发明名称 METHOD TO DETECT AND CONTROL DETONATION PHENOMENA IN AN INTERNAL COMBUSTION ENGINE
摘要 Method to detect and control detonation phenomena in an internal combustion engine provided with a number of cylinders and with at least two detonation sensors; for each combustion cycle as a function of the cylinder and of the engine point that is being explored, the method comprises processing the signal coming from each detonation sensor so as to determine a detonation energy for each detonation sensor; calculating a detonation index for each detonation sensor and controlling the internal combustion engine as a function of a total detonation index through the algebraic sum of the detonation indexes for each detonation sensor.
申请公布号 US2016138551(A1) 申请公布日期 2016.05.19
申请号 US201514944899 申请日期 2015.11.18
申请人 MAGNETI MARELLI S.p.A. 发明人 CAVANNA Filippo;LANZONI Riccardo
分类号 F02P5/145;F02P17/12;F02P9/00 主分类号 F02P5/145
代理机构 代理人
主权项 1. A method to detect and control detonation phenomena in an internal combustion engine (1) provided with a number of cylinders (2) and with at least two detonation sensors (18), in particular two accelerometers (18*, 18**); the method comprising the steps of: acquiring the signal (S*, S**) coming from each detonation sensor (18); processing the signal (S*, S**) coming from each detonation sensor (18) so as to determine a detonation energy (Sel*, Sel**) for each detonation sensor (18); determining a first indicator (α) for each detonation sensor (18) as a function of the cylinder (2) and of the engine point that is being explored, univocally identified by the revolutions per minute (rpm) and by the load; wherein the first indicator (α) is variable as a function of the observability of the detonation phenomena for each detonation sensor (18); defining a second global indicator (β) of observability of the combustion at a given engine point for a cylinder (2), in which the combustion can be fully observable by means of both detonation sensors (18) or by means of a preferred detonation sensor (18), or partially observable by means of the two detonation sensors (18) or not observable by any of the detonation sensors (18); and controlling the ignition advance implemented for the cylinder (2) in the next combustion cycle, as a function of the second global indicator (β) of observability of the combustion at the given engine point for the cylinder (2).
地址 Corbetta IT