Turbo machine and method for the operation thereof
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[0013]FIG. 1 shows a schematic representation of the turbomachine TM or method according to embodiments of the invention as a flow diagram. The turbomachine TM in the exemplary embodiment is designed as a turbocompressor CO with a rotor R which extends along an axis X. Along the axis X, the turbocompressor CO has a high-pressure position HPS and a low-pressure position LPS at which, during operation, a process fluid PF in the flow path of the turbomachine TM is, respectively, at a higher or a lower pressure. A gap GP (not shown in more detail) between the stator CAS and the rotor R of the turbomachine TM is sealed on both sides of the turbomachine by means of gas seals DGS. The turbomachine TM, or the stator CAS which is formed as a casing, has an inlet INL and an outlet OTL, wherein a process fluid PF enters the turbomachine for compression through the inlet INL and is conveyed to the outlet OTL where it leaves the turbomachine at a higher pressure. An extraction point EX for the p...
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