Exhaust-gas turbo charger for an internal combustion engine, and method for producing an exhaust-gas turbocharger

Patent metadata

Field	Value
Publication number	US-10890107-B2
Application number	US-201515522153-A
Country	US
Kind code	B2
Filing date	Oct 24, 2015
Priority date	Oct 27, 2014
Publication date	Jan 12, 2021
Grant date	Jan 12, 2021

Abstract

An exhaust gas turbocharger for an internal combustion engine, includes a turbine; a bypass line fluidly arranged parallel to the turbine; and a cross section adjustment element for adjusting a flow cross section of the bypass line, wherein the cross section adjustment element being configured as a ball valve having a valve housing, two bearing shells arranged in the valve housing and a valve element. The valve element is floatingly supported in the valve housing and arranged between the two bearing shells with a tolerance in a direction which is angled with respect to a rotation axis of the valve element.

First claim

The invention claimed is:

1. An exhaust gas turbocharger for an internal combustion engine, comprising:
a turbine;
a bypass line fluidly arranged parallel to the turbine; and
a cross section adjustment element for adjusting a flow cross section of the bypass line, said cross section adjustment element being configured as a ball valve having a valve housing, two fixed bearing sheds arranged in the valve housing and a valve element, said valve element being floatingly supported in the valve housing and arranged with a tolerance between the two bearing shells such that the valve element always contacts at most one of the bearing shells while spaced apart from the respective other bearing shell when the cross section adjustment element is at least partial closed and exhaust gas pressure acting on the valve element urges the valve element in a direction of one of the bearing shells or the valve element does not contact either of the bearing shells;
wherein the two bearing shells each have a flow passage with a first flow cross section and a receiving opening into which the valve element partially engages to provide a valve seat when the valve element contacts one of the bearing shells;
wherein the valve element has a flow channel having a second flow cross section which equals the first flow cross section so that in at least one rotary angular position of the valve element, the flow passage of the two bearing shells aligns with the flow channel of the valve element; and
wherein the valve element does not contact either of the bearing shells when there is either no exhaust gas pressure acting on the valve element or the flow passage of the two bearing shells aligns with the flow channel of the valve element.

2. The exhaust gas turbocharger of claim 1 , wherein the valve housing has a mounting opening adapted for insertion of the valve element together with the two bearing shells into the valve housing.

3. The exhaust gas turbocharger of claim 2 , further comprising a lid closing the mounting opening, said lid having a through opening, and an adjustment shaft operatively connected with the valve element and traversing the through opening.

4. The exhaust gas turbocharger of claim 3 , further comprising a bearing element fastened on the lid, said bearing element having a further through opening for receiving the adjustment shaft.

5. The exhaust gas turbocharger of claim 4 , wherein at least one of the through opening and the further through opening has an inner diameter which is greater than an outer diameter of the adjustment shaft.

6. The exhaust gas turbocharger of claim 4 , further comprising a bearing sleeve arranged between the lid and the bearing element, said bearing sleeve engaging about the adjustment shaft in a circumferential direction.

7. The exhaust gas turbocharger of claim 6 , wherein the bearing sleeve is in continuous sealing contact with the adjustment shaft in the circumferential direction.

8. The exhaust gas turbocharger of claim 3 , wherein the adjustment shaft is configured in one piece.

9. The exhaust gas turbocharger of claim 3 , wherein the adjustment shaft is made of a same material as the valve element.

10. The exhaust gas turbocharger of claim 1 , wherein the turbine is connected to an exhaust gas line via a turbine outlet, said exhaust gas line having a cross section which is greater than the valve housing, said valve housing being arranged in the exhaust gas line.

11. The exhaust gas turbocharger of claim 1 , wherein the valve housing is integrated in a turbine housing of the turbine.

12. The exhaust gas turbocharger of claim 1 , wherein the valve housing has a flow outlet which widens in a direction away from the valve element.

13. A method for producing an exhaust gas turbocharger for an internal combustion engine, said method comprising:
providing a cross section adjustment element configured as a ball valve, said cross section adjustment element being adapted for adjusting a flow cross section of a bypass line of the exhaust gas turbocharger, said bypass line being arranged fluidly parallel to a turbine of the exhaust gas turbocharger;
providing two fixed bearing shells in a valve housing of the cross section adjustment element;
floatingly supporting a valve element in the valve housing; and
arranging the valve element with a tolerance between the two bearing shells such that the valve element always contacts at most one of the bearing shells while spaced apart from the respective other bearing shell when the cross section adjustment element is at least partially closed and exhaust gas pressure acting on the valve element urges the valve element in a direction of one of the bearing shells or the valve element does not contact either of the bearing shells;
wherein the two bearing shells each have a flow passage with a first flow cross section and a receiving opening into which the valve element partially engages to provide a valve seat when the valve element contacts one of the bearing shells;
wherein the valve element has a flow channel having a second flow cross section which equals the first flow cross section so that in at least one rotary angular position of the valve element the flow passage of the two bearing shells aligns with the flow channel of the valve element; and
wherein the valve element does not contact either of the bearing shells when there is either no exhaust gas pressure acting on the valve element or the flow passage of the two bearing shells aligns with the flow channel of the valve element.

Assignees

• Audi Ag

Inventors

• Lindner Marko
• Bäumel Franz
• Köhnlein Maximilian
• Simon Dominik

Classifications

• F01D17/105

  by passing part of the fluid · CPC title

• F16K5/0647

  Spindles or actuating means · CPC title

• F02B37/183 Primary

  Arrangements of bypass valves or actuators therefor · CPC title

• Y02T10/12

  Improving ICE efficiencies · CPC title

• F05D2220/40

  in turbochargers · CPC title