Exhaust gas turbocharger for an internal combustion engine
View Patent ↗In an exhaust gas turbocharger for an internal combustion engine including an exhaust gas turbine in the exhaust line and a compressor in the intake tract of the internal combustion engine, and the exhaust gas turbine includes a gas inlet passage with a variable guide vane structure supported on one side of a support ring arranged in the inlet flow passage to the turbine wheel, the support ring is mounted in a floating manner such that the side thereof, which faces away form the guide vanes is exposed to the gas pressure in the inlet flow passage in order to bias the support ring toward the opposite inlet flow passage wall and spacer sleeves with expansion properties similar to those of the guide vanes are provided between the support ring and the opposite flow passage wall for delimiting the clearance between the guide vanes and the opposite flow passage wall.
1. An exhaust gas turbocharger for an internal combustion engine, including:
an air intake tract ( 6 ),
an exhaust gas line ( 4 ),
a compressor ( 5 ) disposed in the air intake tract ( 6 ) of the internal combustion engine ( 1 ),
an exhaust gas turbine ( 3 ) having a turbine housing ( 14 ) with a turbine wheel ( 12 ) and being disposed in the exhaust gas line ( 4 ), the exhaust gas turbine ( 3 ) having an inflow duct ( 13 ) arranged upstream of the turbine wheel ( 12 ) in the turbine housing ( 14 ) of the exhaust gas turbine ( 3 ),
a variable turbine guide vane structure ( 11 ) arranged in an inlet flow passage ( 16 ) of the inflow duct ( 13 ) to the turbine wheel ( 12 ), said variable turbine guide vane structure ( 11 ) comprising a support ring ( 18 ) with guide vanes ( 19 ) supported on one side of the support ring ( 18 ) and the support ring ( 18 ) being mounted in a floating manner in a wall section ( 21 ) of the turbine housing ( 14 ), and
spacer sleeves ( 24 ) arranged in the inlet flow passage ( 16 ), so as to define an end-side operating gap of the guide vanes ( 19 ) having a predetermined size between 0.02 and 0.1 mm as measured in the cold state, the spacer sleeves ( 24 ) consisting of a material having expansion properties which match expansion properties of the guide vanes ( 19 ) during temperature changes in the inlet flow passage ( 16 ) in order to maintain the end side operating gap of the guide vanes ( 19 ) with changing temperatures at the predetermined size.
2. The exhaust gas turbocharger as claimed in claim 1 , wherein the spacer sleeve ( 24 ) has an opening in its side facing away from the support ring ( 18 ).
3. The exhaust gas turbocharger as claimed in claim 2 , wherein the spacer sleeve ( 24 ) is connected to the support ring ( 18 ) by a detachable connection.
4. The exhaust gas turbocharger as claimed in claim 3 , wherein the detachable connection is a screw connection.
5. The exhaust gas turbocharger as claimed in claim 1 , wherein the spacer sleeve ( 24 ) is formed in one piece with the support ring ( 18 ).
6. The exhaust gas turbocharger as claimed in claim 1 , wherein the spacer sleeve ( 24 ) is disposed on a shaft ( 26 ), with the shaft ( 26 ) being supported by the support ring ( 18 ).
7. The exhaust gas turbocharger as claimed in claim 6 , wherein the shaft ( 26 ) is formed separately from the spacer sleeve ( 24 ).