TRICYCLIC COMPOUNDS
    21.
    发明申请
    TRICYCLIC COMPOUNDS 审中-公开
    三聚体化合物

    公开(公告)号:US20090181942A1

    公开(公告)日:2009-07-16

    申请号:US12090870

    申请日:2006-10-23

    摘要: The present invention relates to tricyclic compounds each represented by the following formula (I): (wherein, R1, R2, R2′, R3, R4, X, Y and Z have the same meanings as defined in the specification); and a drug containing the compound.Since the compounds according to the present invention exhibit an excellent squalene synthetase inhibitory effect and cholesterol synthesis inhibitory effect so that they are useful as a drug such as preventive and/or remedy for diseases in mammals including humans such as hyperlipemia, e.g., hypercholesterolemia, hypertriglyceridemia, and low HDL cholesterolemia and/or arteriosclerosis.

    摘要翻译: 本发明涉及由下式(I)表示的三环化合物:(其中,R1,R2,R2',R3,R4,X,Y和Z与说明书中定义相同); 和含有该化合物的药物。 由于根据本发明的化合物表现出优异的角鲨烯合成酶抑制作用和胆固醇合成抑制作用,因此它们可用作诸如高脂血症(例如高胆固醇血症,高甘油三酯血症)的哺乳动物疾病的预防和/或治疗药物 ,和低HDL胆固醇血症和/或动脉硬化。

    Gas turbine combustor including a diffusion nozzle assembly with a
double cylindrical structure
    22.
    发明授权
    Gas turbine combustor including a diffusion nozzle assembly with a double cylindrical structure 失效
    燃气轮机燃烧器包括具有双圆柱结构的扩散喷嘴组件

    公开(公告)号:US5450725A

    公开(公告)日:1995-09-19

    申请号:US266591

    申请日:1994-06-28

    摘要: A gas turbine combustor comprises a cylindrical outer casing having one end closed by a header plate. A combustor liner provided with an inner combustion chamber which is divided into a first-stage combustion region on a side of the header plate and a second-stage combustion region formed on a downstream side of the first-stage combustion region. A first-stage fuel supply unit mounted to the header plate for injecting a first-stage fuel to the first-stage combustion region and a second-stage fuel supply unit mounted to the header plate for injecting a second-stage fuel previously mixed in a lean fuel state. The first-stage fuel supply unit includes a first-stage fuel nozzle assembly, which supplies the first-stage fuel, formed by combining a diffusion combustion nozzle and a pre-mixture combustion nozzle. The pre-mixture combustion nozzle has, at an intermediate portion thereof, a pre-mixing portion for preliminarily mixing the first-stage fuel with an air, and the pre-mixing portion having a diameter in a downstream portion thereof smaller than that of an upstream portion thereof so as to form a pre-mixed flow into a contraction flow. The pre-mixing fuel nozzle of the first stage fuel nozzle assembly is disposed so as to surround the diffusion combustion nozzle disposed in a central portion thereof.

    摘要翻译: 燃气轮机燃烧器包括一个圆柱形的外壳,其一端通过集管板封闭。 一种燃烧器衬套,其具有内燃室,该内燃室被分为集管板一侧的第一级燃烧区域和形成在第一级燃烧区域的下游侧的第二级燃烧区域。 第一级燃料供给单元,安装到集管板,用于将第一级燃料喷射到第一级燃烧区域;以及第二级燃料供应单元,安装到集管板,用于将预混合在第一级燃料中的第二级燃料 贫燃状态。 第一级燃料供给单元包括:第一级燃料喷嘴组件,其供给通过组合扩散燃烧喷嘴和预混合燃烧喷嘴形成的第一级燃料。 预混合燃烧喷嘴在其中间部分具有用于预先混合第一级燃料与空气的预混合部分,并且预混合部分的下游部分中的直径小于 上游部分,以形成预混合流入收缩流。 第一级燃料喷嘴组件的预混合燃料喷嘴设置成围绕设置在其中心部分的扩散燃烧喷嘴。

    Rotating device and light beam deflecting apparatus
    25.
    发明授权
    Rotating device and light beam deflecting apparatus 失效
    旋转装置和光束偏转装置

    公开(公告)号:US5946122A

    公开(公告)日:1999-08-31

    申请号:US840671

    申请日:1997-04-29

    CPC分类号: G02B26/121

    摘要: In a rotating device which comprises a rotor; a radial bearing; a lower thrust bearing; a dynamic pressure generating means, a radial bearing area (mm.sup.2) which is the area of the rotor facing the radial bearing, a thrust bearing area (mm.sup.2) which is the area of the rotor facing the lower thrust bearing, and the rotor weight (g) are determined so as to satisfy the following formula:(a radial bearing area)/(thrust bearing area).times.(rotor weight)

