Mounting structure for an air-fuel ratio sensor in a motorcycle, and exhaust subassembly including same
    1.
    发明授权
    Mounting structure for an air-fuel ratio sensor in a motorcycle, and exhaust subassembly including same 有权
    摩托车中的空燃比传感器的安装结构以及包括其的排气组件

    公开(公告)号:US07610748B2

    公开(公告)日:2009-11-03

    申请号:US11236683

    申请日:2005-09-27

    IPC分类号: F01N3/00

    摘要: A mounting structure is provided for an air-fuel ratio sensor on an exhaust pipe in a motorcycle in which a concentration of oxygen in an exhaust gas can be detected efficiently and accurately by the air-fuel ratio sensor. The air-fuel ratio sensor is mounted on a convergent connector of exhaust pipes, which, in turn, are operatively connected to the cylinders of a multi-cylinder engine. The air-fuel ratio sensor is located upstream of catalytic converters provided in the exhaust pipes, and may be mounted so as to be oriented substantially vertically when the motorcycle is in an upright configuration, or alternatively, may be inclined toward the rear of the motorcycle.

    摘要翻译: 在机动二轮车的排气管上设置空燃比传感器的安装结构,能够通过空燃比传感器有效且准确地检测废气中的氧浓度。 空燃比传感器安装在排气管的会聚连接器上,排气管又连接到多缸发动机的气缸。 空燃比传感器位于设置在排气管内的催化转化器的上游,并且当摩托车处于直立构造时可以安装成基本垂直地定向,或者可以朝向摩托车的后部倾斜 。

    Jet-propelled watercraft
    2.
    发明授权
    Jet-propelled watercraft 有权
    喷气推进的船只

    公开(公告)号:US07364481B2

    公开(公告)日:2008-04-29

    申请号:US11524480

    申请日:2006-09-21

    IPC分类号: B63H21/22 B63H11/00

    CPC分类号: F02M23/06 Y02T10/146

    摘要: A jet-propelled watercraft capable of maintaining a propulsion force required for a turn made at the same time as closing of a throttle valve. The jet-propelled watercraft has an auxiliary intake valve and an ECU. The auxiliary intake valve in an intake pipe opens/closes an auxiliary intake passage to bypass a throttle valve. The ECU performs control such that an opening of the auxiliary intake valve in a state where the rotation speed of the engine is not lower than a threshold value is larger than the opening of the auxiliary intake valve in a state where the engine is idling. When in a state where the rotation speed is not lower than the threshold value, it is detected that the throttle valve is completely closed and that a steering mechanism has been turned by a prescribed angle or more, a current opening of the auxiliary intake valve is maintained.

    摘要翻译: 能够在关闭节流阀的同时保持转弯所需的推进力的喷气推进船只。 喷气式船舶具有辅助进气阀和ECU。 进气管中的辅助进气门打开/关闭辅助进气通道以绕过节流阀。 ECU执行控制,使得在发动机的转速不低于阈值的状态下的辅助进气门的打开大于在发动机空转的状态下的辅助进气门的打开。 当处于旋转速度不低于阈值的状态时,检测到节气门完全关闭,并且转向机构已经转动规定角度以上,辅助进气门的电流开度为 保持。

    Jet-propelled watercraft
    4.
    发明申请
    Jet-propelled watercraft 有权
    喷气推进的船只

    公开(公告)号:US20070082568A1

    公开(公告)日:2007-04-12

    申请号:US11524480

    申请日:2006-09-21

    IPC分类号: F02B61/04

    CPC分类号: F02M23/06 Y02T10/146

    摘要: A jet-propelled watercraft capable of maintaining a propulsion force required for a turn made at the same time as closing of a throttle valve. The jet-propelled watercraft has an auxiliary intake valve and an ECU. The auxiliary intake valve in an intake pipe opens/closes an auxiliary intake passage to bypass a throttle valve. The ECU performs control such that an opening of the auxiliary intake valve in a state where the rotation speed of the engine is not lower than a threshold value is larger than the opening of the auxiliary intake valve in a state where the engine is idling. When in a state where the rotation speed is not lower than the threshold value, it is detected that the throttle valve is completely closed and that a steering mechanism has been turned by a prescribed angle or more, a current opening of the auxiliary intake valve is maintained.

