Granted Patent B2

US 10,526,954 · App. 14/820,523 · Granted Jan 7, 2020

Abstract

Claims (25)

1. A turbocharger assembly comprising:

a center housing;

a turbine housing; and

an insert disposed between the center housing and the turbine housing wherein a surface of the turbine housing and a first surface of the insert define a volute and wherein a surface of the center housing and a second surface of the insert define a chamber, wherein the turbine housing comprises a recessed annular surface that seats the insert, wherein the recessed annular surface comprises a radius that exceeds a maximum radius of the volute, wherein the recessed annular surface comprises an insert mating surface that extends radially inwardly to form an end of the volute, wherein the volute is defined in part by a tongue, and wherein the end of the volute is at the tongue.

2. The turbocharger assembly of claim 1 comprising a turbine wheel wherein the insert comprises an inner edge and an outer edge wherein the inner edge defines a radial clearance with respect to an outermost edge of the turbine wheel.

3. The turbocharger assembly of claim 1 wherein the insert comprises an annular ring portion and segments that extend at least in part radially inwardly from the annular ring portion.

4. The turbocharger assembly of claim 1 wherein a load is applied to the insert via contact of the insert with the center housing and via contact of the insert with the turbine housing.

5. The turbocharger assembly of claim 1 wherein the turbine housing comprises a cast turbine housing.

6. The turbocharger assembly of claim 1 wherein the turbine housing comprises a wastegate opening and a wastegate shaft bore.

7. The turbocharger assembly of claim 1 wherein the insert comprises a material of construction that comprises a density that is less than a material of construction of the turbine housing.

8. The turbocharger assembly of claim 1 wherein the insert comprises a thermal conductivity that is less than a thermal conductivity of the turbine housing.

9. The turbocharger assembly of claim 1 wherein the insert comprises a resilient insert.

10. The turbocharger assembly of claim 9 wherein the resilient insert comprises radial channels that form segments.

11. The turbocharger assembly of claim 1 wherein the center housing comprises a turbine side that comprises extensions that comprise axial end surfaces that face the second surface of the insert.

12. The turbocharger assembly of claim 1 wherein the insert is supported at a first radius and supported at a second, different radius.

13. The turbocharger assembly of claim 12 wherein the insert is supported at a third radius intermediate the first radius and the second radius.

14. The turbocharger assembly of claim 1 comprising dowels that contact the turbine housing and that contact the insert.

15. The turbocharger assembly of claim 14 wherein the insert comprises apertures, wherein each of the apertures receives at least a portion of a corresponding one of the dowels.

16. The turbocharger assembly of claim 1 wherein the volute is a scroll that spirals with diminishing cross-sectional flow area for exhaust gas and wherein the scroll ends at the end of the volute.

17. The turbocharger assembly of claim 1 wherein the turbine housing is a unitary cast turbine housing and wherein the insert is a unitary component.

18. The turbocharger assembly of claim 17 wherein the volute is defined exclusively by two pieces, which are the turbine housing and the insert.

19. A turbocharger assembly comprising:

a center housing;

a turbine housing; and

an insert disposed between the center housing and the turbine housing wherein a surface of the turbine housing and a first surface of the insert define a volute and wherein a surface of the center housing and a second surface of the insert define a chamber, wherein the turbine housing comprises a recessed annular surface that seats the insert, wherein the recessed annular surface comprises a radius that exceeds a maximum radius of the volute, wherein the recessed annular surface comprises an insert mating surface that extends radially inwardly to form an end of the volute, wherein the turbine housing is a unitary cast turbine housing, wherein the insert is a unitary component, and wherein the volute is defined exclusively by two pieces, which are the turbine housing and the insert.

Assignments (8)