发明名称 SHAFT SEAL ASSEMBLY, ESPECIALLY FOR HIGH-PRESSURE TURBOCOMPRESSORS
摘要 A turbocompressor shaft seal, especially for a high-pressure turbocompressor, has each of its gas-side and atmosphere-side slide rings biased toward a rotor ring of the shaft and associated with blocking-liquid compartments which are interconnected by an annular passage around the rotor ring. The compartments are connected in a closed circulation path with a circulating pump and a cooler and leakage liquid is returned by a feed pump to the liquid circulation with the aid of a pressure transformer biased on one side by the gas pressure to be sealed and an adjustable spring force and, on the other side, by the pressure of the blocking liquid.
申请公布号 US5158431(A) 申请公布日期 1992.10.27
申请号 US19910659107 申请日期 1991.02.21
申请人 MANNESMANN A.G.;PACIFIC WIETZ GMBH & CO. K.G. 发明人 SCHELLONG, HELMUT;VICTOR, KARL-HEINZ;LAARMANN, HANS-WILHELM;MASER, GUSTAV;DEDEKEN, RALF
分类号 F16J15/40 主分类号 F16J15/40
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