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Process for preventing rotating stall and surge in a turbomachine

机译:防止涡轮机旋转失速和喘振的方法

摘要

The present application provides a process for preventing rotating stall and surge in a turbomachine compressor. The compressor may include air extraction pipes connecting the compressor to a turbomachine exhaust area or to the atmosphere, at least one of the pipes is fitted with a flow regulation valve, and each valve has an adjustable degree of opening. The process includes, for at least one of the valves, a complete opening command when the compressor rotation speed is less than a predetermined threshold value beyond which there is no longer any risk of rotating stall and surge and a command for lowering the degree of opening of the valve when the rotation speed of the compressor exceeds the threshold value.
机译:本申请提供了一种用于防止涡轮机压缩机中的旋转失速和喘振的方法。压缩机可以包括将压缩机连接到涡轮机排气区域或大气的抽气管,至少其中一根管装有流量调节阀,并且每个阀的开度都可调。该过程包括:对于至少一个阀,当压缩机转速小于预定阈值时完全打开命令,超过该阈值不再存在旋转失速和喘振的风险,以及降低开度的命令当压缩机的旋转速度超过阈值时,阀门的最大角度。

著录项

  • 公开/公告号US9759134B2

    专利类型

  • 公开/公告日2017-09-12

    原文格式PDF

  • 申请/专利权人 GE ENERGY PRODUCTS FRANCE SNC;

    申请/专利号US201414515639

  • 发明设计人 LAURENT BALCER;

    申请日2014-10-16

  • 分类号F04D27/02;F02C9/18;F01D21/14;

  • 国家 US

  • 入库时间 2022-08-21 13:48:49

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