Patent ID: 7097415

Claim:
A low-pressure turbine of a turbomachine, said turbomachine comprising a high-pressure turbine disposed upstream from the low-pressure turbine in the flow direction of gas passing therethrough, and an exhaust casing disposed downstream from the low-pressure turbine in the flow direction of said gas, said low-pressure turbine comprising a rotor fastened on a low-pressure trunnion, and a rotary low-pressure shaft, said low-pressure turbine further comprising a first rolling bearing disposed on said low-pressure shaft and supporting a high-pressure trunnion on which there is fastened a rotor of the high-pressure turbine, a second rolling bearing disposed on said low-pressure trunnion downstream from said first rolling bearing and enabling said low-pressure trunnion to be centered relative to said exhaust casing, and a system of fluting enabling said low-pressure trunnion to drive said low-pressure shaft, said system of fluting being disposed between said first and second rolling bearings.