A gas turbine arrangement

Details A gas turbine arrangement A gas turbine arrangement

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 3/04 (2006.01) F01D 25/12 (2006.01)

Patent

CA 2333269

A gas turbine arrangement which comprises a compressor (2) with a rotor (7), a turbine (3), with a rotor (12) and connected with the compressor (2), and a balancing member (18) connected with the turbine rotor (12), arranged to counteract the axial forces generated by the compressor rotor (7) and the turbine rotor (12), wherein the balancing member (18) is arranged to be activated by means of a pressure fluid. The gas turbine arrangement (1) comprises at least one channel (26) which is arranged to lead at least a part of the pressure fluid used for said activation to at least a part of the turbine (3) for influencing the temperature of the same.

L'invention concerne une conception d'une turbine à gaz comprenant un compresseur (2) doté d'un rotor (7), une turbine (3) dotée d'un rotor (12) et raccordée au compresseur (2), et un élément d'équilibrage (18) relié au rotor de turbine (12), conçu pour contrecarrer les forces axiales générées par le rotor de compresseur (7) et le rotor de turbine (12). L'élément d'équilibrage (18) est conçu pour être activé à l'aide d'un fluide de pression. Cette turbine à gaz (1) comprend au moins un canal (26) qui est conçu pour acheminer au moins une partie du fluide de pression utilisé pour cette activation jusqu'à au moins une partie de la turbine (3) afin d'agir sur sa température.

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