IP Library Granted Patent US 9,828,913
Granted Patent B2
US 9,828,913 · App. 14/338,579 · Granted Nov 28, 2017

Turbine housing

Inventors: Clayton A. Sloss (Paris, CA); Joseph Gerald Jimmie Coulombe (Brantford, CA)
Assignee: WESCAST INDUSTRIES, INC.
F02C7/04F01D9/026F02C6/12F05D2210/12F05D2220/40F05D2240/15F05D2260/20F05D2260/231F05D2300/121F05D2300/502F05D2300/5023F05D2300/50212
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Quick Facts
Patent No.
US 9,828,913
App. No.
14/338,579
Granted
Nov 28, 2017
Kind
B2
Abstract

A turbocharger system may include a turbine housing and a tongue insert. The turbine housing may include an inlet, an outlet, and a gas pathway between the inlet and outlet. The gas pathway may include a volute portion and an inlet portion extending approximately tangent to the volute portion. The turbine housing may be formed from a first material. The tongue insert may be received in the turbine housing and may at least partially define the volute portion and the inlet portion. The tongue insert may be formed from a second material that is more heat resistant than the first material.

Claims (10)

1. A turbocharger system comprising:

a turbine housing including an inlet, an outlet, and a gas pathway between the inlet and outlet, the gas pathway including a volute portion and an inlet portion extending approximately tangent to the volute portion, the turbine housing being formed from a first material; and

a tongue insert received in the turbine housing and at least partially defining the volute portion and the inlet portion, the tongue insert being formed from a second material that is more heat resistant than the first material and including an annular ring portion and a non-annular tongue portion, the tongue portion extending axially outward from an axial end of the ring portion and into the volute portion, the tongue portion defining an intersection between the inlet portion and the volute portion,

wherein the ring portion encircles a rotational axis of a shaft of a turbine disposed within the turbine housing,

wherein the ring portion has an inner diameter that is larger than an outermost diameter of a blade of the turbine,

wherein the entire ring portion is disposed within the turbine housing, and

wherein the ring portion at least partially defines the volute portion of the gas pathway.

2. The turbocharger system of claim 1 , wherein the ring portion is sandwiched between the turbine housing and a turbine bearing housing.

3. The turbocharger system of claim 2 , wherein the tongue portion is received in a recess in the turbine housing.

4. The turbocharger system of claim 3 , wherein the turbine housing includes a coolant passage formed therein.

Assignments (2)
SECURITY INTEREST Recorded Jun 26, 2018
From: WESCAST INDUSTRIES INC.
To: WELLS FARGO CAPITAL FINANCE CORPORATION CANADA, AS AGENT
Reel/Frame 046200/0889 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 23, 2014
From: SLOSS, CLAYTON A.; COULOMBE, JOSEPH GERALD JIMMIE
To: WESCAST INDUSTRIES, INC.
Reel/Frame 033372/0627 →
Continuity (2)
Provisional Application 61866641 · Aug 16, 2013
Related Publication 20150050131A1 · Feb 19, 2015