Patent ID: 6925805

Claim:
An exhaust gas turbocharger for an internal combustion engine, comprising at least one turbine adapted for receiving exhaust gas flow from the internal combustion engine, wherein the turbine ( 2 ) comprises: a flow channel ( 13 ) with at least one radial in-flow cross-section ( 13 a ) between opposite sides, a nozzle ring ( 7 ) bordering the radial in-flow cross-section ( 13 a ), a guide vane assembly ( 5 ) which is variably adjustable for adjusting the radial flow-through cross-section ( 13 a ), and a compensation ring ( 20 ) mounted to the nozzle ring and displaceable axially from the nozzle ring towards the guide vane ( 5 ), wherein the guide vane assembly is mounted on one side of the flow channel ( 13 ) and the compensation ring ( 20 ) is mounted on the opposite side of the flow channel ( 13 ).