公开(公告)号：US08027762B2

公开(公告)日：2011-09-27

申请号：US12480169

申请日：2009-06-08

申请人： Yukio Otake ,  Toshiki Kindo

发明人： Yukio Otake ,  Toshiki Kindo

IPC分类号： G08G1/0962 ,  G08G1/16

CPC分类号： B60T7/22 ,  B60W30/10 ,  B60W2550/22 ,  G08G1/164

摘要： A driving assist apparatus 1 that performs driving assist on the basis of a traffic rule of a mobile object includes a traffic rule acquisition unit 11, 12, and 13 acquiring a traffic rule which a mobile object is highly likely to observe in an arbitrary region, and performs driving assist on the basis of the traffic rule acquired by the traffic rule acquisition unit. In particular, the driving assist apparatus includes a region acquisition unit 13 acquiring a traffic rule deviation region where a defined traffic rule in an arbitrary region does not conform to the traffic rule acquired by the traffic rule acquisition unit, or a traffic rule correction unit correcting the traffic rule acquired by the traffic rule acquisition unit when a defined traffic rule in an arbitrary region does not conform to the traffic rule acquired by the traffic rule acquisition unit.

摘要翻译： 基于移动对象的交通规则执行驾驶辅助的行驶辅助装置1包括获取移动对象在任意区域中很可能观察到的交通规则的交通规则获取单元11,12,13， 并且基于由交通规则获取单元获取的交通规则来执行驾驶辅助。 特别地，驾驶辅助装置包括区域获取单元13，其获取任意区域中定义的交通规则不符合由交通规则获取单元获取的交通规则的交通规则偏差区域，或者修正交通规则校正单元 当任意区域中的规定的流量规则不符合由规则获取单元获取的流量规则时由流量规则获取单元获取的流量规则。

公开(公告)号：US06247455B1

公开(公告)日：2001-06-19

申请号：US09407229

申请日：1999-09-27

申请人： Yukio Otake ,  Takashi Hayashi

发明人： Yukio Otake ,  Takashi Hayashi

IPC分类号： F01D1700

CPC分类号： F02D3/02 ,  F02B61/04 ,  F02B75/243 ,  F02D41/38 ,  F02D2041/389 ,  F02D2200/0406 ,  F02M51/02 ,  F02M69/20 ,  F02M69/24 ,  F02M69/467

摘要： An injection quantity control apparatus provided to an internal combustion engine having an injection nozzle which continuously injects fuel is provided. The apparatus includes a fuel quantity adjustment mechanism which has a static pressure chamber and a total pressure chamber to which a static pressure and a total pressure of an intake pipe of said engine are supplied, respectively, and adjusts an amount of fuel supplied to said injection nozzle in accordance with a dynamic pressure between a pressure of said static pressure chamber and a pressure of said total pressure chamber. The apparatus also includes a dynamic pressure corrector which corrects said dynamic pressure so that an air-fuel ratio of the engine is controlled to be substantially a target value. Thus, a desired air-fuel ratio can be achieved without a necessity of a manual operation by an operator.

摘要翻译： 提供一种喷射量控制装置，其设置在具有连续喷射燃料的喷射喷嘴的内燃机中。 该装置包括：燃料量调节机构，其具有静压室和分别供给所述发动机的进气管的静压和总压的总压力室，并且调节供给到所述喷射器的燃料量 喷嘴，其根据所述静压室的压力与所述总压力室的压力之间的动态压力。 该装置还包括动态压力校正器，其校正所述动态压力，使得将发动机的空燃比控制为基本上为目标值。 因此，可以实现期望的空燃比，而不需要操作者的手动操作。

公开(公告)号：US06468035B1

公开(公告)日：2002-10-22

申请号：US09652783

申请日：2000-08-31

申请人： Yukio Otake ,  Shinichiro Tanaka

发明人： Yukio Otake ,  Shinichiro Tanaka

IPC分类号： B64C1136

CPC分类号： F02D29/02 ,  B64C11/305 ,  B64D31/14

摘要： An airplane engine control method and apparatus are provided which form an engine control system easy to operate, which set a reciprocating engine of an airplane in such an operating condition in a partial power mode as to maximize the efficiency of the airframe and the engine as a whole, and which enable setting of suitable partial power in a reciprocating engine with a variable-pitch propeller in such a manner that, when predetermined partial power is set, a relationship expressed by Te ∝ &rgr;N2 is established with respect to the engine torque (Te), the number of engine revolutions (N) and the atmospheric density (&rgr;).

