Exhaust Tract For An Internal Combustion Engine

Patent metadata

Field	Value
Publication number	US-2016356207-A1
Application number	US-201615174294-A
Country	US
Kind code	A1
Filing date	Jun 6, 2016
Priority date	Jun 6, 2015
Publication date	Dec 8, 2016
Grant date	—

Abstract

An exhaust tract for an internal combustion engine, having an exhaust turbine having a housing and a turbine flow duct, into which exhaust gas flow coming from the engine flows, a wastegate, by which a proportion of the exhaust gas can bypass the turbine rotor, the turbine flow duct ducting the exhaust gas flow via the turbine rotor, and the wastegate on a discharge side of the exhaust turbine. The exhaust turbine-side outlet chamber is subdivided into a first exhaust turbine-side turbine exhaust gas flow inlet area, into which the exhaust gas flow coming from the turbine rotor flows, and a second exhaust turbine-side wastegate exhaust gas flow inlet area flow-separated from the first inlet area. A wastegate flow duct is provided adjoining the wastegate exhaust gas flow inlet area downstream of where the turbine exhaust gas flow inlet area opens.

First claim

What is claimed is:

1 . An exhaust tract for an internal combustion engine comprising:
an exhaust turbine of an exhaust turbocharger arranged in the exhaust tract and having an exhaust turbine housing and comprising a turbine flow duct, into which an exhaust gas flow coming from the internal combustion engine flows a turbine rotor of the exhaust turbine, driven by the exhaust gas flow arranged in the turbine flow duct, a wastegate by which a proportion of the exhaust gas flow flowing into the exhaust turbine can be made to bypass the turbine rotor as a wastegate exhaust gas flow, an exhaust turbine-side outlet chamber subdivided into a first exhaust turbine-side turbine exhaust gas flow inlet area and a second exhaust turbine-side wastegate exhaust gas flow inlet area flow-separated from the first inlet area and into which the turbine flow duct ducting the exhaust gas flow via the turbine rotor and the wastegate on a discharge side of the exhaust turbine open; a discharge duct adjoining the discharge side of the exhaust turbine and via which an exhaust gas flow from at least one of the turbine rotor and the wastegate exhaust gas flow fed via the wastegate flows out, wherein: the first exhaust turbine-side turbine exhaust gas flow inlet area adjoins the discharge duct and into which the exhaust gas flow coming from the turbine rotor flows, and the second exhaust turbine-side wastegate exhaust gas flow inlet area is configured to receive the exhaust gas flow fed via the wastegate; and a wastegate flow duct arranged adjoining the wastegate exhaust gas flow inlet area, down-stream of the turbine exhaust gas flow inlet area, tangentially into the adjoining discharge duct such that the wastegate exhaust gas flow introduced into the discharge duct via the wastegate flow duct flows through the discharge duct as a peripheral flow on an inside wall of the discharge duct and spirally around a central longitudinal axis of the discharge duct away from the exhaust turbine.

2 . The exhaust tract according to claim 1 , wherein the discharge duct directly adjoins the exhaust turbine-side turbine exhaust gas flow inlet area, such that the exhaust gas flow from the turbine rotor flows through the discharge duct in a direction of the central longitudinal axis of the discharge duct away from the exhaust turbine.

3 . The exhaust tract according to claim 2 , wherein outlet apertures of the exhaust turbine-side turbine exhaust gas flow inlet area and of the adjoining discharge duct are of substantially identical design, the outlet apertures of the exhaust turbine-side turbine exhaust gas flow inlet area and of the adjoining discharge duct aligned with one another.

4 . The exhaust tract according to claim 1 , wherein a cross sectional area of the wastegate flow duct is less than a cross sectional area of the discharge duct at least in an area where it opens into the discharge duct.

5 . The exhaust tract according to claim 1 , wherein the wastegate-flow duct, relative to a cross section through the discharge duct one of tangentially and eccentrically adjoins an outer wall portion of the discharge duct, such that an outer outlet-side duct wall portion of the wastegate flow duct lies substantially at a level of an apex of the discharge duct, and merges continuously into the discharge duct.

6 . The exhaust tract according to claim 5 , wherein a central longitudinal axis of the wastegate flow duct is situated at a defined distance from the apex of the discharge duct.

