SILENCER AND ROTATING MACHINE EQUIPPED THEREWITH
    1.
    发明申请
    SILENCER AND ROTATING MACHINE EQUIPPED THEREWITH 有权
    安装和旋转机器

    公开(公告)号:US20130213733A1

    公开(公告)日:2013-08-22

    申请号:US13753063

    申请日:2013-01-29

    IPC分类号: F02C7/24

    摘要: In a silencer, holes are disposed in one row with intervals to each other along one direction, holes forming the one row are disposed in a plurality of rows in a direction perpendicular to the one direction, and positions of the holes in adjacent rows are shifted in the one direction and disposed in a zigzag pattern. A disposition interval of the holes of an outer edge hole row forming one row in at least two sides opposite to each other in the silencing porous plate is set to be larger than a disposition interval of the holes of a row inside the outer edge hole row.

    摘要翻译: 在消音器中,孔沿着一个方向彼此间隔设置成一排,形成一排的孔在垂直于该一个方向的方向上排列成多行,相邻行中的孔的位置偏移 在一个方向上并且以锯齿形图案布置。 在消音多孔板中,至少在彼此相对的两侧形成一排的外边缘孔列的孔的布置间隔被设定为大于外边缘孔列内的一排孔的布置间隔 。

    Variable nozzle device and variable-geometry type exhaust turbocharger

    公开(公告)号:US11015518B2

    公开(公告)日:2021-05-25

    申请号:US16326633

    申请日:2017-03-16

    IPC分类号: F02B37/24 F01D17/16

    摘要: A variable nozzle device includes: a first plate-shaped member having a first plate portion having an annular shape and being fixed to a bearing housing; a second plate-shaped member having a second plate portion which has an annular shape and which defines a nozzle flow passage between the first plate portion and the second plate portion, the second plate portion having a surface disposed so as to face the first plate portion and another surface disposed so as to face at least partially a scroll flow passage formed inside a turbine housing; at least one nozzle support having, with respect to an axial direction of the nozzle support, an end coupled to the first plate portion and another end coupled to the second plate portion; at least one nozzle vane rotatably supported between the first plate portion and the second plate portion; and a variable nozzle mechanism configured to change a vane angle of the at least one nozzle vane. The second plate portion is formed to have a larger thickness than the first plate portion.

    Disc axis adjusting mechanism in gas turbine
    3.
    发明授权
    Disc axis adjusting mechanism in gas turbine 有权
    燃气轮机中的圆盘轴调整机构

    公开(公告)号:US09567873B2

    公开(公告)日:2017-02-14

    申请号:US14376035

    申请日:2013-02-08

    摘要: In a disc axis adjusting mechanism in a gas turbine, the gas turbine has an exhaust gas diffuser provided between a casing wall and a bearing case which are connected to a downstream side of a turbine, a plurality of struts provided at intervals in a circumferential direction, and strut covers coupling an outer diffuser and an inner diffuser of the exhaust gas diffuser so as to cover the struts, and the mechanism comprises: a plurality of air introduction holes formed in the casing wall so as to allow the interior and exterior of the wall to communicate with each other; a sensor unit configured to detect a parameter corresponding to the thermal elongation of each of the struts; and a flow rate adjustor configured to adjust the flow rate of air flowing through each of the air introduction holes based on a detection value detected by the sensor unit.

    摘要翻译: 在燃气轮机的盘轴调整机构中,燃气轮机具有设置在与涡轮的下游侧连接的壳体壁与轴承箱之间的排气扩散器,沿圆周方向间隔设置的多个支柱 以及将排气扩散器的外部扩散器和内部扩散器联接以覆盖支柱的支柱盖,并且该机构包括:形成在壳体壁中的多个空气引入孔,以允许排气扩散器的内部和外部 墙相互沟通; 传感器单元,被配置为检测与每个所述支柱的热伸长相对应的参数; 以及流量调节器,其被配置为基于由所述传感器单元检测到的检测值来调节流过每个所述空气导入孔的空气的流量。

    DISC SHAFT CENTER ADJUSTING MECHANISM IN GAS TURBINE
    4.
    发明申请
    DISC SHAFT CENTER ADJUSTING MECHANISM IN GAS TURBINE 有权
    DISC轴心调节气体涡轮机械

    公开(公告)号:US20150078887A1

    公开(公告)日:2015-03-19

    申请号:US14376035

    申请日:2013-02-08

    IPC分类号: F01D25/30 F01D25/14 F01D9/02

    摘要: In a disc axis adjusting mechanism in a gas turbine, the gas turbine has an exhaust gas diffuser provided between a casing wall and a bearing case which are connected to a downstream side of a turbine, a plurality of struts provided at intervals in a circumferential direction, and strut covers coupling an outer diffuser and an inner diffuser of the exhaust gas diffuser so as to cover the struts, and the mechanism comprises: a plurality of air introduction holes formed in the casing wall so as to allow the interior and exterior of the wall to communicate with each other; a sensor unit configured to detect a parameter corresponding to the thermal elongation of each of the struts; and a flow rate adjustor configured to adjust the flow rate of air flowing through each of the air introduction holes based on a detection value detected by the sensor unit.

    摘要翻译: 在燃气轮机的盘轴调整机构中,燃气轮机具有设置在与涡轮的下游侧连接的壳体壁与轴承箱之间的排气扩散器,沿圆周方向间隔设置的多个支柱 以及将排气扩散器的外部扩散器和内部扩散器联接以覆盖支柱的支柱盖,并且该机构包括:形成在壳体壁中的多个空气引入孔,以允许排气扩散器的内部和外部 墙相互沟通; 传感器单元,被配置为检测与每个所述支柱的热伸长相对应的参数; 以及流量调节器,其被配置为基于由所述传感器单元检测到的检测值来调节流过每个所述空气导入孔的空气的流量。