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Petrol injection engine and method for controlling the gasoline injection engine

机译:汽油喷射发动机和控制汽油喷射发动机的方法

摘要

A gasoline fuel injection engine having a self-ignition combustion operating range that allows autoignition of fuel injected into a cylinder through an injector and containing at least gasoline, the engine having a geometric compression ratio in the range of 18 to 40, including both limits, the engine comprising: an injection control section configured to control fuel injection of the injector; andan ignition assisting section configured to apply energy to the fuel injected into the cylinder through the injector to assist the autoignition combustion of the fuel when the engine is within the autoignition combustion operating range, wherein when the engine is within the autoignition combustion operating range, the injection control section sets a start time of the fuel injection within a period from an end stage of a compression stroke to an upper compression dead center, and the ignition assisting section applies the energy to the fuel injected into the cylinder in a period from the start of fuel injection to an initial stage of an expansion stroke, characterized that is, a time of a specific crank angle which is in a range of 4 ° CA to 15 ° CA after the upper compression dead center, and at wherein a cylinder internal pressure increase rate, which is a ratio of a change in the cylinder internal pressure to a change in crank angle in operation of the engine, reaches a negative maximum value overlaps with a main combustion period in which a combustion mass percentage of the fuel is in the range of 10% up to 90%, both limits included, with the ignition assist section applying the energy to the fuel injected into the cylinder through plasma ignition.
机译:具有自燃燃烧操作范围的汽油燃料喷射发动机,其允许通过喷射器喷射到气缸中的燃料自动点火并至少包含汽油,该发动机的几何压缩比在18至40的范围内,包括两个极限值,该发动机包括:喷射控制部,该喷射控制部构造成控制喷射器的燃料喷射。点火辅助部分,其构造成当发动机在自燃燃烧操作范围内时,将能量施加到通过喷射器喷射到气缸中的燃料,以辅助燃料的自燃燃烧,其中,当发动机在自燃燃烧操作范围内时,喷射控制部设定从压缩行程的结束阶段到上压缩死点为止的期间内的燃料喷射的开始时间,点火辅助部在从开始起的期间内向喷射到气缸内的燃料施加能量。燃料喷射到膨胀冲程的初始阶段的时间,其特征在于,在上压缩死点之后的特定曲柄角的时间在4°CA到15°CA的范围内,并且其中发动机运转时气缸内压的变化与曲柄角的变化之比的增加率达到负值最大值与主燃烧期重叠,在主燃烧期中,燃料的燃烧质量百分比在10%到90%(包括两个限制)的范围内,点火辅助部分将能量施加到通过等离子注入到气缸中的燃料点火。

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