发明名称 Knock detector for internal combustion engine
摘要 An engine knock detector including a first mechanism for sensing engine noise during a first time period of an engine combustion cycle and providing a first signal in response thereto. A second mechanism is also provided for sensing engine noise and engine knock during a second time period of the combustion cycle and providing a second signal in response thereto. Finally, a third mechanism is included for comparing the first and second signals and generating a third signal to determine the occurrence of an engine knock. In a preferred embodiment, a vibration signal represented by an electrical voltage is bandpass amplified, digitized and filtered by a tunable filter. The filtered digital signal, which represents engine vibrations, is then directed to first and second energy detectors. The coefficients of the tunable filter and the timing signals of the energy detectors are provided by a programmable memory. Each energy detector respectively provides an energy signal which represents the total energy within one of two separate regions within a single combustion cycle. The two separate regions represent a no-knock time duration and a knock time duration of the combustion cycle. The two energy signals are then subjected to a hypothesis test within a comparator to determine the occurrence of an engine knock.
申请公布号 US5408863(A) 申请公布日期 1995.04.25
申请号 US19930048100 申请日期 1993.04.15
申请人 HUGHES AIRCRAFT COMPANY 发明人 SAWYERS, JAMES H.;THOMPSON, GERALD A.;HELANDER, WAYNE
分类号 F02B1/04;F02D41/14;G01L23/22;G01M15/12;(IPC1-7):G01L23/22 主分类号 F02B1/04
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