AVL粘液的火焰传播和敲击中心位置的详细燃烧分析。本文介绍了燃烧系统开发计划中采用的整体工作程序以及分析和实验方法和工具。它还提供有关发动机测试结果,燃烧可视化的价值和贡献的信息,以及最终达到的发动机性能。

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