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    • 2. 发明授权
    • Fault recognition system and method for an internal combustion engine
    • 内燃机故障识别系统及方法
    • US6112150A
    • 2000-08-29
    • US289553
    • 1999-04-09
    • John M. IronsEdward J. LewandowskiScott G. DeckerGregg G. GreathouseIrfan Tusneem
    • John M. IronsEdward J. LewandowskiScott G. DeckerGregg G. GreathouseIrfan Tusneem
    • F02D45/00F02D41/22F02D41/26G05B9/02G05B23/02G06G7/76G06F17/00
    • F02D41/266F02D41/22
    • A fault recognition system is implemented as an adjunct to fault determination software of an on-board engine control module (ECM). The ECM activates a "Type A" or "Type B" fault code for each signal received from a plurality of sensors disposed about the engine when that signal exceeds a predetermined threshold. A "Type C" fault is recognized and activated when all of a predetermined group of underlying "Type A" or "Type B" fault codes have been activated. The "Type C" fault is displayed, while the underlying faults may or may not be displayed. The "Type C" fault provides a better and more immediate indication of the source of the engine problem than any of the underlying faults. Only those underlying faults that aid in the recognition of the source of the engine problem are displayed. The remaining faults underlying the "Type C" fault are masked. When the "Type C" fault becomes inactive, any underlying fault codes are unmasked for subsequent evaluation. To avoid false positives or negatives, all of the underlying faults must be activated for a predetermined period before the "Type C" fault will be activated. Likewise, before the "Type C" fault is de-activated, at least one of the underlying faults must be inactive for a predetermined period.
    • 故障识别系统被实现为车载发动机控制模块(ECM)的故障确定软件的附件。 当该信号超过预定阈值时,ECM为从发动机周围设置的多个传感器接收的每个信号激活“A型”或“B型”故障代码。 当所有基本的“A型”或“B型”故障代码组都被激活时,识别并激活“C型”故障。 显示“C型”故障,而底层故障可能显示也可能不显示。 “C型”故障提供了比任何潜在故障更好和更直接的指示发动机问题的来源。 仅显示有助于识别发动机问题源的潜在故障。 “C型”故障的其余故障被屏蔽。 当“类型C”故障变为无效时,任何潜在的故障代码都将被屏蔽以供后续评估。 为了避免误报或否定,在“C型”故障被激活之前,所有的底层故障必须被激活一段预定的时间。 类似地,在“类型C”故障被去激活之前,至少一个潜在故障必须在预定的时间段内是无效的。
    • 3. 发明授权
    • Duty cycle monitoring system for an engine
    • 发动机的占空比监控系统
    • US06601442B1
    • 2003-08-05
    • US09400666
    • 1999-09-20
    • Scott G. DeckerGregory G. GreathouseJohn M. Irons
    • Scott G. DeckerGregory G. GreathouseJohn M. Irons
    • G01P2100
    • G07C5/085F02D41/2451F02D41/263
    • A system and method for monitoring engine performance utilizes a monitoring micro-controller that integrates with an engine/vehicle controller to receive data indicative of the current operating conditions of the engine/vehicle. A duty cycle map is defined within the micro-controller by a plurality of sectors bounded by a specific performance curve based on two or more engine operating parameters, such as engine torque and speed. Each sector corresponds to a range of values for the specific operating parameters. During iterations of the monitoring routine, current data indicative of the specific engine operating parameters is sensed and compared with the range of values for each duty cycle sector. A duty cycle parameter, such as elapsed time or fuel consumption, is maintained for each sector. When the current engine operating conditions fall within a particular target sector, its corresponding duty cycle parameter is updated. This process is continued over several iterations to define a duty cycle map over a predetermined number of engine operating hours. In one embodiment, a long term map is accumulated between engine rebuilds, for example. In another embodiment, the long term duty cycle map is augmented by sequentially accessed short term maps, each storing duty cycle information for much shorter engine hours. The duty cycle maps can be used to evaluate engine maintenance requirements or suggest modifications to engine control routines and fueling strategies.
    • 用于监测发动机性能的系统和方法利用与发动机/车辆控制器集成的监控微控制器来接收指示发动机/车辆的当前操作条件的数据。 基于两个或多个发动机工作参数(例如发动机扭矩和速度),通过由特定性能曲线界定的多个扇区在微控制器内定义占空比图。 每个扇区对应于特定操作参数的值范围。 在监视程序的迭代期间,检测指示特定发动机运行参数的当前数据,并将其与每个占空比扇区的值的范围进行比较。 对于每个扇区维持占空比参数,例如经过时间或燃料消耗。 当当前的发动机工作条件落在特定目标扇区内时,其相应的占空比参数被更新。 该过程在多次迭代中持续以在预定数量的发动机运转小时上定义占空比图。 在一个实施例中,例如,在发动机重建之间累积长期地图。 在另一个实施例中,通过顺序访问的短期映射增加长期占空比图,每个存储占空比信息用于短得多的发动机小时。 占空比图可用于评估发动机维护要求或建议对发动机控制程序和加油策略的修改。