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    • 6. 发明授权
    • Ignition timing control system for in-cylinder injection internal
combustion engine
    • 用于缸内喷射内燃机的点火正时控制系统
    • US5875756A
    • 1999-03-02
    • US919614
    • 1997-08-28
    • Hitoshi KamuraKenjiro HatayamaAtsuyoshi KojimaHiroki Tamura
    • Hitoshi KamuraKenjiro HatayamaAtsuyoshi KojimaHiroki Tamura
    • F02D41/02F02D41/04F02D41/24F02D41/30F02D43/00F02P5/04F02P5/15F02B17/00
    • F02D41/3029F02D41/2422F02D41/307F02P5/045F02P5/1504Y02T10/46
    • An ignition timing control system is provided for an in-cylinder injection internal combustion engine to reduce a torque shock upon switching a fuel injection mode between a compression-stroke injection mode, in which an injection of fuel is performed primarily in a compression stroke, and an intake-stroke injection mode, in which an injection of fuel is performed primarily in an intake stroke, in accordance with an operation state of said internal combustion engine. The ignition timing control system is provided with an injection timing correction unit for correcting ignition timing of a spark plug, which is arranged in a combustion chamber, upon switching said fuel injection mode. A correction amount for ignition timing, by which said ignition timing is corrected by said ignition timing correction unit upon switching from said compression-stroke injection mode to said intake-stroke injection mode, is greater than a correction amount for ignition timing, by which said ignition timing is corrected upon switching from said intake-stroke injection mode to said compression-stroke injection mode.
    • 提供了一种用于缸内喷射内燃机的点火正时控制系统,以在主要在压缩冲程中执行燃料喷射的压缩冲程喷射模式和主要在压缩冲程中执行燃料的压缩冲程喷射模式之间切换燃料喷射模式时减小扭矩冲击,以及 根据所述内燃机的运转状态,主要在进气冲程中进行燃料喷射的进气冲程喷射模式。 点火正时控制系统设置有用于在切换所述燃料喷射模式时校正布置在燃烧室中的火花塞的点火正时的喷射正时校正单元。 在从所述压缩冲程喷射模式切换到所述进气冲程喷射模式时,通过所述点火正时校正单元校正所述点火正时的点火正时的校正量大于点火正时的校正量,由此, 在从所述进气冲程喷射模式切换到所述压缩冲程喷射模式时,点火正时被校正。
    • 8. 发明授权
    • Combustion control device for internal combustion engine
    • 内燃机燃烧控制装置
    • US5870992A
    • 1999-02-16
    • US914653
    • 1997-08-19
    • Hitoshi KamuraKenjiro HatayamaAtsuyoshi KojimaMasato YoshidaKatsuhiko Miyamoto
    • Hitoshi KamuraKenjiro HatayamaAtsuyoshi KojimaMasato YoshidaKatsuhiko Miyamoto
    • F02B17/00F02B23/10F02D41/02F02D41/04F02D41/14F02D41/30F02D41/38F02D45/00G01M15/11F02B5/00
    • F02D41/1475F02D41/1498F02D41/3029G01M15/11F02B2275/18F02D2041/389F02D2200/1015F02D41/3809
    • In a combustion control device for an internal combustion engine provided with a plurality of fuel injection modes having different target air-fuel ratios, threshold values for detecting deterioration of combustion in the internal combustion engine are determined separately for each fuel injection mode depending on features of variation of combustion in the internal combustion engine in each fuel injection mode. Quantity of variation of combustion in the internal combustion engine is, for example, detected in the form of revolution angular acceleration or revolution angular acceleration deviation of the engine. The detected quantity of revolution fluctuation is compared with a threshold value in the currently chosen fuel injection mode. Thus, deterioration of combustion is surely judged according to each fuel injection mode. In particular, threshold values in a compression stroke injection mode are determined to be larger than threshold values in an intake stroke injection mode. A threshold value in the compression stroke injection mode is so determined as to substantively correspond to a complete misfire state of the engine, and threshold values in the intake stroke injection mode consist of a first threshold value substantively corresponding to a complete misfire state of the engine and a second threshold value substantively corresponding to an unstable combustion state of the engine.
    • 在具有不同目标空燃比的多个燃料喷射模式的内燃机的燃烧控制装置中,根据燃料喷射模式的特征,分别确定用于检测内燃机的燃烧劣化的阈值 在每种燃料喷射模式中内燃机的燃烧变化。 例如,以内燃机的转角角加速度或回转角加速度偏差的形式检测内燃机的燃烧变化量。 将检测到的转速波动与当前选择的燃料喷射模式中的阈值进行比较。 因此,根据各燃料喷射模式可靠地判断燃烧的劣化。 特别地,压缩冲程喷射模式中的阈值被确定为大于进气冲程喷射模式中的阈值。 压缩冲程喷射模式中的阈值被确定为实质上对应于发动机的完全失火状态,并且进气冲程喷射模式中的阈值由实质上对应于发动机的完全失火状态的第一阈值组成 以及实质上对应于发动机的不稳定燃烧状态的第二阈值。