Method of intermediate cooling of compressed gases
AssigneeM.A.N. Uternehmensbereich G.H.H. Sterkrade
InventorWilfried Blotenberg
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Abstract
An improved method of cooling compressed gases intermediate successive compressive stages in a multi-stage intercooled compressor system without forming condensate is provided. Cooling water flow to an intercooler intermediate successive compressive stages is regulated as a function of the actual temperature of the gas downstream of the intercooler and a set point temperature generated as a function of a linear approximation relating the inlet dew point temperature and the pressure of the gases downstream of the intercooler.
Claims1
In a multi-stage intercooled compressor system having a plurality of compression stages connected in series with a cooling unit controlled by adjustment means between each stage, an improved method of cooling compressed gases intermediate the stages without forming condensate comprising:
- measuring the absolute humidity of the gases to be compressed at the suction side of a first compression stage which corresponds to a dew point .tau. of the gases at the suction side of the first compression stage;
- measuring the temperature and pressure of the compressed gases at the suction side of a successive compression stage designated i;
- generating a set point temperature signal on the basis of the linear equation
- T.sub.i =a.sub.i .multidot..tau..sub.a +b.sub.i .multidot.P.sub.i +c.sub.i
- where P.sub.i is the pressure of the compressed gases at the suction side of the successive compression stage designated i, and a.sub.i, b.sub.1 and C.sub.i are constants;
- generating a control signal for controlling the cooling of the gases upstream of the compression stage designated i as a function of the set point temperature signal and the actual temperature of the compressed gases at the suction side of the compression stage designated i;
- and
- using the control signal to control the adjustment signal to control the adjustment means of the cooling unit which is upstream of the compression stage designated i.
Dependencies are inferred from the claim text.