SYSTEM AND METHOD FOR INSTALLATION OR REMOVAL OF ONE OR MORE COMBUSTION CANS

    公开(公告)号:US20230018703A1

    公开(公告)日:2023-01-19

    申请号:US17379052

    申请日:2021-07-19

    IPC分类号: F02C3/14

    摘要: A system includes an annular track that surrounds the turbomachine. The annular track includes an upper rail portion and a lower rail portion removably coupled to one another. The system further includes a drive assembly operably coupled to the annular track. The drive assembly includes a drive chain that extends along the annular track. The system further includes a plurality of carts rotatably coupled to the annular track and connected to the drive chain such that operation of the drive assembly alters a circumferential position of the plurality of carts with respect to an axial centerline of the turbomachine. The system further includes a plurality of combustion can cradle assemblies each coupled to a respective cart of the plurality of carts. Each combustion can cradle assembly of the plurality of combustion can cradle assemblies is configured to removably couple to a combustion can of the one or more combustion cans.

    System and method for installation or removal of one or more combustion cans

    公开(公告)号:US11773772B2

    公开(公告)日:2023-10-03

    申请号:US17379052

    申请日:2021-07-19

    IPC分类号: F02C3/14

    摘要: A system includes an annular track that surrounds the turbomachine. The annular track includes an upper rail portion and a lower rail portion removably coupled to one another. The system further includes a drive assembly operably coupled to the annular track. The drive assembly includes a drive chain that extends along the annular track. The system further includes a plurality of carts rotatably coupled to the annular track and connected to the drive chain such that operation of the drive assembly alters a circumferential position of the plurality of carts with respect to an axial centerline of the turbomachine. The system further includes a plurality of combustion can cradle assemblies each coupled to a respective cart of the plurality of carts. Each combustion can cradle assembly of the plurality of combustion can cradle assemblies is configured to removably couple to a combustion can of the one or more combustion cans.

    AIR SUPPLY AND CONDITIONING SYSTEM FOR A GAS TURBINE
    5.
    发明申请
    AIR SUPPLY AND CONDITIONING SYSTEM FOR A GAS TURBINE 有权
    用于气体涡轮机的空气供应和调节系统

    公开(公告)号:US20170002739A1

    公开(公告)日:2017-01-05

    申请号:US14755406

    申请日:2015-06-30

    IPC分类号: F02C7/141 F02C7/052

    摘要: An air supply and conditioning system for an inlet system of a gas turbine includes an air processing unit having an inlet configured to receive compressed air from a compressor of the gas turbine. The air processing unit includes a heat exchanger that is downstream from the inlet. A vortex cooler is disposed downstream from the inlet of the air processing unit. The vortex cooler is in fluid communication with the heat exchanger and with an outlet of the air processing unit. The system further includes a self-cleaning filter that is disposed within a duct of the inlet system. The self-cleaning filter is in fluid communication with at least one of the outlet of the air processing unit or an outlet of the vortex cooler.

    摘要翻译: 用于燃气轮机的入口系统的空气供应和调节系统包括空气处理单元,其具有被配置为从燃气轮机的压缩机接收压缩空气的入口。 空气处理单元包括在入口下游的热交换器。 涡流冷却器设置在空气处理单元的入口的下游。 涡流冷却器与热交换器和空气处理单元的出口流体连通。 该系统还包括设置在入口系统的管道内的自清洁过滤器。 自清洁过滤器与空气处理单元的出口或涡流冷却器的出口中的至少一个流体连通。