公开(公告)号：US06758189B2

公开(公告)日：2004-07-06

申请号：US10309008

申请日：2002-12-04

申请人： Mamoru Uraki ,  Sumio Sato ,  Tomoya Kono ,  Hajime Shogase

发明人： Mamoru Uraki ,  Sumio Sato ,  Tomoya Kono ,  Hajime Shogase

IPC分类号： F02D100

CPC分类号： B63H11/08 ,  F02D31/006 ,  F02D41/045

摘要： When a large load is exerted during restraint control of an engine of a jet propulsion boat, the drop of the engine revolution frequency causes a feeling of harsh braking. An engine revolution frequency control apparatus provided to prevent this problem includes a engine revolution frequency detector for detecting an engine revolution frequency, and threshold value setting units for setting first and second engine revolution frequency threshold values. The second threshold value is set to be higher than the first threshold value. An engine control unit includes an overspeed governing capability that starts restraint control for restraining rotation when the engine revolution frequency detected by the engine revolution frequency detector is more than said first threshold value when the engine is accelerating, and terminates restraint control when the engine revolution frequency is less than a second thresholds value during deceleration.

摘要翻译： 当在喷射推进船的发动机的限制控制期间施加大的负载时，发动机转速的下降引起严酷制动的感觉。 用于防止这个问题的发动机转速控制装置包括用于检测发动机转速的发动机转速检测器和用于设定第一和第二发动机转数的频率阈值的阈值设定单元。 将第二阈值设定为高于第一阈值。 发动机控制单元包括超速控制能力，当发动机加速时，当由发动机转速检测器检测到的发动机转速大于所述第一阈值时，开始抑制旋转的约束控制，并且当发动机转速为 在减速期间小于第二个阈值。

公开(公告)号：US06783408B2

公开(公告)日：2004-08-31

申请号：US10351519

申请日：2003-01-27

申请人： Mamoru Uraki ,  Takao Kochi ,  Tomoya Kono ,  Hajime Shogase

发明人： Mamoru Uraki ,  Takao Kochi ,  Tomoya Kono ,  Hajime Shogase

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。

公开(公告)号：US06960105B2

公开(公告)日：2005-11-01

申请号：US10245286

申请日：2002-09-18

申请人： Mamoru Uraki ,  Yoshiaki Hirakata ,  Takao Kochi ,  Hajime Shogase

发明人： Mamoru Uraki ,  Yoshiaki Hirakata ,  Takao Kochi ,  Hajime Shogase

IPC分类号： B63B35/73 ,  B63H11/08 ,  B63H21/14 ,  F02B61/04 ,  B63H21/21

CPC分类号： F02B61/045 ,  B63B35/731 ,  B63H11/08 ,  B63H21/14

摘要： A control unit is provided for increasing the number of engine revolutions per minute to a predetermined number of revolutions per minute when the throttle is closed and when the engine has been rotated for more than a prescribed time period at more than a prescribed number of revolutions per minute, and the throttle has been opened for more than a prescribed time period at more than a prescribed opening. The control unit increases the number of engine revolutions per minute to a predetermined number of revolutions per minute irrespective of the throttle and maintains the same for a predetermined retention time when the steering handle is turned to the left or the right by more than a prescribed angle. The time to start controlling the number of engine revolutions per minute may be delayed by providing a delay time for delaying the time to start controlling the engine revolutions. The number of engine revolutions per minute may be controlled after the hull is underwater. As a consequence, the amount of sideslip of the jet propulsion boat can be improved. In addition, since the control unit for increasing the number of engine revolutions per minute to a predetermined number of revolutions per minute irrespective of the throttle and maintaining the same for a predetermined retention time is provided, the quantity of jet water stream is secured. As a result, the steering of the jet propulsion boat is improved.

摘要翻译： 提供一种控制单元，用于当节气门关闭时将每分钟的发动机转数增加到预定转数，并且当发动机以大于规定转速旋转超过规定时间段时 分钟，并且在超过规定的开度时，节气门已经打开了超过规定的时间段。 控制单元将每分钟的发动机转数增加到每分钟预定转数，而不管节气门，并且当转向手柄向左或向右转动超过规定角度时，将其保持相同的预定保持时间 。 通过提供延迟开始控制发动机转数的时间的延迟时间，可以延迟开始控制每分钟发动机转数的时间。 发动机转数每分钟可以在船体在水下后进行控制。 因此，可以提高喷射推进船的侧滑量。 此外，由于提供了用于将发动机转数每分钟增加到每分钟预定转数而不考虑节气门并且在预定保持时间保持相同的控制单元，所以确保喷射水流的量。 结果，喷气推进船的转向得到改善。

公开(公告)号：US07610748B2

公开(公告)日：2009-11-03

申请号：US11236683

申请日：2005-09-27

申请人： Tomoya Kono ,  Takeru Abe ,  Ryutaro Yamazaki ,  Mamoru Uraki

发明人： Tomoya Kono ,  Takeru Abe ,  Ryutaro Yamazaki ,  Mamoru Uraki

IPC分类号： F01N3/00

CPC分类号： F02B77/086 ,  B62J99/00 ,  B62J2099/002 ,  B62K2207/00 ,  F01N13/008 ,  F01N13/009 ,  F01N13/011 ,  F01N13/107 ,  F01N2560/025 ,  F02B61/02