    摘要翻译: 在包括转子的旋转装置中; 径向轴承; 下推力轴承; 动压发生装置,面向径向轴承的转子面积的径向支承面积(mm2),面向下推力轴承的转子面积的推力承载面积(mm2)和转子重量( g)被确定为满足下式:(径向轴承面积)/(推力承载面积)×(转子重量)<300。

    Gas turbine combustor with nozzle pressure ratio control
    26.
    发明授权
    Gas turbine combustor with nozzle pressure ratio control 失效
    燃气轮机燃烧器与喷嘴压力比控制

    公开(公告)号:US5311742A

    公开(公告)日:1994-05-17

    申请号:US982583

    申请日:1992-11-27

    CPC分类号: F23R3/34 F05D2270/31

    摘要: A gas turbine combustor for a gas turbine power plant comprises a combustion liner connected to a turbine and provided with a main fuel nozzle assembly and a sub-fuel nozzle assembly for jetting fuel to an inside of the combustion liner through nozzle holes, a base fuel supply line, a main fuel line for supplying a fuel to the main nozzle assembly for premixing an air with the fuel jetted through the nozzle hole for carrying out a lean burning in the combustion liner, and a plurality of sub-fuel lines for supplying the fuel to the sub-fuel nozzle assembly for mixing the fuel with a combustion air for carrying out a diffusion burning in the combustion liner. The main and sub-fuel lines branch off a front end of the base fuel supply line. Distributing valves are incorporated in the main fuel line and at least one of the sub-fuel lines for distributing the fuel into the main and sub-fuel lines and degree of openings of the distributing valves are controlled by a control unit for controlling a fuel distribution ratio. The sub-fuel nozzle assembly includes a swirler provided with swirling vanes at an end portion inserted in the combustion liner for swirling the fuel therein The swirling vanes are provided with a combustion air passage to which the nozzle holes of the sub-fuel nozzle assembly are opened.

    摘要翻译: 用于燃气轮机发电厂的燃气轮机燃烧器包括连接到涡轮机的燃烧衬套,并且设置有主燃料喷嘴组件和用于通过喷嘴孔将燃料喷射到燃烧衬套的内部的副燃料喷嘴组件,基础燃料 供应管线,用于向主喷嘴组件供应燃料的主燃料管线,用于预先混合通过喷嘴孔喷射的燃料的空气,以在燃烧衬套中进行稀燃;以及多个副燃料管线, 燃料到副燃料喷嘴组件,用于将燃料与用于在燃烧衬套中进行扩散燃烧的燃烧空气混合。 主燃料和副燃料管线从基础燃料供应管线的前端分支。 分配阀被并入主燃料管线中,并且用于将燃料分配到主和副燃料管线中的至少一个子燃料管线和分配阀的开口程度由用于控制燃料分配的控制单元控制 比。 副燃料喷嘴组件包括在插入在燃烧衬套中的端部处设置有旋动叶片的旋流器,用于在其中旋转燃料。涡流叶片设置有燃烧空气通道,副燃料喷嘴组件的喷嘴孔 开了

    Bicycle ergometer and eddy current brake therefor
    27.
    发明授权
    Bicycle ergometer and eddy current brake therefor 失效
    自行车测力计和涡流制动器

    公开(公告)号:US4800310A

    公开(公告)日:1989-01-24

    申请号:US748675

    申请日:1985-06-25

    摘要: A bicycle ergometer includes an eddy current brake having a flywheel rotor assembly including an inner part of iron material having a carbon content of 0.12% or less and a silicon content of 0.35% or less, a stator provided inside the rotor assembly, a plurality of exciting coils provided on the stator, and a power source for energizing the exciting coils. The outer part of the flywheel rotor can be made of concrete. The ergometer includes an input panel for inputting physical attributes of the user, e.g., age and sex, a pulse sensor for measuring the heart rate of the user at rest and during exercise on the ergometer, an arithmetic control circuit for calculating a training program and heart rate range and for controlling the eddy current brake to present a load to the user which will maintain the user's heart rate in a predetermined range. The method of using the ergometer enables a user to select a physical strength program and a weight reduction program with the selected program reflecting the age, sex, and the present physical condition of the user.

    摘要翻译: 自行车测力计包括具有飞轮转子组件的涡流制动器,所述飞轮转子组件包括碳含量为0.12%以下且硅含量为0.35%以下的铁材料的内部,设置在转子组件内部的定子, 设置在定子上的励磁线圈和用于激励励磁线圈的电源。 飞轮转子的外部部分可以由混凝土制成。 测力计包括用于输入用户的物理属性的输入面板,例如年龄和性别,用于测量休息时和运动时在测力计上的用户的心率的脉搏传感器,用于计算训练程序的算术控制电路, 并且用于控制涡流制动以向用户呈现将使用户心率保持在预定范围内的负载。 使用测力计的方法使得用户能够使用所选择的程序来选择体力计划和减重程序,以反映用户的年龄,性别和当前身体状况。