摘要翻译： 提供了一种形成易于操作的发动机控制系统的飞机发动机控制方法和装置，其以部分动力模式将飞机的往复式发动机设置在这样的运行状态，以使机身和发动机的效率最大化为 并且能够以可变螺距螺旋桨在往复式发动机中设定适当的部分功率，使得当设定预定的部分功率时，关于发动机转矩（Te）建立由Te prop rhoN2表示的关系 ），发动机转数（N）和大气密度（rho）。

公开(公告)号：US20120116635A1

公开(公告)日：2012-05-10

申请号：US13383558

申请日：2010-07-09

申请人： Yoshihiro Ohkuwa ,  Yukio Otake

发明人： Yoshihiro Ohkuwa ,  Yukio Otake

IPC分类号： G06G7/70 ,  B62D6/00 ,  G06F7/00

CPC分类号： B60W50/06 ,  B60W50/0098

摘要： A control target processing system includes: a first generating unit that generates first time-series data that are time-series data of an input value; a second generating unit that is formed of a plurality of processing units, that exchanges time-series data among the plurality of processing units, and that calculates intermediate computation values corresponding to the respective input values contained in the input time-series data in the respective processing units to thereby generate second time-series data that are time-series data of the intermediate computation value; a selecting unit that selects a selection value from among the second time-series data in accordance with a first selection condition; and an output unit that calculates and outputs a control variable for controlling a controlled object on the basis of the selection value.

摘要翻译： 控制目标处理系统包括：第一生成单元，其生成作为输入值的时间序列数据的第一时间序列数据; 第二生成单元，其由多个处理单元形成，所述多个处理单元在所述多个处理单元之间交换时间序列数据，并且计算与所述输入时间序列数据中包含的各个输入值对应的中间计算值 从而生成作为中间计算值的时间序列数据的第二时间序列数据; 选择单元，根据第一选择条件从第二时间序列数据中选择选择值; 以及输出单元，其基于所述选择值计算并输出用于控制受控对象的控制变量。

公开(公告)号：US06732521B2

公开(公告)日：2004-05-11

申请号：US10219494

申请日：2002-08-16

申请人： Yukio Otake

发明人： Yukio Otake

IPC分类号： F02D2300

CPC分类号： F02D1/065 ,  B64C11/303 ,  B64C11/305 ,  B64D27/04 ,  B64D31/14 ,  F02C9/48 ,  F02D23/02 ,  F02D31/001 ,  F02D41/0007 ,  F02D41/021 ,  F02D2250/38 ,  F05D2270/05 ,  Y02T10/144

摘要： In the control system for a turbo-charged diesel aircraft engine, the engine speed and the fuel injection amount are controlled by a single control lever in such a manner that the engine speed and the fuel injection amount maintain a predetermined fixed relationship in which the fuel injection amount is always smaller than a smoke limit amount. The control system further includes a boost compensator, that restricts the fuel injection amount to a value less than a boost pressure fuel limit determined by the boost pressure of the engine, and an altitude compensator that restricts the fuel injection amount to the value less than an altitude fuel limit.

摘要翻译： 在用于涡轮增压柴油飞机发动机的控制系统中，发动机转速和燃料喷射量由单个控制杆控制，使得发动机转速和燃料喷射量保持预定的固定关系，其中燃料 喷射量总是小于烟雾限制量。 控制系统还包括升压补偿器，其将燃料喷射量限制为小于由发动机的增压压力确定的增压压力燃料极限的值;以及高度补偿器，其将燃料喷射量限制为小于 高空燃油限制。

公开(公告)号：US06883316B2

公开(公告)日：2005-04-26

申请号：US10600450

申请日：2003-06-23

申请人： Yukio Otake

发明人： Yukio Otake

IPC分类号： B64D31/00 ,  F02B37/00 ,  F02D1/06 ,  F02M59/44 ,  F02D23/00 ,  F02D1/02 ,  F02D41/02 ,  F02D41/04 ,  F04D29/18 ,  F04D29/26

CPC分类号： F02M59/447 ,  B64D31/00 ,  F02B37/00 ,  F02D1/065

摘要： In the control system for a turbo-charged diesel aircraft engine, a target value for a fuel injection amount is determined by the stroke of a throttle lever. A boost compensator determines the maximum limit for the fuel injection amount in accordance with the boost pressure of the engine in order to suppress the formation of exhaust smoke. The actual fuel injection amount is set at the target value or the maximum limit whichever is smaller. An electronic control unit (ECU) calculates an increase rate of the stroke of the throttle lever based on an output of the stroke sensor disposed near the throttle lever. The ECU determines that the current operating condition of the aircraft requires a rapid increase in the engine output power when the increase rate of the stroke is larger than a predetermined value and increases the maximum limit determined by the boost compensator.

