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34 条记录 (耗时 0.025 秒)

    Cassette clamping mechanism
    4.
    发明授权
    Cassette clamping mechanism 有权
    盒式夹紧机构

    公开(公告)号：US07712802B2

    公开(公告)日：2010-05-11

    申请号：US11451050

    申请日：2006-06-12

    申请人： David L. Williams ,  Michael Bowman

    发明人： David L. Williams ,  Michael Bowman

    IPC分类号： B65D45/00

    CPC分类号： A61M1/0058 ,  Y10T292/20 ,  Y10T292/225

    摘要： A mechanism having a pair of pivoting cassette clamping bars. The clamping bars are connected to a pneumatic cylinder or an electromechanical actuator through a series of links and an actuator wheel so that extension and retraction of the pneumatic cylinder or the electromechanical actuator causes the clamping bars to rotate and counter-rotate. The use of a pneumatic cylinder provides smooth, well-controlled movement of the clamping bars.

    摘要翻译： 具有一对枢转盒式夹紧杆的机构。 夹紧杆通过一系列连杆和致动器轮连接到气动缸或机电致动器，使得气动缸或机电致动器的伸出和缩回导致夹紧杆旋转并反向旋转。 气动缸的使用提供了夹紧杆的平稳，良好控制的运动。

    Systems and methods for power generation with carbon dioxide isolation
    6.
    发明申请
    Systems and methods for power generation with carbon dioxide isolation 有权
    用二氧化碳隔离发电的系统和方法

    公开(公告)号：US20070006592A1

    公开(公告)日：2007-01-11

    申请号：US11178165

    申请日：2005-07-08

    申请人： Chellappa Balan ,  Michael Bowman ,  Joell Hibshman ,  Andrei Evulet ,  Jennifer Molaison

    发明人： Chellappa Balan ,  Michael Bowman ,  Joell Hibshman ,  Andrei Evulet ,  Jennifer Molaison

    IPC分类号： F02C6/18

    CPC分类号： F02C9/40 ,  F02C3/22 ,  F02C3/34 ,  Y02E20/16

    摘要： A power generation system and method includes a first gas turbine system comprising a first combustion chamber configured to combust a first fuel stream of primarily hydrogen that is substantially free of carbon-based fuels. The first gas turbine system also includes a first compressor configured to supply a first portion of compressed oxidant to the first combustion chamber and a first turbine configured to receive a first discharge from the first combustion chamber and generate a first exhaust and electrical energy. The power generation system further includes a second gas turbine system comprising a second combustion chamber configured to combust a second fuel stream to generate a second discharge. The first compressor of the first gas turbine system is configured to supply a second portion of compressed oxidant to the second combustion chamber. The second turbine system also includes a second turbine configured to receive the second discharge from the second combustion chamber to generate a second exhaust and electrical energy and a second compressor configured to receive the second discharge comprising carbon dioxide. The second compressor is also configured to discharge a recycle stream to the second combustion chamber and a split stream to a separator system adapted to recover carbon dioxide.

    摘要翻译： 发电系统和方法包括第一燃气轮机系统，其包括构造成燃烧基本上不含碳基燃料的主要为氢的第一燃料流的第一燃烧室。 第一燃气轮机系统还包括配置成将第一部分压缩氧化剂供应到第一燃烧室的第一压缩机和被配置为接收来自第一燃烧室的第一次排放并产生第一排气和电能的第一涡轮机。 发电系统还包括第二燃气轮机系统，其包括被配置为燃烧第二燃料流以产生第二排放的第二燃烧室。 第一燃气轮机系统的第一压缩机构造成将第二部分的压缩氧化剂供应到第二燃烧室。 第二涡轮机系统还包括构造成从第二燃烧室接收第二排出物以产生第二排气和电能的第二涡轮机，以及配置成接收包括二氧化碳的第二排放物的第二压缩机。 第二压缩机还构造成将再循环流排放到第二燃烧室，并将分流流分配到适于回收二氧化碳的分离器系统。

    METHOD AND APPARATUS FOR REDUCING GAS TURBINE ENGINE EMISSIONS
    9.
    发明申请
    METHOD AND APPARATUS FOR REDUCING GAS TURBINE ENGINE EMISSIONS 审中-公开
    减少气体涡轮发动机排放的方法和装置

    公开(公告)号：US20080016876A1

    公开(公告)日：2008-01-24

    申请号：US11773015

    申请日：2007-07-03

    申请人： Andrei Colibaba-Evulet ,  Michael Bowman ,  Simon Sanderson ,  Anthony Dean

    发明人： Andrei Colibaba-Evulet ,  Michael Bowman ,  Simon Sanderson ,  Anthony Dean

    IPC分类号： F02C1/00

    CPC分类号： F02C9/40 ,  F05D2220/75 ,  F05D2250/82 ,  F05D2260/96 ,  F05D2270/082 ,  F23C2900/03001 ,  F23R3/14 ,  F23R3/286 ,  F23R3/44 ,  F23R2900/00002 ,  Y02T50/675 ,  Y02T50/677 ,  Y02T50/678

    摘要： A low emission turbine includes a reverse flow can-type combustor that generally includes a primary and secondary fuel delivery system that can be independently controlled to produce low CO, UHC, and NOx emissions at design set point and at conditions other than design set point. The reverse flow can-type combustor generally includes an annularly arranged array of swirler and mixer assemblies within the combustor, wherein each swirler and mixer in the array includes a primary and secondary fuel delivery system that can be independently controlled. Also disclosed herein is a can-type combustor that includes fluid passageways that perpendicularly impinge the backside of a heat shield. Processes for operating the can-type combustors are also disclosed.

    摘要翻译： 低排放涡轮机包括逆流罐式燃烧器，其通常包括主燃料输送系统和辅助燃料输送系统，其可独立控制以在设计设定点和设计设定点以外的条件下产生低CO，UHC和NOx排放。 反向流动罐式燃烧器通常包括在燃烧器内的环形排列的旋流器和混合器组件，其中阵列中的每个旋流器和混合器包括可以独立控制的主要和次要燃料输送系统。 本文还公开了一种罐型燃烧器，其包括垂直地撞击隔热罩背面的流体通道。 还公开了用于操作罐式燃烧器的方法。