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Turbo-compressor with single cantilever rotor - has centrifugal compressor and axial flow turbine between which is seal with dia. chosen to equalise pressures

机译:具有单悬臂转子的涡轮压缩机-具有离心压缩机和轴流式涡轮机,两者之间通过直径密封。选择均衡压力

摘要

A turbo-compressor has a single cantilever rotor mounted on a shaft(1) which runs in bearings(4, 5). The single rotor incorporates a centrifugal compressor(2) and an axial flow turbine (3). The gas flowing to the turbine(3) passes between fixed blades(7) which impart an initial switch to the gas. This combination rotor simplifies the designa dn provides earlier access to the barings. In addition the seal diameter(10) between the compressor and turbine flow paths is so chosen that the pressures are the same on both sides so that there is no leakage.
机译:涡轮压缩机具有安装在轴(1)上的单个悬臂转子,该轴在轴承(4,5)中运行。单转子装有离心压缩机(2)和轴流式涡轮机(3)。流入涡轮机(3)的气体在固定叶片(7)之间通过,从而对气体进行初始切换。这种组合式转子简化了设计,从而可以更早地进入裸机。另外,选择压缩机和涡轮机流动路径之间的密封直径(10),以使两侧的压力相同,从而不会泄漏。

著录项

  • 公开/公告号FR2411300A1

    专利类型

  • 公开/公告日1979-07-06

    原文格式PDF

  • 申请/专利权人 ELECTRO MECANIQUE CIE;

    申请/专利号FR19770036807

  • 发明设计人 JEAN CHABOSEAU;

    申请日1977-12-07

  • 分类号F01D15/08;F01D1/04;F04D25/04;

  • 国家 FR

  • 入库时间 2022-08-22 19:31:54

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