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    • 2. 发明申请
    • Electronic control device for aviation engine
    • 航空发动机电子控制装置
    • US20060235601A1
    • 2006-10-19
    • US11394094
    • 2006-03-31
    • Hiroshi UrunoAkira HamauzuKiyoaki YokoyamaHirohisa Kitaura
    • Hiroshi UrunoAkira HamauzuKiyoaki YokoyamaHirohisa Kitaura
    • G06F19/00G06G7/70
    • F02P15/02F02D37/02F02D41/266F02D2250/12F02D2400/08F02P5/1518F02P15/08Y02T10/46
    • An electronic control device is provided for an aviation engine. Each cylinder of the engine is equipped with main ignition plugs and back-up ignition plugs. Lane A including a first CPU and lane B including a second CPU are included in an ECU. The ignition control system is multiplexed by the two lanes A, B. The first and second CPU independently calculate ignition timing for each cylinder based on each sensor signal, and then exchange the results of these calculations with each other. At each cylinder, ignition timing is synchronized in such a manner that ignition timing of the main ignition plugs and ignition timing of the back-up ignition plugs match. The electronic control device so configured has a high level of redundancy with a small number of CPU's. Thus, electronic control device can be provided for the aviation engine with few limitations placed in relation to installation location.
    • 为航空发动机提供电子控制装置。 发动机的每个气缸都装有主火花塞和备用火花塞。 包括第一CPU的通道A和包括第二CPU的通道B包括在ECU中。 点火控制系统由两条通道A,B复用。第一和第二CPU基于每个传感器信号单独计算每个气缸的点火正时,然后将这些计算的结果相互交换。 在每个气缸处,点火正时同步,使得主火花塞的点火正时和备用火花塞的点火正时相匹配。 如此配置的电子控制装置具有很少的CPU的冗余度。 因此,可以为航空发动机提供电子控制装置,相对于安装位置几乎没有限制。
    • 3. 发明授权
    • Electronic control device for aviation engine
    • 航空发动机电子控制装置
    • US07299121B2
    • 2007-11-20
    • US11394094
    • 2006-03-31
    • Hiroshi UrunoAkira HamauzuKiyoaki YokoyamaHirohisa Kitaura
    • Hiroshi UrunoAkira HamauzuKiyoaki YokoyamaHirohisa Kitaura
    • G06F19/00F02P5/00
    • F02P15/02F02D37/02F02D41/266F02D2250/12F02D2400/08F02P5/1518F02P15/08Y02T10/46
    • An electronic control device is provided for an aviation engine. Each cylinder of the engine is equipped with main ignition plugs and back-up ignition plugs. Lane A including a first CPU and lane B including a second CPU are included in an ECU. The ignition control system is multiplexed by the two lanes A, B. The first and second CPU independently calculate ignition timing for each cylinder based on each sensor signal, and then exchange the results of these calculations with each other. At each cylinder, ignition timing is synchronized in such a manner that ignition timing of the main ignition plugs and ignition timing of the back-up ignition plugs match. The electronic control device so configured has a high level of redundancy with a small number of CPU's. Thus, electronic control device can be provided for the aviation engine with few limitations placed in relation to installation location.
    • 为航空发动机提供电子控制装置。 发动机的每个气缸都装有主火花塞和备用火花塞。 包括第一CPU的通道A和包括第二CPU的通道B包括在ECU中。 点火控制系统由两条通道A,B复用。第一和第二CPU基于每个传感器信号独立计算每个气缸的点火正时,然后将这些计算的结果相互交换。 在每个气缸处,点火正时同步,使得主火花塞的点火正时和备用火花塞的点火正时相匹配。 如此配置的电子控制装置具有很少的CPU的冗余度。 因此,可以为航空发动机提供电子控制装置,相对于安装位置几乎没有限制。
    • 4. 发明申请
    • MOTORCYCLE
    • 摩托车
    • US20120188777A1
    • 2012-07-26
    • US13393065
    • 2010-08-31
    • Akira HamauzuKotaro FujiyamaJun Suzuki
    • Akira HamauzuKotaro FujiyamaJun Suzuki
    • B62J6/04
    • B62J6/04B62J15/00
    • A motorcycle wherein an attachment angle of a tail light bulb is increased to reduce a distance between a seat and a tail light unit, to improve the flexibility of a short tail design around a tail light of a motorcycle. The motorcycle includes a rear cowl attached to a rear part of a vehicle body frame, a seat catch arranged on a rear end portion of the vehicle body frame and configured to lock and to unlock an openable/closable seat, a tail light unit arranged behind the seat catch and attached to the rear cowl, a tail light bulb attached to the tail light unit in a forward-tilted state, and a rear fender covering an upper part of a rear wheel WR. An opening that allows access to the tail light bulb is formed at a portion of the rear fender facing the tail light bulb.
    • 一种摩托车,其中增加了尾灯泡的附着角度以减小座椅和尾灯单元之间的距离,以提高围绕摩托车的尾灯的短尾设计的灵活性。 摩托车包括安装在车身框架的后部的后罩,设置在车体框架的后端部的座扣,其构造为锁定和解锁可开闭的座椅,尾灯单元布置在 座椅卡扣并附接到后整流罩,以向前倾斜状态附接到尾灯单元的尾灯,以及覆盖后轮WR的上部的后挡泥板。 在后挡泥板的面向尾灯泡的一部分处形成允许进入尾灯泡的开口。
    • 8. 发明授权
    • Motorcycle
    • 摩托车
    • US08845154B2
    • 2014-09-30
    • US13393065
    • 2010-08-31
    • Akira HamauzuKotaro FujiyamaJun Suzuki
    • Akira HamauzuKotaro FujiyamaJun Suzuki
    • B62J6/00B62J6/04B62J15/00
    • B62J6/04B62J15/00
    • A motorcycle wherein an attachment angle of a tail light bulb is increased to reduce a distance between a seat and a tail light unit, to improve the flexibility of a short tail design around a tail light of a motorcycle. The motorcycle includes a rear cowl attached to a rear part of a vehicle body frame, a seat catch arranged on a rear end portion of the vehicle body frame and configured to lock and to unlock an openable/closable seat, a tail light unit arranged behind the seat catch and attached to the rear cowl, a tail light bulb attached to the tail light unit in a forward-tilted state, and a rear fender covering an upper part of a rear wheel WR. An opening that allows access to the tail light bulb is formed at a portion of the rear fender facing the tail light bulb.
    • 一种摩托车,其中增加了尾灯泡的附着角度以减小座椅和尾灯单元之间的距离,以提高围绕摩托车的尾灯的短尾设计的灵活性。 摩托车包括安装在车身框架的后部的后罩,设置在车体框架的后端部的座扣,其构造为锁定和解锁可开闭的座椅,尾灯单元布置在 座椅卡扣并附接到后整流罩,以向前倾斜状态附接到尾灯单元的尾灯,以及覆盖后轮WR的上部的后挡泥板。 在后挡泥板的面向尾灯泡的部分处形成允许进入尾灯泡的开口。