发明名称 Turbosupercharged internal combustion engine control method
摘要 A method of controlling an internal combustion engine supercharged by a turbosupercharger having a turbine and a compressor; the control method including the steps of: determining, in a reduced mass flow/compression ratio graph, at least one limit operation curve of the compressor representing a limit of the operating range of the compressor; controlling the turbosupercharger to keep the actual reduced mass flow and actual compression ratio of the compressor within the limit defined by the limit operation curve of the compressor; determining an index as a function of the dynamics of the reduced mass flow of the compressor; and modifying the limit operation curve of the compressor as a function of the index.
申请公布号 US9008945(B2) 申请公布日期 2015.04.14
申请号 US201113270330 申请日期 2011.10.11
申请人 Magneti Marelli S.p.A. 发明人 Panciroli Marco
分类号 G06F19/00;G06G7/70;F02D41/00;F02D41/10;F02B37/18;F02B37/16;F02D41/20 主分类号 G06F19/00
代理机构 Howard & Howard Attorneys PLLC 代理人 Howard & Howard Attorneys PLLC
主权项 1. A method of controlling an internal combustion engine (1) supercharged by a turbosupercharger (12) comprising a turbine (13) and a compressor (14); the control method comprising the steps of: determining, in a reduced mass flow/compression ratio graph, at least one limit operation curve (28, 30, 32, 34) of the compressor (14) representing a limit of the operating range of the compressor (14); and controlling the turbosupercharger (12) to keep the actual reduced mass flow (QAHR) and actual compression ratio (CR) of the compressor (14) within the limit defined by the limit operation curve (28, 30, 32, 34) of the compressor (14); determining an index (Δdyn) varying as a function of the dynamics of the reduced mass flow (QAHR) of the compressor (14); and modifying the limit operation curve (28, 30, 32, 34) of the compressor (14) as a function of the index (Δdyn) wherein a first limit operation curve (28, 30, 32, 34) of the compressor (14) is shifted, in the reduced mass flow/compression ratio graph, by an amount which is a function of the index (Δdyn) and wherein the first limit operation curve (28) of the compressor (14) is a pump curve (28) of the compressor (14), which defines the points beyond which the internal aerodynamic balance of the compressor (14) is disrupted; and the first limit operation curve (28) of the compressor (14) is shifted up, in the reduced mass flow/compression ratio graph, when the internal combustion engine (1) accelerates, and down when the internal combustion engine (1) decelerates.
地址 Corbetta IT