首页> 外国专利> METHOD OF MEASURING DISTANCE BETWEEN WORKING POINT OF TURBO-COMPRESSOR AND ITS SURGING BOUNDARY (VERSIONS) AND DEVICE FOR DETERMINATION OF POSITION OF WORKING POINT OF TURBO-COMPRESSOR RELATIVE TO ITS SURGING BOUNDARY (VERSIONS)

METHOD OF MEASURING DISTANCE BETWEEN WORKING POINT OF TURBO-COMPRESSOR AND ITS SURGING BOUNDARY (VERSIONS) AND DEVICE FOR DETERMINATION OF POSITION OF WORKING POINT OF TURBO-COMPRESSOR RELATIVE TO ITS SURGING BOUNDARY (VERSIONS)

机译:涡轮压缩机工作点与工作边界(版本)之间距离的测量方法以及相对于其工作边界(版本)的涡轮压缩机工作点位置的确定装置

摘要

FIELD: measurement of distance between working point and surging boundary of turbo-compressor. SUBSTANCE: surging boundary is determined as function of corrected power Pr/Ks; magnitude characterizing working point of turbo-compressor is calculated as function of corrected power Pr/Ks. Set point calculation units include units for calculation of set point relative to surging boundary of turbo-compressor as function of corrected power Pr/Ks and units for calculation of magnitude characterizing working point of turbo-compressor includes units for calculation of this magnitude as function of corrected power Pr/Ks. Invention contains description of this method and device. EFFECT: reliable protection of turbo-compressor against surging and flow break- away due to use of various coordinate systems invariant relative to suction conditions with minor amount of sensors. 30 cl, 39 dwg
机译:领域:测量工作点到涡轮压缩机喘振边界之间的距离。实质:浪涌边界确定为校正功率Pr / Ks的函数;根据校正功率Pr / Ks计算出涡轮压缩机工作点的最大幅度。设定点计算单元包括用于计算相对于涡轮压缩机的喘振边界的设定点作为校正功率Pr / Ks的函数的单元,以及用于计算表征涡轮压缩机的工作点的幅值的单元包括用于计算该幅值的单元作为修正函数Pr / Ks的函数校正后的功率Pr / Ks。发明包含对该方法和设备的描述。效果:由于使用了数量少的传感器,由于使用了相对于吸气条件不变的各种坐标系,因此涡轮压缩机的可靠保护免受浪涌和流量中断。 30厘升,39载重吨

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