7 . The exhaust tract according to claim 1 , wherein the wastegate-flow duct opens angularly into the discharge duct forming an angle between the outlet-side area of the wastegate flow duct and the wastegate exhaust gas flow flowing into the discharge duct, and a cross sectional plane, formed by a cross section of the discharge duct in one of the outlet area and oriented transversely to longitudinal axis of the discharge duct in the outlet area of the wastegate flow duct on the other, the angle ranging from 30° to 80°.

8 . The exhaust tract according claim 1 , wherein the discharge duct has a round cross section.

9 . The exhaust tract according to claim 8 , wherein the round cross section of the discharge duct is substantially constant along the discharge duct.

10 . The exhaust tract according to claim 1 , wherein a cross section of the wastegate flow duct downstream of the wastegate is larger than a maximum aperture cross section of a wastegate aperture of the wastegate.

11 . The exhaust tract according claim 1 , wherein the exhaust turbine-side exhaust gas flow inlet area on the discharge side of the exhaust turbine is separated from the exhaust turbine-side wastegate exhaust gas flow inlet area by at least one dividing wall provided on an outlet chamber side.

12 . The exhaust tract according to claim 1 , wherein the discharge duct is a separate component connected to one of the exhaust turbine and an exhaust turbine housing.

13 . A method for operation of an exhaust tract for an internal combustion engine having an exhaust turbine of an exhaust turbocharger arranged in the exhaust tract, comprising:
an exhaust gas flow coming from the internal combustion engine flows in a turbine flow duct of the exhaust turbine, the exhaust turbine having an exhaust turbine housing in which a turbine rotor of the exhaust turbine, driven by the exhaust gas flow, is arranged; a proportion of the exhaust gas flow flowing into the exhaust turbine can be made to bypass the turbine rotor as a wastegate exhaust gas flow the exhaust turbine via a wastegate; wherein the turbine flow duct ducting the exhaust gas flow via the turbine rotor, and the wastegate arranged on a discharge side of the exhaust turbine open into an exhaust turbine-side outlet chamber, and wherein a discharge duct, via which an exhaust gas flow coming from at least one of the turbine rotor and the wastegate exhaust gas flow fed via the wastegate flows out, adjoins the discharge side of the exhaust turbine, subdividing the exhaust turbine-side outlet chamber into a first exhaust turbine-side turbine exhaust gas flow inlet area, into which the exhaust gas flow coming from the turbine rotor flows adjoins the discharge duct, and a second exhaust turbine-side wastegate exhaust gas flow inlet area, which is flow-separated from the first inlet area and into which the exhaust gas flow fed via the wastegate flows, and providing a wastegate flow duct adjoining the wastegate exhaust gas flow inlet area, which downstream of the turbine exhaust gas flow inlet area opens, in particular tangentially, into the adjoining discharge duct, such that the wastegate exhaust gas flow introduced into the discharge duct via the wastegate flow duct flows through the discharge duct as a peripheral flow on an inside wall of the discharge duct and spirally around a central longitudinal axis of the discharge duct in a direction away from the exhaust turbine.

14 . An internal combustion engine comprising:
an exhaust tract for an internal combustion engine comprising: an exhaust turbine of an exhaust turbocharger arranged in the exhaust tract and having an exhaust turbine housing and comprising a turbine flow duct, into which an exhaust gas flow coming from the internal combustion engine flows a turbine rotor of the exhaust turbine, driven by the exhaust gas flow arranged in the turbine flow duct, a wastegate by which a proportion of the exhaust gas flow flowing into the exhaust turbine can be made to bypass the turbine rotor as a wastegate exhaust gas flow, an exhaust turbine-side outlet chamber subdivided into a first exhaust turbine-side turbine exha

Assignees

• Man Truck & Bus Ag

Inventors

• Menard Pierre

Classifications

• F02B37/18

  by bypassing exhaust {from the inlet to the outlet of turbine or to the atmosphere} · CPC title

• F02B37/183 Primary

  Arrangements of bypass valves or actuators therefor · CPC title

• F01N2340/06

  Arrangement of the exhaust apparatus relative to the turbine of a turbocharger · CPC title

• F01N13/08

  Other arrangements or adaptations of exhaust conduits {(pipes, joints or supports therefor in general F16L; collecting or removing exhaust gases of vehicle engines in workshops B08B15/00, on highways E01C1/005)} · CPC title

• F01N2260/06

  for improving exhaust evacuation or circulation, or reducing back-pressure · CPC title