Turbocharger having fastening elements for fastening vane bearing rings of a variable turbine geometry VTG
View Patent ↗A turbocharger with a variable turbine geometry device has one or two blade bearing rings. At least one or more fastening elements are provided for fastening the one or two blade bearing rings. The respective fastening element has at least one section formed with a knurl and/or at least one section formed with at least one or several notches.
1. A turbocharger, comprising:
a variable turbine geometry device with one or two vane bearing ring elements;
at least one or more fastening elements for fastening said one or two vane bearing ring elements, said at least one fastening element having at least one section formed with a knurl and/or at least one section formed with at least one or more notches;
wherein said vane bearing ring element is formed with bore for receiving said fastening element, and wherein a section of said bore of the respective said vane bearing ring element together with said region of said fastening element formed with said knurl or said one or more notches forms a press fit, and wherein said bore together with a region of said fastening element that is not formed with said knurl or with said notches forms a clearance fit.
2. The turbocharger according to claim 1 , wherein said at least one of more fastening elements is a plurality of fastening elements each having said at least one section formed with said knurl and/or at least one section formed with said one or more notches.
3. The turbocharger according to claim 1 , wherein said at least one fastening element is a pin element.
4. The turbocharger according to claim 3 , wherein said at least one fastening element is a cylindrical pin.
5. The turbocharger according to claim 4 , wherein two vane bearing ring elements are positioned in relation to each other via at least one or more fastening element(s) in each case.
6. The turbocharger according to claim 1 , wherein said at least one fastening element is formed with said knurl over an entire length thereof or over at least one or more sections.
7. The turbocharger according to claim 6 , wherein said knurl is a longitudinal knurl or a helical knurl.
8. The turbocharger according to claim 1 , wherein said at least one fastening element is a pin element formed with at least one, two, three, or more notches over an entire length thereof or over at least one or more sections.
9. The turbocharger according to claim 8 , wherein said pin element is a notched pin having a plurality of notches formed therein.
10. The turbocharger according to claim 9 , wherein said notched pin is a pin element selected form the group consisting of a tapered notched pin, a center-grooved notched pin, a conical notched pin, and a close tolerance notched pin.
11. The turbocharger according to claim 8 , wherein said vane bearing ring element is formed with bore for receiving said fastening element, and wherein a fit between said fastening element and an associated said bore in said vane bearing ring element, in a region of said knurl or of said notch, is a press fit.
12. The turbocharger according to claim 1 , wherein a center section or two end sections of said fastening element is formed with said knurl or with said one or more notches.
13. The turbocharger according to claim 12 , wherein said center section or said two end sections of said fastening element are formed with a longitudinal knurl or a helical knurl.
14. The turbocharger according to claim 1 , wherein said fastening element is formed with a knurl or one or more notches along an entire overall length, and said overall length of said fastening element is less than an overall length of said vane bearing ring elements and of guide vanes disposed in between in each case.