Exhaust-gas turbocharger

• US 6,598,395 B2
• Filed: 06/07/2002
• Issued: 07/29/2003
• Est. Priority Date: 06/08/2001
• Status: Expired due to Fees

• Current Assignee: Daimler Chrysler Company LLC (Stellantis NV)
• Original Assignee: Daimler Chrysler Company LLC (Stellantis NV)
• Inventors: Spurk, Joseph, Schenkel, Stephan, Daudel, Helmut
• Primary Examiner(s): NGUYEN, HOANG M
• Application Number:
  US10/165,172
• Publication Number:
  US 20020184882A1
• Time in Patent Office: 417 Days
• Field of Search: 606/051, 606/02, 606/05, 123/559.1, 123/559.2, 123/563
• US Class Current: 60/602
• CPC Class Codes: F01D 17/146 by throttling the volute inlet of radial machines or engines
• CPC Class Codes: F02B 37/22 by varying cross-section of exhaust passages or air passages , e.g. by throttling turbine inlets or outlets or by varying effective number of guide conduits F02B37/24 takes precedence
• CPC Class Codes: F05D 2220/40 in turbochargers
• CPC Class Codes: Y02T 10/12 Improving ICE efficiencies

Abstract

In an exhaust-gas turbocharger having a compressor and an exhaust-gas turbine, which drives the compressor and comprises a multipart exhaust gas supply duct manifold and a turbine rotor, to which pressurized exhaust gas can be delivered by way of the exhaust gas supply duct, the exhaust gas supply duct manifold includes at least three flow passages, which, except for one, are provided with shut-off flaps, which are adjustable independently of one another.

Claims

1. An exhaust-gas turbocharger including a compressor and an exhaust-gas turbine, which drives the compressor, said turbine comprising a turbine housing having an exhaust gas inlet and a turbine rotor, to which pressurized exhaust gas can be delivered by way of the exhaust gas inlet, said exhaust gas inlet being of multipart design with at least three flow ducts a number of which flow ducts can each be closed by a shut-off flap pivotally supported in the respective flow duct, at least one of said flow ducts being designed without any flap, all shut-off flaps being adjustable independently of one another.

2. An exhaust-gas turbocharger according to claim 1, wherein said exhaust gas inlet includes two outer flow ducts each being provided with a shut-off flap.

3. An exhaust-gas turbocharger according to claim 2, wherein the shut-off flaps are pivotally supported in such a way that they are disposed adjacent an inside wall of the turbine housing when they are open.

4. An exhaust-gas turbocharger according to claim 3, wherein the shut-off flaps are pivotally supported on an inside wall of a collecting chamber in the turbine housing, from which the flow ducts branch off, the shut-off flaps being arranged in the area of the inlets of the flow ducts.

5. An exhaust-gas turbocharger according to claim 1, wherein the shut-off flaps are designed to conform to the contour of the inside wall of the turbine housing and, in an open position, fit precisely against the inside wall.

6. An exhaust-gas turbocharger according to claim 1, wherein the flow ducts extend essentially parallel.

7. An exhaust-gas turbocharger according to claim 1, wherein at least some of the flow ducts have different inlet cross sections.

8. An exhaust-gas turbocharger according to claim 7, wherein a total of three flow ducts are provided, of which two flow ducts have an inlet cross-section essentially equal in size and one flow duct has an inlet cross section essentially twice as large as each of the other two flow ducts.

9. An exhaust-gas turbocharger according to claim 7, wherein a total of three flow ducts are provided, the inlet cross sections of which are in a ratio of 3:

2;

1 to one another.

10. An exhaust-gas turbocharger according to claim 1, wherein a flow guide vane structures disposed upstream of the turbine rotor for directing the exhaust gas onto the turbine rotor.

11. An exhaust-gas turbocharger according to claim 1, wherein the exhaust manifold is divided into hermetically separated angular sections, one angular section being assigned to each flow duct.

12. An exhaust-gas turbocharger according to claim 11, wherein the ratio of the angular sections corresponds to the ratio of the inlet cross sections of the flow ducts.