Turbine outlet diffuser

Patent metadata

Field	Value
Publication number	US-9689397-B2
Application number	US-201514713498-A
Country	US
Kind code	B2
Filing date	May 15, 2015
Priority date	Jun 13, 2014
Publication date	Jun 27, 2017
Grant date	Jun 27, 2017

Abstract

A turbocharger for an internal combustion engine includes a rotating assembly having a turbine wheel disposed inside a turbine housing and a compressor wheel disposed inside a compressor cover. The turbine housing defines a turbine outlet cavity, a turbine housing inlet, and a turbine housing outlet. The turbine housing inlet is configured to channel engine post-combustion gases to the turbine wheel and the turbine housing outlet is configured to exhaust the gases aft of the turbine wheel. A diffuser arranged inside the turbine outlet cavity is configured to channel the post-combustion gases aft of the turbine wheel and out to the turbine housing outlet, without discharging into the turbine outlet cavity.

First claim

The invention claimed is:

1. A turbocharger assembly for pressurizing an airflow for delivery to an internal combustion engine that generates post-combustion gases, the turbocharger assembly comprising:
a compressor cover;
a turbine housing defining a turbine outlet cavity, a turbine housing inlet, and a turbine housing outlet;
a rotating assembly having a turbine wheel disposed inside the turbine housing and a compressor wheel disposed inside the compressor cover, wherein the rotating assembly is rotated about an axis by the post-combustion gases, and wherein the turbine housing inlet is configured to channel the post-combustion gases to the turbine wheel and the turbine housing outlet is configured to exhaust the post-combustion gases aft of the turbine wheel;
a waste-gate valve arranged in the turbine housing and configured to selectively redirect at least a portion of the post-combustion gases into the turbine outlet cavity in bypass of the turbine wheel; and
a diffuser arranged inside the turbine outlet cavity, having an outer surface including a cylindrical upstream portion and a flared downstream portion, and configured to separately channel the post-combustion gases aft of the turbine wheel and the portion of post-combustion gases redirected by the waste-gate valve and out to the turbine housing outlet, without discharging into the turbine outlet cavity, to thereby limit disruption of flow of the post-combustion gases aft of the turbine wheel by the portion of post-combustion gases redirected by the waste-gate valve;
wherein:
the diffuser extends beyond the turbine housing outlet; and
a plane perpendicular to the axis intersects each of the turbine housing outlet and the flared downstream portion.

2. The turbocharger assembly of claim 1 , wherein the diffuser includes an outer surface configured to receive and channel the portion of post-combustion gases redirected by the waste-gate valve to the turbine housing outlet.

3. The turbocharger assembly of claim 1 , further comprising a catalytic converter close-coupled to the turbine housing outlet, and wherein the diffuser extends beyond the turbine housing outlet to maintain streamlined and focused flow of the post-combustion gases beyond the turbine housing outlet and out to the catalytic converter.

4. The turbocharger assembly of claim 1 , wherein the turbine housing and the diffuser are separate components, and wherein the diffuser is fixed to the turbine housing.

5. The turbocharger assembly of claim 4 , wherein the diffuser is a steel pipe.

6. The turbocharger assembly of claim 4 , wherein the diffuser is fastened to the turbine housing via a snap ring.

7. The turbocharger assembly of claim 6 , wherein the diffuser includes a first end and a second end, and wherein the first end includes a flange and the snap ring abuts the flange to thereby fix the diffuser to the turbine housing.

8. An internal combustion engine comprising:
a cylinder configured to receive an air-fuel mixture for combustion therein;
a reciprocating piston disposed inside the cylinder and configured to exhaust post-combustion gases therefrom; and
a turbocharger assembly in fluid communication with the piston and configured to pressurize an airflow being received from the ambient and deliver the pressurized airflow to the cylinder, the turbocharger assembly including:
a compressor cover, and a turbine housing defining a turbine outlet cavity, a turbine housing inlet, and a turbine housing outlet;
a rotating assembly having a turbine wheel disposed inside the turbine housing and a compressor wheel disposed inside the compressor cover, wherein the rotating assembly is rotated about an axis by the post-combustion gases, and wherein the turbine housing inlet is configured to channel the post-combustion gases to the turbine wheel and the turbine housing outlet is configured to exhaust the post-combustion gases aft of the turbine wheel;
a waste-gate valve arranged in the turbine housing and configured to selectively redirect at least a portion of the post-combustion gases into the turbine outlet cavity in bypass of the turbine wheel; and
a diffuser arranged inside the turbine outlet cavity, having an outer surface including a cylindrical upstream portion and a flared downstream portion, and configured to separately channel the post-combustion gases aft of the turbine wheel and the portion of post-combustion gases redirected by the waste-gate valve and out to the turbine housing outlet, without discharging into the turbine outlet cavity, to thereby limit disruption of flow of the post-combustion gases aft of the turbine wheel by the portion of post-combustion gases redirected by the waste-gate valve;
wherein:
the diffuser extends beyond the turbine housing outlet; and
a plane perpendicular to the axis intersects each of the turbine housing outlet and the flared downstream portion.

9. The engine of claim 1 , wherein the diffuser includes an outer surface configured to receive and channel the portion of post-combustion gases redirected by the waste-gate valve to the turbine housing outlet.

10. The engine of claim 1 , further comprising a catalytic converter close-coupled to the turbine housing outlet, and wherein the diffuser extends beyond the turbine housing outlet to maintain streamlined and focused flow of the post-combustion gases beyond the turbine housing outlet and out to the catalytic converter.

11. The engine of claim 1 , wherein the turbine housing and the diffuser are separate components, and wherein the diffuser is fixed to the turbine housing.

12. The engine of claim 11 , wherein the diffuser is a steel pipe.

13. The engine of claim 11 , wherein the diffuser is fastened to the turbine housing via a snap ring.

14. The engine of claim 13 , wherein the diffuser includes a first end and a second end, and wherein the first end includes a flange and the snap ring abuts the flange to thereby fix the diffuser to the turbine housing.

Assignees

• Gm Global Tech Operations Llc

Inventors

• Edwards Brian J
• Begin Louis P
• Williams Carnell E

Classifications

• F05D2220/40

  in turbochargers · CPC title

• F05D2250/52

  Outlet · CPC title

• F02B37/00

  Engines characterised by provision of pumps driven at least for part of the time by exhaust · CPC title

• F01D9/026 Primary

  Scrolls for radial machines or engines · CPC title

• F05D2250/324

  divergent · CPC title