Flap device for opening and closing a wastegate channel in a turbine housing of a turbocharger, turbocharger, and method for production
A flap configuration opens and closes a wastegate channel in a turbine housing of a turbocharger. The flap configuration has a lever element having a through-bore in which a cylindrical bushing is arranged. A flap having a pin is arranged on the lever element such that the pin passes through the bushing. A cover disk is arranged on an opposite side from the flap and has an opening through which the pin of the flap passes. The flap is riveted to the lever element by the pin.
1. A flap configuration for opening and closing a wastegate duct in a turbine housing of a turbocharger, the flap configuration comprising:
a cylindrical bushing having at least one groove formed therein;
a lever having a through-bore formed therein and in said through-bore said cylindrical bushing is disposed;
a spring sheet disposed in said at least one groove such that a radial clamping force of said spring sheet acts between said through-bore and said cylindrical bushing;
a flap having a pin disposed on said lever element such that said pin passes through said cylindrical bushing;
a cover disk disposed on an opposite side from said flap and having an opening formed therein through which said pin of said flap passes; and
said flap is riveted to said lever by means of said pin.
2. The flap device according to claim 1 , wherein said through-bore, said cylindrical bushing and said pin are dimensioned with respect to one another such that, before riveting, a radial clearance is formed between said cylindrical bushing and said through-bore and between said cylindrical bushing and said pin.
3. The flap device according to claim 1 , wherein said cover disk rests on said cylindrical bushing.
4. The flap device according to claim 1 , wherein said cover disk and said cylindrical bushing are formed in one piece.
5. The flap device according to claim 1 , wherein said spring sheet is formed and/or has been introduced into said groove such that said spring sheet protrudes at at least one axial end of said cylindrical bushing with regard to an axial direction of extension of said cylindrical bushing in a mounted state before riveting, and an axial clamping force of said spring sheet acts with regard to the axial direction of extension after riveting.
6. A turbocharger for an internal combustion engine, the turbocharger comprising:
a rotor shaft;
a bearing housing in which said rotor shaft is mounted in a rotatable manner;
a turbine wheel disposed for conjoint rotation on said rotor shaft;
a turbine housing mechanically secured to said bearing housing;
a wastegate duct formed in said turbine housing; and
a flap configuration for opening and closing said wastegate duct, said flap configuration containing:
a cylindrical bushing having at least one groove formed therein;
a lever having a through-bore formed therein and in said through-bore said cylindrical bushing is disposed;
a spring sheet disposed in said at least one groove such that a radial clamping force of said spring sheet acts between said through-bore and said cylindrical bushing;
a flap having a pin disposed on said lever element such that said pin passes through said cylindrical bushing;
a cover disk disposed on an opposite side from said flap and having an opening formed therein through which said pin of said flap passes; and
said flap is riveted to said lever by means of said pin.
7. A method for producing a flap configuration, which comprises the steps of:
providing a lever having a through-bore formed therein;
providing a bushing having at least one groove formed therein and a spring sheet disposed in the at least one groove, and introducing the bushing into the through-bore in the lever together with the spring sheet, such that a radial clamping force acts between the through-bore and the bushing;
providing a flap having a pin;
disposing the flap on the lever such that the pin passes through the bushing;
placing a cover disk on an opposite side from the flap such that the pin projects through an opening in the cover disk; and
riveting the flap to the lever by means of the pin.
8. The method according to claim 7 , wherein, after the flap has been disposed on the lever, a respective radial clearance is formed between the pin and the bushing and between the bushing and the through-bore.
9. The method according to claim 7 , wherein the spring sheet is formed and/or has been introduced into the groove such that before the riveting the spring sheet protrudes at least partially at an axial end of the bushing, and during the riveting the spring sheet is axially clamped and an axial clamping force of the spring sheet acts with regard to an axial direction of extension of the bushing.