Power supply control system for heater used in gas sensor

    公开(公告)号:US06578563B2

    公开(公告)日:2003-06-17

    申请号:US10202865

    申请日:2002-07-26

    IPC分类号: F02D4100

    摘要: A heater power supply control system is provided for controlling the temperature of a heater used to heat a solid electrolyte-made sensor element of a gas concentration sensor up to a desired activation temperature. The heater power supply control system measures a resistance value of the sensor element and controls an electric power supply to the heater using a PI control function. The heater power supply control system works to limit the value of an integral term of the PI control function in the course of activation of the sensor element, thereby avoiding overshoot of the resistance value of the sensor element, which avoids thermal damage of the sensor element.

    Gas concentration sensing apparatus
    13.
    发明授权
    Gas concentration sensing apparatus 有权
    气体浓度检测装置

    公开(公告)号:US06453724B1

    公开(公告)日:2002-09-24

    申请号:US09399949

    申请日:1999-09-20

    IPC分类号: G01N700

    摘要: A gas concentration sensor comprises a pump cell for detecting an oxygen concentration in an exhaust gas and a sensor cell for detecting a NOx concentration in the exhaust gas. A porous diffusive layer is interposed between these cells. Furthermore, the sensor comprises a heater for heating these cells. A control circuit produces a sensor cell voltage having an A.C. component to detect the impedance of sensor cell. The electric power supplied to the heater is controlled based on a detected impedance value of the sensor cell.

    摘要翻译: 气体浓度传感器包括用于检测排气中的氧浓度的泵室和用于检测废气中的NOx浓度的传感器单元。 这些细胞之间插入多孔扩散层。 此外,传感器包括用于加热这些电池的加热器。 控制电路产生具有交流分量的传感器电池电压,以检测传感器单元的阻抗。 基于检测到的传感器单元的阻抗值来控制提供给加热器的电力。

    Braking force retaining unit
    15.
    发明授权
    Braking force retaining unit 有权
    制动力保持单元

    公开(公告)号:US06370466B1

    公开(公告)日:2002-04-09

    申请号:US09549165

    申请日:2000-04-13

    IPC分类号: B60K4124

    CPC分类号: B60T7/122

    摘要: A braking force retaining unit, which retains braking force until driving force for starting a vehicle increases to a certain value such that the braking force continues to act on the vehicle after releasing a brake pedal, wherein said braking force retaining unit having a device for decreasing the braking force in accordance with the increasing driving force.

    摘要翻译: 制动力保持单元,其保持直到用于起动车辆的驱动力的制动力增加到一定值,使得在释放制动踏板之后制动力继续作用在车辆上,其中所述制动力保持单元具有用于减小的装置 制动力按照增加的驱动力。

    Cooling system of ring segment and gas turbine
    16.
    发明授权
    Cooling system of ring segment and gas turbine 有权
    环段和燃气轮机的冷却系统

    公开(公告)号:US08550778B2

    公开(公告)日:2013-10-08

    申请号:US12763723

    申请日:2010-04-20

    IPC分类号: F01D5/18

    摘要: In a cooling system of ring segment that cools a ring segment of a gas turbine, the segment body of the ring segment is constituted from a collision plate that has a small hole that blows out cooling air, a cooling space that is enclosed by the collision plate and the main body of the segment body; a first cavity that receives the cooling air from the cooling space; and a first cooling passage, of which one end communicates with the first cavity, and the other end blows out the cooling air from openings that are arranged in the side end portion into combustion gas; the openings of the first cooling passages being arranged so that the arrangement pitch of the openings becomes smaller or the opening area of the openings becomes larger on the upstream in the flow direction of the combustion gas than the openings on the downstream, and are arranged so that the arrangement pitch of the openings becomes larger or the opening area of the openings becomes smaller on the downstream in the flow direction of the combustion gas than the openings on the upstream.

