Compressor bypass turbine-generator

• US 9,163,555 B2
• Filed: 12/06/2012
• Issued: 10/20/2015
• Est. Priority Date: 12/06/2012
• Status: Active Grant

• Current Assignee: Ford Global Technologies, LLC (Ford Motor Company)
• Original Assignee: Ford Global Technologies, LLC (Ford Motor Company)
• Inventors: McConville, Gregory Patrick, Maceroni, Karen Elizabeth
• Primary Examiner(s): Trieu, Thai Ba
• Assistant Examiner(s): Isada, Paolo
• Application Number:
  US13/707,443
• Publication Number:
  US 20140157774A1
• Time in Patent Office: 1,048 Days
• Field of Search: 606/11, 603/27, 604/59
• US Class Current: 1/1
• CPC Class Codes: F02B 37/164 the bypassed air being used in an auxiliary apparatus, e.g. in an air turbine
• CPC Class Codes: Y02T 10/12 Improving ICE efficiencies

Abstract

Embodiments for a turbine-generator position in a compressor bypass flow path are presented. In one example, a method for an engine having a compressor comprises generating energy via a turbine-generator positioned in a bypass flow path of the compressor. In this way, the energy of the recirculated intake air may be recovered by the turbine-generator.

Claims

1. A method of controlling air of an engine having a compressor, comprising:

generating energy by directing at least a portion of compressed intake air through a turbine of a turbine-generator by closing a compressor bypass valve to block recirculation of the compressed intake air,

wherein the compressor bypass valve arranged in a compressor bypass passage is in a first position, the turbine positioned in a turbine passage, and the turbine passage coupled to the compressor bypass passage;

recirculating at least a portion of compressed intake air from an outlet of the compressor to an inlet of the compressor without passing through the turbine of the turbine-generator by opening the compressor bypass valve to a second position.

2. The method of claim 1, wherein the compressor bypass valve is positioned over an intersection of the compressor bypass passage and the turbine passage.

3. The method of claim 1, further comprising adjusting the compressor bypass valve based on a ratio of a compressor pressure ratio to a mass air flow.

4. A method of controlling air of an engine having a compressor, comprising:

directing intake air through a compressor and to the engine;

when a ratio of a compressor pressure ratio to a mass air flow is above a first threshold and below a second threshold, recirculating at least a portion of the intake air from downstream of the compressor to upstream of the compressor via a turbine of a turbine-generator, by closing the compressor bypass valve, wherein the turbine is positioned in a turbine passage coupled to a compressor bypass passage; and

when the ratio is above the second threshold, recirculating at least a portion of the intake air from downstream of the compressor to upstream of the compressor without passing through the turbine of the turbine-generator by opening the compressor bypass valve.

5. The method of claim 4, wherein recirculating at least a portion of the intake air from downstream of the compressor to upstream of the compressor without passing through the turbine-generator further comprises opening the compressor bypass valve to a second position in which the compressor bypass valve is fully open.

6. A system comprising:

a compressor bypass passage configured to recirculate compressed intake air from an outlet of a turbocharger compressor to an inlet of the turbocharger compressor;

a turbine positioned in a turbine passage coupled to the compressor bypass passage;

a compressor bypass valve positioned over an intersection of the compressor bypass passage and the turbine passage; and

an energy conversion device coupled to the turbine.

7. The system of claim 6, further comprising a controller configured to adjust the valve to a first position to direct at least a portion of the recirculated compressed intake air through the turbine passage and to the inlet of the compressor.

8. The system of claim 7, wherein the controller is configured to adjust the valve to a second position to direct the recirculated compressed intake air through the compressor bypass passage and block at least a portion of the recirculated compressed intake air from reaching the turbine.

9. The system of claim 8, wherein the valve is a throttle-type vavle.

10. The system of claim 8, wherein the valve is a three-way vavle.

11. The system of claim 10, wherein in the first position of the valve, all of the recirculated compressed intake air is routed through the turbine, and wherein in the second position of the valve, all of the recirculated compressed intake air is routed through the compressor bypass passage and blocked from reaching the turbine.

12. The system of claim 9, wherein in the first position of the valve, an edge of the valve interfaces with a far edge of the turbine passage where it intersects the compressor bypass passage.

13. The system of claim 12, wherein in the second position of the valve, the edge of the valve is positioned past the interface with the turbine passage and the valve is fully open.

14. The system of claim 7, wherein the controller is configured to close the valve to block recirculation of the compressed intake air and direct the compressed intake air to the engine.

15. The system of claim 7, wherein the controller is configured to adjust the valve based on a pressure ratio and a mass flow rate of the compressor.

16. The system of claim 6, wherein the turbine is a first turbine, and further comprising a second turbine positioned in an exhaust path of the engine and coupled to the compressor via a shaft.

17. The system of claim 6, wherein the energy conversion device is coupled to a battery.