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 。

公开(公告)号：US20060064964A1

公开(公告)日：2006-03-30

申请号：US11236683

申请日：2005-09-27

申请人： Tomoya Kono ,  Takeru Abe ,  Ryutaro Yamazaki ,  Mamoru Uraki

发明人： Tomoya Kono ,  Takeru Abe ,  Ryutaro Yamazaki ,  Mamoru Uraki

IPC分类号： F01N3/00 ,  F01N7/10

CPC分类号： F02B77/086 ,  B62J99/00 ,  B62J2099/002 ,  B62K2207/00 ,  F01N13/008 ,  F01N13/009 ,  F01N13/011 ,  F01N13/107 ,  F01N2560/025 ,  F02B61/02

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.

公开(公告)号：US07562592B2

公开(公告)日：2009-07-21

申请号：US11236684

申请日：2005-09-27

申请人： Tomoya Kono ,  Takeru Abe ,  Ryutaro Yamazaki ,  Mamoru Uraki

发明人： Tomoya Kono ,  Takeru Abe ,  Ryutaro Yamazaki ,  Mamoru Uraki

IPC分类号： G01D21/00

CPC分类号： F01N13/008 ,  F01N2560/02 ,  F01N2590/04

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。

公开(公告)号：US20060150962A1

公开(公告)日：2006-07-13

申请号：US11315256

申请日：2005-12-23

申请人： Mamoru Uraki ,  Ryutaro Yamazaki ,  Tatsuo Hayashi ,  Tomoya Kono ,  Takeru Abe

发明人： Mamoru Uraki ,  Ryutaro Yamazaki ,  Tatsuo Hayashi ,  Tomoya Kono ,  Takeru Abe

IPC分类号： F02D41/14

CPC分类号： F02D41/1456 ,  F02D41/1479 ,  F02D41/1484 ,  F02D41/1489 ,  F02D2041/2048

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。

公开(公告)号：US20060065041A1

公开(公告)日：2006-03-30

申请号：US11236684

申请日：2005-09-27

申请人： Tomoya Kono ,  Takeru Abe ,  Ryutaro Yamazaki ,  Mamoru Uraki

发明人： Tomoya Kono ,  Takeru Abe ,  Ryutaro Yamazaki ,  Mamoru Uraki

IPC分类号： G01N33/497 ,  G01N7/00 ,  F01N3/00

CPC分类号： F01N13/008 ,  F01N2560/02 ,  F01N2590/04

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.

公开(公告)号：US06796289B2

公开(公告)日：2004-09-28

申请号：US10282199

申请日：2002-10-29

申请人： Mamoru Uraki ,  Sumio Sato ,  Kazunori Okada ,  Kazuhiko Tomoda

发明人： Mamoru Uraki ,  Sumio Sato ,  Kazunori Okada ,  Kazuhiko Tomoda

IPC分类号： F02D1300

CPC分类号： F02D37/02 ,  F02B37/00 ,  F02B37/16 ,  F02B37/18 ,  F02P5/1504 ,  F02P5/1516 ,  Y02T10/144 ,  Y02T10/46

摘要： The burning of unburned fuel in an exhaust pipe is a technique for preventing a turbo lag. However, since the technique requires combustion in the exhaust pipe, the temperature in the exhaust pipe becomes high, which is likely to damage the exhaust pipe, cause the exhaust emissions to deteriorate. The present invention addresses this problem by providing an ignition control apparatus for an engine with a turbocharger, capable of adjusting an ignition timing and a turbocharger. When a throttle valve is opened rapidly, the ignition control apparatus causes the ignition timing to advance with respect to the ordinary ignition timing. Consequently, the start of combustion is advanced, and the speed of rotation of the engine is raised, thereby increasing the speed of an exhaust turbine to achieve the desired increase in engine performance, without the problems of conventional ignition control systems.

摘要翻译： 排气管中未燃燃料的燃烧是用于防止涡轮滞后的技术。 然而，由于该技术需要在排气管中燃烧，排气管内的温度变高，容易损坏排气管，导致废气排放恶化。 本发明通过提供一种具有能够调节点火正时的涡轮增压器的发动机的点火控制装置和涡轮增压器来解决这个问题。 当节气门快速打开时，点火控制装置使得点火正时相对于正常点火正时提前。 因此，燃烧开始进行，并且发动机的转速提高，从而提高排气涡轮机的速度，以达到期望的发动机性能的提高，而没有常规点火控制系统的问题。

公开(公告)号：US20070082568A1

公开(公告)日：2007-04-12

申请号：US11524480

申请日：2006-09-21

申请人： Mamoru Uraki ,  Hideki Sugiyama ,  Junji Higashiyama ,  Takao Kochi

发明人： Mamoru Uraki ,  Hideki Sugiyama ,  Junji Higashiyama ,  Takao Kochi

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。