    摘要翻译: 在冷却燃气轮机的环段的环段的冷却系统中,环段的节段主体由具有吹出冷却空气的小孔的碰撞板,被碰撞包围的冷却空间构成 板体和主体的主体; 从冷却空间接收冷却空气的第一腔; 以及第一冷却通路,其一端与第一空腔连通,另一端从布置在侧端部的开口吹出冷却空气为燃烧气体; 第一冷却通道的开口被布置成使得开口的排列间距变得更小,或者在燃烧气体的流动方向上游的开口面积比下游的开口更大,并且被布置成 在燃烧气体的流动方向的下游,开口的排列间距比上游的开口变大,开口的开口面积变小。

    Gas turbine blade, manufacturing method therefor, and gas turbine using turbine blade
    17.
    发明授权
    Gas turbine blade, manufacturing method therefor, and gas turbine using turbine blade 有权
    燃气轮机叶片及其制造方法,以及使用涡轮叶片的燃气轮机

    公开(公告)号:US08506251B2

    公开(公告)日:2013-08-13

    申请号:US13093437

    申请日:2011-04-25

    IPC分类号: F01D5/18

    摘要: Gas turbine blades which simplify the formation of cooling channels provided inside the turbine blades while simultaneously avoiding loss of turbine blade strength and rigidity due to forming of the cooling channels. Cooling channels provided in the interior of a gas turbine blade include a plurality of straight channel-like base-side elongated holes extending in a longitudinal direction at a base side of the turbine blade, a plurality of straight channel-like tip-side elongated holes extending in a longitudinal direction at a tip side of the turbine blade, and a plurality of communicating hollow portions interposed at connection portions between the two types of elongated holes to allow the two types of elongated holes to communicate with each other, and have larger cross-sectional areas than the channel cross-sectional areas of both elongated holes. The communicating hollow portions are formed to match the position of a platform portion of the turbine blade.

    摘要翻译: 燃气轮机叶片,其简化了设置在涡轮机叶片内部的冷却通道的形成,同时避免了由于形成冷却通道而导致的涡轮机叶片强度和刚度的损失。 设置在燃气轮机叶片的内部的冷却通道包括在涡轮机叶片的基部侧沿纵向延伸的多个直的通道状的基本侧的细长孔,多个直的通道状的顶端侧的长孔 在涡轮机叶片的前端侧沿长度方向延伸;以及多个连通的中空部,插入在两种类型的长孔之间的连接部分处,以允许两种类型的细长孔彼此连通,并具有较大的十字形 横截面积比两个长孔的通道横截面积。 连通的中空部分形成为与涡轮叶片的平台部分的位置相匹配。

    Cooling system of ring segment and gas turbine
    18.
    发明授权
    Cooling system of ring segment and gas turbine 有权
    环段和燃气轮机的冷却系统

    公开(公告)号:US08480353B2

    公开(公告)日:2013-07-09

    申请号:US12913397

    申请日:2010-10-27

    IPC分类号: F04D29/58

    摘要: A cooling system of a ring segment for a gas turbine, which includes first cooling passages disposed in an axial direction of the rotating shaft of a main body of the segment body, second cooling passages disposed at one end portion in a direction approximately perpendicular to the first cooling passages, and blowing a cooling air toward the end portion of a neighboring segment body, and third cooling passages connecting a first cavity, which is disposed approximately perpendicular to the axial direction of the rotating shaft at the upstream-end portion, with a cooling space, which is surrounded by the segment body and a collision plate having a plurality of small holes. The first cooling passages include cooling passages of a first region and a second region having a smaller passage cross-sectional area than the first-region cooling passages or a greater arrangement pitch than the first-region cooling passages.

