首页> 外国专利> ACTION TURBINE STAGE WITH REDUCED SECONDARY LOSSES.

ACTION TURBINE STAGE WITH REDUCED SECONDARY LOSSES.

机译:涡轮机级具有减少的二次损失。

摘要

Impulse turbine stage comprising a bank (1) of fixed blades (2) integral with the stator (3) of the turbine supporting a diaphragm (4) followed by a bank (7) of moving blades (8) mounted on a disc (9) integral with the rotor (6) of the turbine, characterised in that the said disc (9) is provided with transverse ducts (2) parallel to the axis of the rotor (6) and in that the inlets of the said ducts (12) opening into the space between the diaphragm (4) and the disc (9) are provided with scoops (15) oriented to send the fluid towards the inside of the ducts (12). …??The invention allows a reduction of the secondary losses of an impulse turbine. …IMAGE…
机译:脉冲式涡轮机级,包括与涡轮的定子(3)集成在一起的固定叶片(2)的排(1),支撑叶片(4),随后是安装在圆盘(9)上的动叶片(8)的排(7) )与涡轮的转子(6)成一整体),其特征在于,所述盘(9)设置有平行于转子(6)的轴线的横向管道(2),并且所述管道(12)的入口开口到隔膜(4)和圆盘(9)之间的空间设有勺(15),该勺(15)定向成将流体朝着导管(12)的内部输送。本发明可以减少脉冲涡轮的二次损失。 …<图像>…

著录项

  • 公开/公告号FR2661946B1

    专利类型

  • 公开/公告日1994-06-10

    原文格式PDF

  • 申请/专利权人 GEC ALSTHOM SA;

    申请/专利号FR19900005992

  • 发明设计人 DETANNE FRANCOIS;

    申请日1990-05-14

  • 分类号F01D11/00;F01D1/04;

  • 国家 FR

  • 入库时间 2022-08-22 04:34:01

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