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Surge avoidance control method and surge avoidance control device for exhaust turbine turbocharger

机译:排气涡轮增压器的避雷控制方法及避雷控制装置

摘要

A surge avoidance control method that includes a surge detection step of determining whether the operation point of the compressor is positioned in a surge operation region at each predetermined timing; a surge avoidance opening-degree calculation step calculating a surge avoidance opening degree of the operation device necessary for moving the operation point of the compressor determined to be positioned in the surge operation region in the surge detection step out of the surge operation region; a correction opening-degree calculation step calculating a correction opening degree of the operation device on the basis of a moving velocity of the operation point of the compressor which is determined to be positioned in the surge operation region in the surge detection step; and an opening-degree command value calculation step calculating an opening-degree command value of the operation device on the basis of the surge avoidance opening degree and the correction opening degree.
机译:一种喘振避免控制方法,包括:喘振检测步骤,其在每个预定时刻确定压缩机的工作点是否位于喘振操作区域中;以及防喘振开度计算步骤计算出将在喘振检测步骤中被确定为位于喘振操作区域中的压缩机的操作点移出喘振操作区域所需的操作装置的喘振避免开度;校正开度计算步骤基于在喘振检测步骤中被确定为位于喘振操作区域中的压缩机的操作点的移动速度来计算操作装置的校正开度;开度指令值计算步骤基于避雷器开度和校正开度来计算操作装置的开度指令值。

著录项

  • 公开/公告号US10677149B2

    专利类型

  • 公开/公告日2020-06-09

    原文格式PDF

  • 申请/专利号US201615781864

  • 发明设计人 RYO SASE;NAOKI YAHATA;

    申请日2016-03-08

  • 分类号F02B37/16;F02B37/18;F02B37/24;F02B37/12;F02B39/16;F02D41;F02B37/22;F04D27;F04D27/02;

  • 国家 US

  • 入库时间 2022-08-21 11:27:01

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