    摘要翻译: 一种用于燃气轮机的环段的冷却系统,其包括沿着所述节段主体的主体的轴的轴向设置的第一冷却通道,第二冷却通道,其设置在大致垂直于所述节段主体的方向的一个端部处 第一冷却通道,朝向相邻段体的端部吹送冷却空气;以及第三冷却通道,其将在上游侧部分大致垂直于旋转轴的轴向设置的第一空腔与第一空腔连接, 冷却空间,其被节段主体包围,具有多个小孔的碰撞板。 第一冷却通道包括具有比第一区域冷却通道更小的通道横截面面积的第一区域和第二区域的冷却通道或比第一区域冷却通道更大的排列间距。

    Method for determining and calculating work related incentives
    19.
    发明授权
    Method for determining and calculating work related incentives 失效
    确定和计算工作相关激励的方法

    公开(公告)号:US08433599B2

    公开(公告)日:2013-04-30

    申请号:US13178646

    申请日:2011-07-08

    申请人: Satoshi Hada

    发明人: Satoshi Hada

    IPC分类号: G06Q10/00

    摘要: A fair incentive calculating method with a reasonable amount of computation is performed by inputting a set of x jobs X={1, 2, . . . , x} and processing times of each worker {t(i)} (1≦i≦n) and providing a set of jobs W(A, X, t(i), t(−i)) assigned to each worker i, where A is a given scheduling algorithm; determining MaxInc(X, t(i)) by recursively solving MaxInc(X, t(i))=Σ_{wεX} t(i, Kind(w))+max_{s(i) εSlower(t(i))} MaxInc(X, s(i)); and using the step of determining MaxInc(X, t(i)) to calculate an incentive NewInc(A, X, t(i), t(−i)) for each worker i based on NewInc(A, X, t(i), t(−i))=Σ_{wεW(A, X, t(i), t(−i))} t(i, Kind(w))+max_{s(i) εSlower(t(i))} MaxInc(X, s(i)).

    摘要翻译: 通过输入一组x作业X = {1,2,...)来执行具有合理计算量的公平激励计算方法。 。 。 ,x}和每个工人{t(i)}(1 @ i @ n)的处理时间,并提供分配给每个工人i的一组作业W(A,X,t(i),t(-i) ,其中A是给定的调度算法; 通过递归求解MaxInc(X,t(i))= Sigma_ {wepsilon X} t(i,Kind(w))+ max_ {s(i)epsilonSlower(t(i))来确定MaxInc(X,t } MaxInc(X,s(i)); 并且使用确定MaxInc(X,t(i))的步骤来基于NewInc(A,X,t(i))来计算每个工人i的激励NewInc(A,X,t(i),t(-i) i(i),t(-i))= Sigma_ {wepsilonW(A,X,t(i),t(-i))} t(i,Kind(w))+ max_ {s(i) i))} MaxInc(X,s(i))。

    TURBINE BLADE AND GAS TURBINE
    20.
    发明申请
    TURBINE BLADE AND GAS TURBINE 有权
    涡轮叶片和气体涡轮

    公开(公告)号:US20120263603A1

    公开(公告)日:2012-10-18

    申请号:US13307675

    申请日:2011-11-30

    申请人: Satoshi Hada

    发明人: Satoshi Hada

    IPC分类号: F01D5/18

    摘要: A turbine blade includes: a base portion fixed to a rotor; a platform that is fixed to the base portion and includes a cooling flow channel; a blade shape portion that extends from the platform to an outer side in a radial direction; and a fillet portion provided in a joint surface between the blade shape portion and the platform, and the turbine blade further includes: a main pipe that is branched off from the cooling flow channel and has an opening at a side end portion of the platform; and a branch pipe that is branched off from the main pipe, extends along the fillet portion so as to be close thereto on an inner side in the radial direction, and includes a film cooling hole opened on a surface of the platform.

    摘要翻译: 涡轮叶片包括:固定到转子的基部; 平台,其固定在所述基部上并且包括冷却流路; 从所述平台向径向外侧延伸的叶片形状部; 以及设置在所述叶片形状部和所述平台之间的接合面的圆角部,所述涡轮叶片还包括:主管,其从所述冷却流路分支并且在所述平台的侧端部具有开口; 并且从主管分支的分支管沿着圆角部分在径向内侧上靠近其延伸,并且包括在平台的表面上开口的薄膜冷却孔。