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Gas turbine driven high speed centrifugal compressor unit

机译:燃气轮机驱动的高速离心压缩机组

摘要

A high speed centrifugal compressor is closely directly coupled to the power turbine of a two-shaft gas turbine having a gas generator section separate from its power turbine. Through the direct close coupling and centerline mounting of the gas turbine exhaust casing for free and uniform heat expansion, alignment between stationary and rotating parts of the power turbine and compressor is maintained free from mechanical problems. The compressor stage assembly elements are conveniently interfitted together in the vertically split compressor casing by means of compression bolts minimizing fastening means. Bearings and oil seals are fed by an integrated lubrication and sealing oil system utilizing a compact oil distribution manifold assembly incorporating a quick filter change structure. The turbine fuel distribution system includes means permitting ready replacement and maintenance of individual fuel nozzles without disassembly of the entire fuel nozzle system. The gas turbine-compressor finds particularly useful application in areas where high power, compact, relatively maintenance-free units are required, as, for example, on offshore platforms in the natural gas industry.
机译:高速离心压缩机紧密地直接联接到两轴燃气轮机的动力涡轮,该双轴燃气轮机具有与其动力涡轮分开的气体发生器部分。通过燃气轮机排气箱的直接紧密联接和中心线安装以实现自由和均匀的热膨胀,可保持动力涡轮机和压缩机的固定部分和旋转部分之间的对准,而不会出现机械问题。借助于最小化紧固装置的压缩螺栓,压缩机级组装元件可方便地相互组装在垂直分开的压缩机壳体中。轴承和油封由集成的润滑和密封油系统供油,该系统利用紧凑的机油分配歧管组件结合了快速更换滤芯的结构。涡轮机燃料分配系统包括允许在不拆卸整个燃料喷嘴系统的情况下容易地更换和维护各个燃料喷嘴的装置。燃气轮机压缩机在需要大功率,紧凑,相对免维护的装置的领域中找到了特别有用的应用,例如在天然气工业中的海上平台上。

著录项

  • 公开/公告号FR2269650B1

    专利类型

  • 公开/公告日1980-09-12

    原文格式PDF

  • 申请/专利权人 NORWALK TURBO INC;

    申请/专利号FR19750013675

  • 发明设计人

    申请日1975-04-30

  • 分类号F04D17/08;F04D25/02;

  • 国家 FR

  • 入库时间 2022-08-22 17:26:38

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