Axially thrust-compensated turbo machine
AssigneeSulzer-Escher Wyss GmbH
InventorHeinrich Lorenzen
Life of this patent
Estimating the term…
Abstract
In a turbo machine with magnetic bearings on both sides and dry gas seals for the rotor, the axial thrust acting upon the rotor and generated by the pressure difference between the pressure side and the suction side is compensated for in that a dry gas seal provided on the suction side and the end of the shaft are acted upon by a certain pressure, which generates a compensating axial thrust, so that the resultant axial thrust becomes as slight as possible. Advantageously, this pressure is regulated via the bearing gap of an axial magnetic bearing of the rotor such that the bearing gas assumes a predetermined value.
Claims10
A turbo machine comprising:
- a rotor comprising a shaft having a suction side and a pressure side;
- a housing extending around said rotor along at least a portion of the length of said rotor;
- first and second magnetic bearings mounted at said housing and supporting opposite respective axial portions of said shaft, said first and second magnetic bearings having respective bearing chambers with interiors;
- a third magnetic bearing mounted at said housing, adjacent said first magnetic bearing, between said first and second magnetic bearings, for supporting said shaft against axial force;
- seals for sealing said shaft from the interiors of said bearing chambers of said housing at said suction side and at said pressure side, comprising an arrangement for absorbing an initially produced axial force generated by a pressure difference between the suction side and the pressure side acting upon said rotor;
- said seals comprise first and second dry gas seals, which act outwardly, each against said respective suction side and pressure side bearing chambers of said first and second magnetic bearings, respectively;
- a further dry gas seal provided on an end of said shaft at said suction side of said housing and acting inversely relative to said first dry gas seal, wherein said further dry gas seal and at least a portion of said end of said shaft are acted upon by a seal gas pressure such that over an impingement face of said shaft end, a compensating axial force is generated which at least substantially compensates for said initially produced axial force generated by the pressure difference between the suction side and the pressure side acting upon said rotor.
A turbo machine comprising:
- a rotor comprising a shaft;
- a housing extending around said rotor along at least a portion of the length of said rotor, said housing having an interior, a suction side and a pressure side;
- bearings mounted at said housing and supporting opposite axial portions of said shaft;
- first and second seals for sealing said shaft from the interior of said housing at said suction side and at said pressure side, respectively, said seals acting outwardly, each against said respective suction side and pressure side, said seals comprising an arrangement for absorbing an initially produced axial force acting upon said rotor generated by a pressure differential among axial forces acting on said shaft;
- an additional seal provided on said shaft, between said first and second seals and acting conversely to that of said first seal, wherein a force acts upon said additional seal so that a compensating axial force is generated which at least substantially compensates for said initially produced axial force.
Dependencies are inferred from the claim text.