Diffuser in wastegate turbine housings

Patent metadata

Field	Value
Publication number	US-10731546-B2
Application number	US-201715425134-A
Country	US
Kind code	B2
Filing date	Feb 6, 2017
Priority date	Feb 6, 2017
Publication date	Aug 4, 2020
Grant date	Aug 4, 2020

Abstract

A number of variations may include a turbine housing comprising a turbine body; an inlet passage and an outlet passage connected to the turbine body; a wastegate passage operatively connected to the outlet passage; a diffuser positioned within the outlet passage comprising at least one radial opening; wherein the first flow passage accepts fluid flow from the wastegate passage and the second flow passage accepts fluid flow from the turbine wheel; wherein a first end of the diffuser is attached to a first end of the turbine outlet and a second end of the diffuser is attached to a second end of the turbine outlet so that fluid flow from the first flow passage is directed into the second flow passage through the at least one radial opening before exiting the outlet passage, and wherein the at least one radial opening minimizes turbulence of fluid flow exiting the turbine housing.

First claim

What is claimed is:

1. A method comprising:
fabricating a turbine housing comprising a body constructed and arranged to house a turbine wheel; an inlet passage connected to the body constructed and arranged to direct fluid flow into the body; an outlet passage connected to the body constructed and arranged to direct fluid flow out of the turbine housing;
drilling a wastegate passage between the inlet passage and the outlet passage of the turbine housing; and
wherein a first end of the diffuser includes one or more radial lips which extend outward from the outer surface of the diffuser; wherein an inner surface of the outlet passage includes one or more radial grooves; and wherein the one or more radial lips snap into the one or more radial grooves to lock the diffuser into place,
attaching a diffuser within the outlet passage comprising snapping one or more radial lips of the diffuser into one or more radial grooves or channels in a first end of the turbine outlet passage, wherein the diffuser is constructed and arranged to define a first flow passage and a second flow passage, wherein the first flow passage is defined by an inner surface of the outlet passage and an outer surface of the diffuser and the second flow passage is defined by an inner surface of the diffuser, and wherein the snapping one or more radial lips of the diffuser into one or more radial grooves or channels in a first end of the turbine outlet passage provide a diffuser to turbine housing connection that allows for variances in thermal growth between the diffuser and the turbine housing,
where the diffuser includes at least one radial opening defined by a surface of the diffuser and extending through the body of the diffuser so that fluid flow from the first flow passage is directed to the second flow passage through the at least one radial opening before exiting the outlet passage, and wherein the at least one radial opening is adjacent the first end of the diffuser adjacent an exit of the outlet passage.

2. A method as set forth in claim 1 wherein the diffuser comprises a body and wherein one or more exit ports extend through the body.

3. A method as set forth in claim 1 wherein the attachment between the diffuser and the turbine housing is constructed and arranged to allow for variances in thermal growth between the diffuser and the turbine housing.

4. The method of claim 1 wherein at least one of the outlet passage or the body is constructed and arranged to include a radial seat to support a second end of the diffuser.

Assignees

• Borgwarner Inc

Inventors

• Mchenry Joseph P
• Olin Daniel M
• Kurle Charles J
• Jenks Gordon C
• Wallace Robert M

Classifications

• F05D2230/21

  by casting · CPC title

• F02B37/18 Primary

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

• F01D25/24 Primary

  Casings (modified for heating or cooling F01D25/14); Casing parts, e.g. diaphragms, casing fastenings (casings for rotary machines or engines in general F16M {; special arrangements in stators dealing with breaking-off of part of rotor F01D21/045}) · CPC title

• F01D17/14

  varying effective cross-sectional area of nozzles or guide conduits · CPC title

• F05D2220/40

  in turbochargers · CPC title