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    • 21. 发明授权
    • Valve driving apparatus driving a valve apparatus at a high voltage by
connecting two power sources in series
    • 阀驱动装置通过串联连接两个电源来驱动高压阀装置
    • US5537960A
    • 1996-07-23
    • US418345
    • 1995-04-07
    • Takashi IzuoIwao Maeda
    • Takashi IzuoIwao Maeda
    • F01L9/04
    • F01L9/04
    • A valve driving apparatus has a second electric power source in addition to a main electric power source used in an internal combustion engine. The additional electric power source can be connected in series to the main electric power source so as to supply a high voltage to a solenoid used in the valve driving apparatus. The valve driving apparatus has an electromagnetic linear actuator for reciprocating a valve body of the electromagnetic valve apparatus so as to open or close the electromagnetic valve apparatus. The additional electric power source is provided separately from the main power source. A power source switching unit switches a voltage supplied to the electromagnetic linear actuator between the high voltage and a low voltage. The high voltage is generated by connecting the main electrical power source and the additional electric power source in series. The low voltage is generated by either one of the first electric power source and the second electric power source.
    • 除了在内燃机中使用的主电源之外,阀驱动装置还具有第二电力源。 附加电源可以与主电源串联连接,以向阀驱动装置中使用的螺线管提供高电压。 阀驱动装置具有电磁线性致动器,用于使电磁阀装置的阀体往复运动,以打开或关闭电磁阀装置。 附加电源与主电源分开设置。 电源切换单元在高电压和低电压之间切换提供给电磁线性致动器的电压。 通过串联连接主电源和附加电源来产生高电压。 低电压由第一电力源和第二电力源中的任一个产生。
    • 22. 发明授权
    • Apparatus for adjustably mounting a camera on aircraft
    • 用于可调节地将相机安装在飞机上的装置
    • US5365291A
    • 1994-11-15
    • US948672
    • 1992-09-22
    • Iwao Maeda
    • Iwao Maeda
    • B64D47/08G03B15/00G03B17/56G03B37/00G03B39/00
    • B64D47/08G03B15/006
    • A mechanism for mounting a camera on an aircraft, such as a helicopter, comprising a camera housing for holding a camera and a camera support section including a linkage system for mounting the camera housing to the underside of the aircraft in a manner permitting movement between a retracted position proximate the aircraft fuselage and an extended position below the plane of the landing skids to facilitate 360.degree. photography. The mechanism includes a motor driven actuator for positioning the support section between limit positions and a manual back-up system in the event that the motor driven system becomes inoperable.
    • 用于将相机安装在诸如直升机的飞机上的机构,包括用于保持相机的相机外壳和相机支撑部分,所述照相机支撑部分包括用于将相机外壳安装到飞行器的下侧的联动系统, 靠近飞机机身的缩回位置,以及在着陆滑行平面下方的延伸位置,以方便360度摄影。 该机构包括用于在电机驱动系统变得不可操作的情况下将支撑部分定位在极限位置和手动备用系统之间的马达驱动致动器。
    • 25. 发明授权
    • Control apparatus for internal combustion engine using air-amount-first
fuel-amount-second control method
    • 使用空气量第一燃料量 - 第二控制方法的内燃机的控制装置
    • US6014955A
    • 2000-01-18
    • US932541
    • 1997-09-17
    • Ichiro HosotaniHiroshi TanakaNaohide FuwaIwao MaedaShigeo KikoriKen Kuretake
    • Ichiro HosotaniHiroshi TanakaNaohide FuwaIwao MaedaShigeo KikoriKen Kuretake
    • F02D41/00F02D41/10F02D41/34F02D11/10
    • F02D41/34F02D41/0002F02D41/10Y02T10/42Y02T10/44
    • An air-amount-first fuel-amount-second control apparatus for an internal combustion engine having an electronically-controlled throttle valve. The response characteristic of the throttle valve is stored, a target value of the throttle valve opening degree corresponding to the operating position of the accelerator pedal is calculated, the intake air valve closing time of the fuel injection cylinder is calculated in accordance with the engine operating condition, the time required for reaching a target throttle valve opening degree is calculated from the target throttle valve opening degree and the stored value of the response characteristic of the throttle valve, the throttle valve opening degree as of the intake air valve closing time is calculated from the calculated time required for reaching the target throttle valve opening degree and the intake air valve closing time of the fuel injection cylinder. A fuel supply amount constituting a target air-fuel ratio is calculated from the target air-fuel ratio and the intake air amount corresponding to the throttle valve opening degree as of the intake air valve closing time, and the fuel in the calculated amount is supplied to the engine fuel injection cylinder.
    • 一种具有电子节流阀的内燃机的空气量第一燃料量 - 第二控制装置。 存储节流阀的响应特性,计算与加速踏板的运转位置对应的节气门开度的目标值,根据发动机运转来计算燃料喷射气缸的进气门关闭时间 条件是根据目标节气门开度和节流阀的响应特性的存储值计算达到目标节气门开度所需的时间,计算出进气门关闭时间的节气门开度 从达到目标节气门开度所需的计算时间和燃料喷射气缸的进气阀关闭时间。 从目标空燃比和与进气阀关闭时间相应的节气门开度的吸入空气量计算构成目标空燃比的燃料供给量,供给计算量的燃料 到发动机燃油喷射缸。