Turbocharger comprising a floating bush bearing
A turbocharger has an exhaust gas turbine, a fresh-air compressor and a bearing seat. A rotor shaft that is equipped with the turbine and the compressor wheel is rotatably mounted in the bearing seat by way of at least one radial bearing. The radial bearing is a floating bush bearing with a hollow-cylindrical floating bush body positioned between a bearing seat of the bearing housing and the rotor shaft. The floating bush body is provided with a defined imbalance in order to counteract an imbalance of the turbo rotor.
1. An exhaust-gas turbocharger, comprising:
a common rotor shaft, an exhaust-gas turbine with a turbine wheel mounted on said rotor shaft, and a fresh-air compressor with a compressor wheel mounted on said rotor shaft;
said rotor shaft with said turbine wheel and said compressor wheel together forming a turbo rotor;
at least one radial bearing rotatably mounting said rotor shaft in a bearing housing;
said at least one radial bearing being a floating-bushing bearing having a floating bushing body formed as a hollow cylinder with an inner diameter for receiving said rotor shaft and with an outer diameter by which said floating bushing body is received in a bearing receptacle, wherein an inner lubrication gap is formed between said rotor shaft and said inner diameter of said floating bushing body and an outer lubrication gap is formed between a bearing receptacle and said outer diameter; and
said floating bushing body being formed with a defined imbalance with respect to an axis of rotation, said imbalance counteracting, in a stabilizing fashion, an imbalance of said turbo rotor during operation;
wherein said defined imbalance of said floating bushing body is at least partially formed by an eccentricity indicating a deviation between a position of an axis of inertia of said floating bushing body in relation to an axis of rotation of said floating bushing body, said eccentricity amounting to between 0.003 mm and 0.008 mm.
2. The exhaust-gas turbocharger according to claim 1 , wherein said eccentricity amounts to substantially 0.005 mm.
3. The exhaust-gas turbocharger according to claim 1 , wherein said defined imbalance of said floating bushing body is partially formed by at least one stepped bore formed into said floating bushing body.
4. The exhaust-gas turbocharger according to claim 1 , wherein said defined imbalance of said floating bushing body is partially formed by at least one blind bore formed into said floating bushing body.
5. The exhaust-gas turbocharger according to claim 1 , wherein said defined imbalance of said floating bushing body is partially formed by a through-bore formed into said floating bushing body.
6. The exhaust-gas turbocharger according to claim 5 , wherein said floating bushing body has a plurality of oil supply bores formed therein, and said through-bore partially forming said defined imbalance is an oil supply bore having a diameter larger than a diameter of other said oil supply bores.
7. The exhaust-gas turbocharger according to claim 5 , wherein said through-bore is a through-bore provided in addition to oil supply bores formed in said floating bushing body.
8. The exhaust-gas turbocharger according to claim 1 , wherein said defined imbalance of said floating bushing body is partially formed by an internal groove formed into said floating bushing body, wherein said internal groove does not form part of a through-bore formed into said floating bushing body.
9. The exhaust-gas turbocharger according to claim 1 , wherein said defined imbalance of said floating bushing body is partially formed by a deformation of an outer shell of said floating bushing body, wherein said deformation does not form part of a through-bore formed into said floating bushing body.
10. The exhaust-gas turbocharger according to claim 9 , wherein said deformation is formed by a removal of material from said outer shell of said floating bushing body.
11. An exhaust-gas turbocharger, comprising:
a common rotor shaft, an exhaust-gas turbine with a turbine wheel mounted on said rotor shaft, and a fresh-air compressor with a compressor wheel mounted on said rotor shaft;
said rotor shaft with said turbine wheel and said compressor wheel together forming a turbo rotor;
at least one radial bearing rotatably mounting said rotor shaft in a bearing housing;
said at least one radial bearing being a floating-bushing bearing having a floating bushing body formed as a hollow cylinder with an inner diameter for receiving said rotor shaft and with an outer diameter by which said floating bushing body is received in a bearing receptacle, wherein an inner lubrication gap is formed between said rotor shaft and said inner diameter of said floating bushing body and an outer lubrication gap is formed between a bearing receptacle and said outer diameter; and
said floating bushing body being formed with a defined imbalance with respect to an axis of rotation, said imbalance counteracting, in a stabilizing fashion, an imbalance of said turbo rotor during operation;
wherein said defined imbalance of said floating bushing body is an eccentric arrangement of said inner diameter of said floating bushing body in relation to said outer diameter of said floating bushing body.