Method of monitoring a pumping limit of a multistage turbocompressor with intermediate cooling
AssigneeAtlas Copco Energas GmbH
InventorsIoan Ispas, Ulrich Grundmann, Yvan Van Hoof
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AssigneeAtlas Copco Energas GmbH
InventorsIoan Ispas, Ulrich Grundmann, Yvan Van Hoof
Estimating the term…
A method of operating a multistage turbocompressor or of monitoring the pump limit thereof, whereby the pump limit function is stored in the control unit in the form Y=m.F+b and the coefficients m and b are determined by the linear relationships m=m.sub.0 +m.sub.1.dT.sub.s +.SIGMA.m.sub.2i.dT.sub.ri b=b.sub.0 +b.sub.1.dT.sub.s +.SIGMA.b.sub.2i.dT.sub.ri where T.sub.s and T.sub.ri represent the intake temperature and the backcooling temperatures following coolers after each turbocompressor and dT.sub.s and T.sub.ri and reference temperatures T.sub.ref. The system automatically compensates for the shift of the pump limit with temperature and allows operation closer to the pump limit or boundary for stable aerodynamic operation.
A method of operating a multistage turbocompressor system in which at an intake temperature T.sub.s and pressure p.sub.1 a gas is drawn into a first turbocompressor, gas compressed in the first turbocompressor is subject to intermediate cooling, cooled gas is compressed in subsequent turbocompressors in cascade with subsequent cooling to temperatures T.sub.ri where i is a number which represents the number of the cooling stage in succession at which said cooling occurs, and the gas after a last turbocompressor and cooling stage of the cascade has a discharge pressure p.sub.2 for a volume rate of flow F through the cascade, said method comprising the steps of:
Dependencies are inferred from the claim text.