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Bottle - Antofagasta having improved cooling other structures - Others - Binro

机译:瓶子-具有改善其他结构冷却效果的Antofagasta-其他-Binro

摘要

By easy pre-rotation of the nozzle [Abstract] Disclosed is manufactured to provide a gas turbine to increase the cooling effect of the turbine rotor by reducing the pressure loss of the cooling air. The apparatus includes a compressor 2 for compressing air, a turbine to extract a combustor 3 to be combusted by mixing the fuel F to the compressed air A from the compressor 2, the power from the combustion gas G from the combustor 3 The gas turbine 1 with a 4 I constructed as follows. The pre-rotation nozzle 37 at rest is provided, for the pre-rotation of the nozzle 37 of the turbine 4 rotor 13A, and supplies the cooling air CA to pivot in the direction of rotation of the rotor 13A. In the pre-rotation nozzle 37, the cooling air C Toward the entrance of the A to the outlet to form a conical nozzle holes 39 passage width is narrowed, thereby to make the pressure loss of the cooling air CA at the inlet of the nozzle hole 39 is reduced, and the cooling air CA with respect to the rotor 13A the relative total temperature T rel I be low.
机译:通过喷嘴的容易的预旋转[摘要]制造一种燃气涡轮机,以通过减少冷却空气的压力损失来提高涡轮机转子的冷却效果。该设备包括:用于压缩空气的压缩机2;涡轮机,其通过将来自压缩机2的燃料F与压缩空气A混合而抽出待燃烧的燃烧器3;来自燃烧器3的燃烧气体G的动力。燃气轮机1用4我构造如下。静止的预旋转喷嘴37被设置用于涡轮4转子13A的喷嘴37的预旋转,并且供给冷却空气CA以在转子13A的旋转方向上枢转。在预旋转喷嘴37中,冷却空气C朝着A的入口进入出口以形成锥形喷嘴孔39,通道宽度变窄,从而使冷却空气CA在喷嘴入口处的压力损失孔39减小,并且相对于转子13A的冷却空气CA的相对总温度T rel I低。

著录项

  • 公开/公告号JP3034519B1

    专利类型

  • 公开/公告日2000-04-17

    原文格式PDF

  • 申请/专利权人 川崎重工業株式会社;

    申请/专利号JP19990107417

  • 发明设计人 杉本 隆雄;

    申请日1999-04-15

  • 分类号F01D5/18;F01D5/08;F02C7/18;

  • 国家 JP

  • 入库时间 2022-08-22 02:04:24

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