摘要翻译： 在涡轮增压柴油飞机发动机的控制系统中，燃料喷射量的目标值由节流杆的行程确定。 增压补偿器根据发动机的增压压力来确定燃料喷射量的最大极限，以抑制排烟的形成。 将实际燃料喷射量设定为目标值或最大极限，以较小者为准。 电子控制单元（ECU）基于设置在油门杆附近的行程传感器的输出来计算节气门杆的行程的增加率。 当行程的增加速度大于预定值并且增加由升压补偿器确定的最大极限值时，ECU确定飞机的当前操作状态需要发动机输出功率的快速增加。

公开(公告)号：US06671588B2

公开(公告)日：2003-12-30

申请号：US10026901

申请日：2001-12-27

申请人： Yukio Otake ,  Kazuya Arakawa

发明人： Yukio Otake ,  Kazuya Arakawa

IPC分类号： B64C1318

CPC分类号： B64C25/48

摘要： The present invention is structured such that, as for travelling on the ground, there is provided a braking mechanism capable of braking wheels by the use of a single brake pedal or a braking mechanism capable of braking the wheels by flare out operation of a control stick, while automatic control of traveling direction is performed in flight using a yaw damper. In addition, a larger braking force is automatically generated, without manual operations by a pilot, for landing gear mounted on the side of an airframe toward which direction of an aircraft is to be changed as compared with the braking force applied to landing gear on the other side.

摘要翻译： 本发明的结构使得对于在地面上行驶，提供了一种制动机构，其能够通过使用单个制动踏板或制动机构来制动车轮，该制动踏板或制动机构能够通过控制杆的展开操作来制动车轮 同时使用偏航阻尼器在飞行中进行行驶方向的自动控制。 另外，与施加到起落架上的制动力相比，自动产生较大的制动力，而不需要飞行员的手动操作，用于安装在机身侧面上的起落架，飞机的方向将改变 另一边。

公开(公告)号：US06652233B2

公开(公告)日：2003-11-25

申请号：US10043242

申请日：2002-01-14

申请人： Yukio Otake

发明人： Yukio Otake

IPC分类号： B64C1134

CPC分类号： B64D31/14 ,  B64D27/04 ,  B64D31/02 ,  F02D1/06 ,  F02D29/02 ,  F02D41/406 ,  F02D2200/602 ,  F02D2200/703 ,  Y02T10/44

摘要： In the control system for a turbo-charged diesel aircraft engine, the engine speed and the fuel injection amount are controlled by a single control lever. However, when the control lever is operated to accelerate the engine, the fuel injection amount immediately increases to the value set by the control lever while the actual speed of the engine requires a relatively long time to reach the set speed. This may cause the actual fuel injection amount to become excessively larger than a value matching the engine speed and to produce exhaust smoke. In order to prevent this problem, the control system includes a delay control device which restricts the rate of increase in the fuel injection amount to a value less than a predetermined maximum value. By restricting the rate of increase in the fuel injection amount, the actual fuel injection amount is maintained at a value matching the actual engine speed during acceleration, and the generation of the exhaust smoke does not occur.

摘要翻译： 在涡轮增压柴油机发动机的控制系统中，发动机转速和燃料喷射量由单个控制杆控制。 然而，当控制杆被操作以加速发动机时，燃料喷射量立即增加到由控制杆设定的值，同时发动机的实际速度需要较长时间才能达到设定速度。 这可能导致实际的燃料喷射量变得过大于与发动机转速匹配的值并产生废气烟雾。 为了防止这种问题，控制系统包括延迟控制装置，其将燃料喷射量的增加率限制为小于预定最大值的值。 通过限制燃料喷射量的增加率，实际燃料喷射量保持在与加速期间的实际发动机转速相匹配的值，并且不会发生排气烟的产生。

公开(公告)号：US4319505A

公开(公告)日：1982-03-16

申请号：US145147

申请日：1980-04-30

申请人： Yukio Otake ,  Yuji Kikuchi ,  Tsuneo Nakanishi ,  Keiji Miyakozawa

发明人： Yukio Otake ,  Yuji Kikuchi ,  Tsuneo Nakanishi ,  Keiji Miyakozawa

IPC分类号： B23D25/06 ,  B23D36/00

CPC分类号： B23D25/06 ,  B23D36/0058 ,  Y10T83/4682 ,  Y10T83/4737 ,  Y10T83/4751

摘要： A pendulum-type flying shear having a speed range of a high speed to a low speed for shearing a hot rolled material having a large cross section in which there are provided vertically movable upper and lower cutting blades within a frame mounted on a crank shaft and the blades are moved towards and away from each other to shear the material while the frame is oscillated. Particularly, while the crank shaft is rotated at a constant speed, the oscillating speed of the frame is synchronized with the speed of movement of the material to be sheared and speed synchronizing apparatus including a gear device and the like is interposed between the oscillating device and the driving device so that a good shearing performance can be obtained with a small capacity of the driving device.

摘要翻译： 一种具有高速到低速的速度范围的摆动式飞剪，用于剪切具有大横截面的热轧材料，其中在安装在曲轴上的框架内设置有可垂直移动的上下切割刀片， 当框架振动时，叶片彼此移动并远离彼此以剪切材料。 特别是在曲轴以恒定速度旋转的同时，框架的摆动速度与要剪切的材料的移动速度同步，包括齿轮装置等的速度同步装置插入振荡装置和 驱动装置能够以较小的驱动装置的容量获得良好的剪切性能。