    摘要翻译: 能够在关闭节流阀的同时保持转弯所需的推进力的喷气推进船只。 喷气式船舶具有辅助进气阀和ECU。 进气管中的辅助进气门打开/关闭辅助进气通道以绕过节流阀。 ECU执行控制,使得在发动机的转速不低于阈值的状态下的辅助进气门的打开大于在发动机空转的状态下的辅助进气门的打开。 当处于旋转速度不低于阈值的状态时,检测到节气门完全关闭,并且转向机构已经转动规定角度以上,辅助进气门的当前开度为 保持。

    Jet propulsion boat
    5.
    发明授权
    Jet propulsion boat 有权
    喷气推进船

    公开(公告)号:US06783408B2

    公开(公告)日:2004-08-31

    申请号:US10351519

    申请日:2003-01-27

    IPC分类号: B63H2300

    CPC分类号: B63B35/731 B63H21/213

    摘要: A controller that executes engine output control that a throttle is closed when a boat is navigated at a predetermined speed or higher and the output of an engine is gradually increased up to predetermined output when a steering system is steered right or left at a predetermined angle or more is provided. Thus, an overshoot phenomenon that the engine speed is held at a predetermined engine speed after the engine speed once increases up to the predetermined engine speed or higher when the engine speed is increased in deceleration can be avoided. As a result, the body of the boat can be prevented from sliding laterally to a great extent at the beginning of turning and the turning performance of the body can be enhanced.

    摘要翻译: 执行发动机输出控制的控制器,当以预定速度或更高速度导航船舶时,节气门关闭,并且当转向系统以预定角度向右或向左转向时,发动机的输出逐渐增加到预定输出;或者 提供更多。 因此,可以避免发动机转速在发动机转速一旦增加到预定的发动机转速或更高时在发动机转速减速增加时将发动机转速保持在预定发动机转速的过冲现象。 结果,可以防止在转弯开始时船的主体在很大程度上横向滑动,并且能够提高车身的转弯性能。

    Mounting structure for an air-fuel ratio sensor in a motorcycle, and exhaust subassembly including same
    6.
    发明授权
    Mounting structure for an air-fuel ratio sensor in a motorcycle, and exhaust subassembly including same 失效
    摩托车中的空燃比传感器的安装结构以及包括其的排气组件

    公开(公告)号:US07562592B2

    公开(公告)日:2009-07-21

    申请号:US11236684

    申请日:2005-09-27

    IPC分类号: G01D21/00

    摘要: A mounting structure for an air-fuel ratio sensor in a motorcycle is provided which eliminates the influence of water gathered in an exhaust pipe upon the air-fuel ratio sensor and improves the mountability of the air-fuel ratio sensor to the exhaust pipe. The air-fuel ratio sensor is mounted on an exhaust pipe connected to an engine in a motorcycle so that the air-fuel ratio sensor extends radially with respect to a longitudinal axis of the exhaust pipe, and is inclined upward by an angle of 10° or more with respect to a horizontal line H passing through the center of the exhaust pipe 32 in its cross section. The air-fuel ratio sensor is pointed toward the central lateral plane of the motorcycle as viewed in front elevation of the motorcycle.

