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    • 1. 发明申请
    • Failure diagnostic system for atmospheric pressure detecting device
    • 大气压力检测装置故障诊断系统
    • US20030126907A1
    • 2003-07-10
    • US10322738
    • 2002-12-19
    • Satoshi NagashimaKenji SaitoHidetugu Kanao
    • G01L027/00
    • F02D41/222F02D41/185F02D2041/228F02D2200/0404F02D2200/0414F02D2200/703F02D2200/704G01L23/24Y02T10/40
    • There is provided a failure diagnostic system for an atmospheric pressure detecting device, which is capable of rationally determining whether that device has failed or not and is capable of improving the diagnostic accuracy. The failure diagnostic system is comprised of an atmospheric pressure sensor for detecting an atmospheric pressure of the air taken into an engine; a condition determination section for determining that conditions required for determining that the atmospheric pressure sensor has failed are satisfied if the number of operations, in each of which the engine continuously operates for a predetermined period of time, has exceeded a predetermined number; and a failure diagnosis section for determining that the atmospheric pressure sensor has failed if a variation in the atmospheric pressure over a period of time equivalent to that predetermined number is equal to or less than a predetermined value and the required conditions have been satisfied.
    • 提供了一种用于大气压检测装置的故障诊断系统,其能够合理地确定该装置是否已经发生故障并且能够提高诊断精度。 该故障诊断系统包括用于检测进入发动机的空气的大气压力的大气压力传感器; 如果发动机连续运行预定时间段的操作次数已经超过预定数量,则满足用于确定确定大气压传感器已经发生故障所需的条件的条件确定部分; 以及故障诊断部,用于如果大于等于该预定值的时间段内的大气压力的变化等于或小于预定值并且满足所需条件,则确定大气压传感器已经失败。
    • 4. 发明授权
    • Fuel supply control apparatus for internal combustion engine
    • 内燃机用燃料供给控制装置
    • US4905155A
    • 1990-02-27
    • US111256
    • 1987-10-19
    • Yoshiaki Kanno
    • Yoshiaki Kanno
    • F02D41/04F02D41/00F02D41/18F02D45/00
    • F02D41/185
    • A fuel supply control apparatus for an internal combustion engine according to the present invention relates to an apparatus, in which the air intake quantity for the internal combustion engine is detected by an air flow sensor and a quantity of a fuel to be supplied to the internal combustion engine is controlled on the basis of an output from said air flow sensor, provided with the air flow sensor and a crank angle sensor for detecting a crank angle of the internal combustion engine and capable of reasonably controlling an air fuel ratio of the internal combustion engine even in the case, where a throttle valve is almost completely opened, by detecting the air intake quantity in a range of a predetermined crank angle interval, determining a resulting value which is proportional to the air intake quantity per one intake stroke of the internal combustion engine, on the basis of the detected value, limiting the resulting value by a predetermined value corrected by parameters of the internal combustion engine, and controlling the quantity of a fuel to be supplied to the internal combustion engine on the basis of the limited resulting value.
    • 根据本发明的用于内燃机的燃料供应控制装置涉及一种装置,其中通过空气流量传感器检测内燃机的进气量和向内部供应的燃料量 基于来自所述空气流量传感器的输出来控制内燃机,所述空气流量传感器设置有空气流量传感器和用于检测内燃机的曲柄角的曲柄角传感器,并且能够合理地控制内燃机的空燃比 即使在通过在预定的曲柄角间隔的范围内检测进气量的情况下,在节气门几乎完全打开的情况下,确定与内部的每个进气冲程的进气量成比例的结果值 内燃机基于检测值,将所得到的值限制在由内部燃烧器的参数校正的预定值 并根据有限的结果值控制供给内燃机的燃料量。
    • 7. 发明授权
    • Vortex shedding device
    • 涡旋脱落装置
    • US4459847A
    • 1984-07-17
    • US322656
    • 1981-11-18
    • Toru Kita
    • Toru Kita
    • F02D41/18G01F1/32G01P5/01G01P5/12
    • F02D41/185G01F1/3272G01P5/01G01P5/12
    • A vortex shedding device for use in measuring air flow rate into an internal combustion engine includes a duct provided therein with an element for forming vortices in air flowing through the duct. A pair of hot wires is located in the duct which are alternately exposed to vortices generated by the vortex forming element. The hot wires are associated with an electric circuit which detects variations in the resistances of the hot wires and determines the frequency at which vortices are generated in air flowing past the vortex forming element. The electric circuit contains a vortex detector for each of the hot wires so that even if one of the hot wires is broken, a pulse signal is still provided during steady operation of the engine.
    • 用于测量进入内燃机的空气流量的涡流脱落装置包括其中设置有用于在流过管道的空气中形成涡流的元件的管道。 一对热丝位于管道中,交替地暴露于由涡流形成元件产生的涡流。 热线与检测热丝电阻变化的电路相关联,并确定在流过涡流形成元件的空气中产生涡流的频率。 电路包含用于每个热丝的涡流检测器,使得即使其中一根热丝断裂,仍然在发动机的稳定运行期间提供脉冲信号。