IP Library Granted Patent US 8,353,666
Granted Patent B2
US 8,353,666 · App. 13/187,295 · Granted Jan 15, 2013

Turbocharger assembly having heat shield-centering arrangements

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Quick Facts
Patent No.
US 8,353,666
App. No.
13/187,295
Granted
Jan 15, 2013
Kind
B2
Abstract

A turbocharger for internal combustion engines, having a heat shield disposed between a turbine housing and center housing of the turbocharger for shielding the center housing from exhaust gases passing through the turbine. The heat shield in one embodiment is centered on a generally conical surface of the center housing, by engagement between the conical surface and a centering portion of the heat shield. In another embodiment, the heat shield has a generally conical portion that is non-axisymmetric, having a plurality of radially enlarged lobes that engage a radially inwardly facing surface of the turbine housing for centering the heat shield.

Claims (13)

1. An assembly for a turbocharger, comprising:

a turbine comprising a turbine housing and a turbine wheel mounted in the turbine housing and connected to a rotatable shaft for rotation therewith;

a center housing for containing a bearing for the shaft, the center housing defining a generally planar first surface facing generally axially toward and axially spaced from a generally planar opposing surface of the turbine housing, the first surface being spaced axially from the turbine wheel by a first axial distance;

the turbine housing further comprising a generally cylindrical surface facing radially inwardly and located radially inwardly relative to said opposing surface; and

a heat shield disposed between the center housing and the turbine housing, the heat shield having an outer portion captured between the first surface of the center housing and the opposing surface of the turbine housing, and a centering portion extending from the outer portion generally axially toward the turbine wheel, the centering portion passing directly radially inwardly of the generally cylindrical surface of the turbine housing, the centering portion having a non-axisymmetric configuration characterized by a plurality of relatively smaller-radius portions alternating in a circumferential direction with a plurality of relatively larger-radius portions, radial clearances existing between the smaller-radius portions and the generally cylindrical surface of the turbine housing, the larger-radius portions engaging the generally cylindrical surface of the turbine housing so as to locate the heat shield substantially coaxially with respect to a central longitudinal axis of the turbine housing.

2. The assembly of claim 1 , wherein the heat shield includes an inner portion joined with the centering portion and extending radially inwardly therefrom, and the inner portion is axially spaced from the center housing.

3. The assembly of claim 1 , wherein the center housing includes a generally cylindrical surface facing radially outwardly and located radially outwardly relative to the first surface and spaced axially from the turbine wheel by a distance greater than the first axial distance, the generally cylindrical surface of the center housing being substantially coaxial with a central longitudinal axis of the center housing, and the turbine housing includes a second generally cylindrical surface facing radially inwardly and engaged with the generally cylindrical surface of the center housing for coaxially locating the turbine housing relative to the center housing.

4. The assembly of claim 3 , wherein a juncture extends between the second generally cylindrical surface of the turbine housing and said opposing surface of the turbine housing, the juncture comprising a smoothly curved radius.

5. The assembly of claim 4 , wherein a radially outermost edge of the heat shield is spaced radially inward of the juncture.

6. The assembly of claim 1 , wherein the heat shield has four of the relatively larger-radius portions spaced about a circumference of the heat shield.

7. A heat shield for being disposed between a center housing and a turbine housing of a turbocharger, the heat shield comprising:

a generally annular body having an annular outer portion that extends generally radially and a centering portion that extends generally axially from a radially inner end of the outer portion, the centering portion having a non-axisymmetric configuration characterized by a plurality of relatively smaller-radius portions alternating in a circumferential direction with a plurality of relatively larger-radius portions.

8. The heat shield of claim 7 , further comprising an inner portion joined with the centering portion and extending radially inwardly therefrom.

Assignments (6)
CORRECTIVE ASSIGNMENT TO CORRECT THE THE TYPOS IN THE APPLICATION NUMBER PREVIOUSLY RECORDED AT REEL: 056111 FRAME: 0583. ASSIGNOR(S) HEREBY CONFIRMS THE ASSIGNMENT. Recorded Feb 25, 2022
From: GARRETT TRANSPORTATION I INC.
To: JPMORGAN CHASE BANK, N.A., AS ADMINISTRATIVE AGENT
Reel/Frame 059250/0792 →
SECURITY AGREEMENT Recorded May 3, 2021
From: GARRETT TRANSPORTATION I INC.
To: JPMORGAN CHASE BANK, N.A., AS ADMINISTRATIVE AGENT
Reel/Frame 056111/0583 →
RELEASE OF SECURITY INTEREST Recorded Apr 30, 2021
From: WILMINGTON SAVINGS FUND SOCIETY, FSB
To: GARRETT TRANSPORTATION I INC.
Reel/Frame 056427/0298 →
ASSIGNMENT AND ASSUMPTION OF SECURITY INTEREST IN PATENTS Recorded Jan 15, 2021
From: JPMORGAN CHASE BANK, N.A., AS RESIGNING ADMINISTRATIVE AND COLLATERAL AGENT
To: WILMINGTON SAVINGS FUND SOCIETY, FSB, AS SUCCESSOR ADMINISTRATIVE AND COLLATERAL AGENT
Reel/Frame 055008/0263 →
SECURITY INTEREST Recorded Oct 1, 2018
From: GARRETT TRANSPORTATION I INC.
To: JPMORGAN CHASE BANK, N.A., AS ADMINISTRATIVE AGENT
Reel/Frame 047172/0220 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 7, 2018
From: HONEYWELL INTERNATIONAL INC.
To: GARRETT TRANSPORATION I INC.
Reel/Frame 046734/0134 →