    摘要翻译: 提供了一种摩托车中的空燃比传感器的安装结构,其消除了排出管中聚集的水对空燃比传感器的影响,并提高了空燃比传感器与排气管的安装性。 空燃比传感器安装在与摩托车中的发动机连接的排气管上,使得空燃比传感器相对于排气管的纵向轴线径向延伸,并且向上倾斜10°的角度 以上,相对于在其横截面中穿过排气管32的中心的水平线H。 当摩托车的前视图观察时,空燃比传感器指向摩托车的中心侧面。

    Air-fuel ratio feedback control apparatus for engines
    7.
    发明申请
    Air-fuel ratio feedback control apparatus for engines 审中-公开
    发动机空燃比反馈控制装置

    公开(公告)号:US20060150962A1

    公开(公告)日:2006-07-13

    申请号:US11315256

    申请日:2005-12-23

    IPC分类号: F02D41/14

    摘要: An air-fuel ratio setting section sets a target air-fuel ratio KCMD according to the conditions of an engine. An air-fuel ratio correction coefficient calculating section calculates an air-fuel ratio correction coefficient KAF for controlling the air-fuel ratio wherein a detected air-fuel ratio KACT detected by a LAF sensor is converged to the target air-fuel ratio KCMD. A lower limit section constrains the air-fuel ratio correction coefficient KAF so as not to underrun the lower limit value. An upper limit section constrains the air-fuel ratio correction coefficient KAF so as not to exceed the upper limit value. A basic fuel injection time determining section calculates a basic fuel injection time TIM. A fuel injection time calculating section calculates a fuel injection time TOUT based on the target air-fuel ratio KCMD, the air-fuel ratio correction coefficient KAF, the basic fuel injection time TIM or the like, and various engine parameters.

    摘要翻译: 空燃比设定部根据发动机的条件设定目标空燃比KCMD。 空燃比校正系数计算部分计算用于控制由LAF传感器检测到的检测空燃比KACT会聚到目标空燃比KCMD的空燃比的空燃比校正系数KAF。 下限部限制空燃比修正系数KAF,以便不低于下限值。 上限部分将空燃比校正系数KAF限制为不超过上限值。 基本燃料喷射时间确定部计算基本燃料喷射时间TIM。 燃料喷射时间计算部分基于目标空燃比KCMD,空燃比校正系数KAF,基本燃料喷射时间TIM等以及各种发动机参数来计算燃料喷射时间TOUT。

    Jet propulsion boat
    9.
    发明申请
    Jet propulsion boat 有权
    喷气推进船

    公开(公告)号:US20060009095A1

    公开(公告)日:2006-01-12

    申请号:US11226098

    申请日:2005-09-14

    IPC分类号: B63H11/103

    CPC分类号: B63H11/08

    摘要: To provide a jet propulsion boat that enables preventing the occurrence of cavitation. In a jet propulsion boat that jets water pressurized and accelerated by a water jet pump from a rear jet nozzle and is propelled by its reaction, a turbocharger is provided to an engine for driving the water jet pump and in case the rate of the rise of engine speed is a predetermined value or more, delay control is applied to the rise of the boost pressure of the turbocharger.

    摘要翻译: 提供能够防止气蚀发生的喷气推进船。 在喷气式推进艇中,喷水由喷水泵从后喷气喷嘴加压和加速,并被其反应推动,涡轮增压器被提供给用于驱动喷水泵的发动机, 发动机转速为规定值以上时,对涡轮增压器的增压压力的上升进行延迟控制。

    Engine control unit
    10.
    发明授权
    Engine control unit 有权
    发动机控制单元

    公开(公告)号:US06971930B2

    公开(公告)日:2005-12-06

    申请号:US10827939

    申请日:2004-04-19

    摘要: To provide an engine control unit that can easily realize reacceleration in a jet propulsion boat. In a controller mounted in a jet propulsion boat that jets water pressurized and accelerated by a water jet pump from a rear jet and is propelled by its reaction, in case a throttle angle of an engine narrows in a state in which the speed of the engine that drives the water jet pump is equal to or exceeds a predetermined value, advance angle control is made over the ignition timing of the engine.

    摘要翻译: 提供可以容易地实现喷气推进船中的再加速的发动机控制单元。 在安装在喷气式推进船中的控制器中,喷射由喷射泵从后喷射器加压和加速的水并通过其反作用力推动,在发动机的节气门角度在发动机的速度变窄的情况下, 驱动水喷射泵等于或超过预定值时,对发动机的点火正时进行提前角控制。