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The Squish-Jet Combustion Chamber for Ultra- Lean Burn Natural Gas Engines

机译:用于超稀燃燃烧天然气发动机的鳞墨布燃烧室

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Operators of natural gas engines, used for both mobile and stationary applications, are increasingly looking at running these engines under very lean air-fuel ratios in order to reduce exhaust emissions and increase thermal efficiency. Lean operation of homogeneous-charge spark-ignited engines reduces peak combustion temperatures, thereby reducing NO_x emissions. Lean operation is normally restricted, however, by the "lean-limit" of combustion, as measured by the air-fuel ratio above which ignition is impossible, or combustion is incomplete. Operation under lean conditions also reduces the mixture burning rate, which can lead to increased spark advance and lower thermal efficiency. In order to increase the burning rate under ultra-lean air-fuel ratios a new "Squish-Jet" combustion chamber concept has been developed. This technique incorporates a series of passages in the crown of a bowl-in-piston type of combustion chamber which generates increased levels of small-scale turbulence just before ignition and during the early phase of combustion. This increased burning rate enables the engine to operate with a smaller spark advance under lean conditions, thereby extending the lean-limit of operation and increasing the thermal efficiency. The additional small-scale turbulence levels generated with the squish-jet type of combustion chamber is also effective in improving the completeness of combustion, thereby reducing unburned hydrocarbon emissions. This paper presents the results of a series of tests of the squish-jet combustion chamber design in a single-cylinder Ricardo Hydra research engine. The engine was run at three different engine speeds and under both naturally aspirated conditions and a boost pressure of 1.75 bar manifold absolute pressure. Two different squish-jet piston geometries were tested, together with a conventional bowl-in-piston design for comparison. The squish-jet combustion chambers were found generally to reduce emissions under ultra-lean operating conditions.
机译:用于移动和静止应用的天然气发动机的操作员越来越多地看着在非常贫的空气燃料比下运行这些发动机,以减少废气排放并提高热效率。均匀电荷火花点火发动机的瘦操作可降低峰燃烧温度,从而减少NO_X排放。然而,通过燃烧的“倾斜限制”通常限制稀释操作,如上不可能点火的空燃比测量,或燃烧不完整。瘦条件下的操作也降低了混合燃烧速率,这可能导致火花提前和较低的热效率。为了提高超贫空燃比下的燃烧率,已经开发出一种新的“挤出式”燃烧室概念。该技术包括一系列圆柱形燃烧室的圆冠上的一系列通道,其在点火之前和在燃烧的早期阶段之前产生增加的小规模湍流水平。这种增加的燃烧速率使发动机能够在贫条件下以较小的火花提前操作,从而延长操作的稀薄限制并增加热效率。用鳞片喷射型燃烧室产生的额外的小型湍流水平也有效地改善燃烧的完整性,从而减少了未燃烧的烃排放。本文介绍了一系列在单缸里卡多水拉研究发动机中的鳞型喷射燃烧室设计试验的结果。发动机以三种不同的发动机速度运行,并且在自然吸气条件下,升压压力为1.75巴歧管绝对压力。测试了两个不同的鳞片式射流活塞几何形状,以及传统的碗内的活塞设计进行比较。鳞片喷射燃烧室通常是在超贫工作条件下减少排放。

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