Mounting of the rotor of a gas turbine

Details Mounting of the rotor of a gas turbine Mounting of the rotor of a gas turbine

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 25/16 (2006.01) F01D 3/00 (2006.01) F02C 7/06 (2006.01) F16C 35/02 (2006.01)

Patent

CA 2489655

The rotor (5) of a gas turbine containing a compressor part (1) and a turbine part (3) is mounted in an axial thrust bearing (19) and in two radial journal bearings (16, 17). One of the bearings is a journal bearing (16) arranged in the intake area of the compressor part (1) and the other journal bearing (17) together with the thrust bearing (19) is arranged in the area of the turbine part (3).

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