Adjustable core turbocharger

Patent metadata

Field	Value
Publication number	US-9695822-B2
Application number	US-201414489300-A
Country	US
Kind code	B2
Filing date	Sep 17, 2014
Priority date	Dec 21, 2011
Publication date	Jul 4, 2017
Grant date	Jul 4, 2017

Abstract

A turbocharger is provided herein. The turbocharger includes a housing and an adjustable core at least partially circumferentially surrounded by the housing, the adjustable core having a turbine rotor coupled to a compressor rotor via a shaft. The turbocharger further includes an adjustment mechanism coupled to the adjustable core configured to adjust an axial position of the housing relative to the adjustable core in response to adjustment commands.

First claim

The invention claimed is:

1. A method for a turbocharger comprising:
adjusting an adjustment mechanism of the turbocharger in response to operating conditions of an engine, the turbocharger including a housing and an adjustable core circumferentially surrounded by the housing, the adjustable core axially slideable relative to the housing and including a turbine rotor coupled to a compressor rotor via a shaft, the adjustment mechanism coupled to the adjustable core, the adjustable core sliding the compressor rotor and the turbine rotor concurrently.

2. The method of claim 1 , wherein the housing includes a compressor volute and a turbine scroll, the compressor volute configured to receive air from the compressor rotor and the turbine scroll configured to direct exhaust gas into the turbine rotor, wherein the adjustable core slides the compressor rotor relative to the compressor volute and the turbine rotor relative to the turbine scroll concurrently.

3. The method of claim 2 , further comprising a second turbine scroll configured to direct exhaust gas to the turbine rotor.

4. The method of claim 3 , wherein the first and second turbine scrolls are separated via a divider.

5. The method of claim 4 , wherein the divider includes a coolant passage configured to flow coolant therethrough.

6. The method of claim 1 , wherein the adjustable core includes an adjustment post extending therefrom.

7. The method of claim 6 , wherein the adjustment post is moveably positioned in a track.

8. The method of claim 7 , wherein the track circumferentially extends around the adjustable core and includes a first end axially offset from a second end.

9. The method of claim 1 , wherein the shaft coupling the turbine rotor and the compressor rotor is axially adjustable.

10. A turbocharger comprising:
a housing;
an axially adjustable core circumferentially surrounded by the housing, the core including a turbine rotor coupled to a compressor rotor via a shaft, a compressor flow guide fluidically coupled between a volute and the compressor rotor, and a turbine flow guide fluidically coupled between a first and a second turbine scroll and the turbine rotor; and
a divider separating the first and second turbine scrolls.

11. The turbocharger of claim 10 , wherein the divider includes a coolant passage configured to flow coolant therethrough.

12. The turbocharger of claim 10 , further comprising an adjustment mechanism coupled to the axially adjustable core configured to adjust an axial position of the housing relative to the axially adjustable core in response to adjustment commands.

13. The turbocharger of claim 10 , wherein the first turbine scroll has a different geometry than the second turbine scroll.

14. The turbocharger of claim 10 , wherein the axially adjustable core slides the compressor rotor relative to the volute and the turbine rotor relative to the first and second turbine scrolls concurrently.

15. A turbocharger control method, comprising:
adjusting one or more of compressor outlet flow and turbine inlet flow of a turbocharger via axially sliding a shaft coupling a compressor rotor and a turbine rotor within a fixed housing during turbocharger operation, the turbocharger coupled to an internal combustion engine.

16. The turbocharger control method of claim 15 , wherein adjusting one or more of compressor outlet flow and turbine inlet flow includes decreasing or increasing a flowrate of exhaust gas from a turbine scroll to the turbine rotor.

17. The turbocharger control method of claim 15 , wherein adjusting one or more of compressor outlet flow and turbine inlet flow includes substantially inhibiting flow of exhaust gas from a turbine scroll to the turbine rotor.

18. The turbocharger control method of claim 15 , wherein adjusting one or more of compressor outlet flow and turbine inlet flow is responsive to engine load.

Assignees

• Ford Global Tech Llc

Inventors

• Ervin James Douglas
• Vaught August Thomas

Classifications

• F05D2250/40

  Movement of components · CPC title

• F04D15/0033

  By-passing by increasing clearance between impeller and its casing · CPC title

• F05D2220/40

  in turbochargers · CPC title

• F04D27/002

  by varying geometry within the pumps, e.g. by adjusting vanes · CPC title

• F04D25/024 Primary

  the driving means being assisted by a power recovery turbine · CPC title