Air injection timed with exhaust release

Patent metadata

Field	Value
Publication number	US-9109494-B2
Application number	US-201213368230-A
Country	US
Kind code	B2
Filing date	Feb 7, 2012
Priority date	Feb 7, 2012
Publication date	Aug 18, 2015
Grant date	Aug 18, 2015

Abstract

Embodiments for injecting air into exhaust ports of an engine are provided. In one example, a multi-cylinder engine method comprises combusting a rich air-fuel mixture, injecting air into a first cylinder's exhaust port and not into a second cylinder's exhaust port during the first cylinder's exhaust stroke, and injecting air into the second cylinder's exhaust port and not into the first cylinder's exhaust port during the second cylinder's exhaust stroke. In this way, injection into each exhaust port may be timed with exhaust release into each exhaust port.

First claim

The invention claimed is:

1. A multi-cylinder engine method, comprising:
combusting a rich air-fuel mixture;
rotating a circular disc with a single cut-out opening comprising a circular sector to one or more first positions, the opening in the one or more first positions fluidically connecting a pressurized air supply with a first cylinder's exhaust port and not a second cylinder's exhaust port, and injecting air from the pressurized air supply into the first cylinder's exhaust port and not into the second cylinder's exhaust port during the first cylinder's exhaust stroke; and
rotating the circular disc to one or more second positions, the cut-out opening in the one or more second positions fluidically connecting the pressurized air supply with the second cylinder's exhaust port and not the first cylinder's exhaust port, and injecting air from the pressurized air supply into the second cylinder's exhaust port and not into the first cylinder's exhaust port during the second cylinder's exhaust stroke.

2. The multi-cylinder engine method of claim 1 , wherein injecting air into the first cylinder's exhaust port further comprises not injecting air into exhaust ports of other cylinders that are not undergoing an exhaust stroke, and wherein injecting air into the second cylinder's exhaust port further comprises not injecting air into exhaust ports of other cylinders that are not undergoing an exhaust stroke.

3. The multi-cylinder engine method of claim 1 , wherein injecting air into the first cylinder's exhaust port further comprises injecting air into the first cylinder's exhaust port in response to a temperature of exhaust being below a threshold.

4. The multi-cylinder engine method of claim 1 , wherein the rotating of the circular disc is mechanically timed to the engine's camshaft.

5. The multi-cylinder engine method of claim 4 , further comprising generating the pressurized air supply by operating an air pump.

6. The multi-cylinder engine method of claim 4 , further comprising generating the pressurized air supply by directing air downstream of a turbocharger compressor to an air injection system.

7. The multi-cylinder engine method of claim 1 , wherein injecting air into the first cylinder's exhaust port further comprises blocking air injection into all other cylinders' exhaust ports, wherein the blocking is mechanically timed to the engine's camshaft.

8. The multi-cylinder engine method of claim 1 , wherein injecting air into the second cylinder's exhaust port further comprises blocking air injection into all other cylinders' exhaust ports, wherein the blocking is mechanically timed to the engine's camshaft.

9. A multi-cylinder engine method, comprising:
combusting a rich air-fuel mixture;
rotating a circular disc with a single cut-out opening mechanically timed to the engine's camshaft so that the cut-out opening fluidically connects a pressurized air supply with a first cylinder's exhaust port, and injecting air from the pressurized air supply into the first cylinder's exhaust port only during the first cylinder's exhaust stroke; and
rotating the circular disc mechanically timed to the engine's camshaft so that the cut-out opening fluidically connects the pressurized air supply with a second cylinder's exhaust port, and injecting air from the air supply into the second cylinder's exhaust port only during the second cylinder's exhaust stroke, the cut-out including a leading edge defining an angle at which the fluid connection starts.

10. The method of claim 9 , wherein combusting the rich air-fuel mixture further comprises combusting the rich air-fuel mixture while operating an air pump to generate the pressurized air supply.

11. The method of claim 9 , wherein combusting the rich air-fuel mixture further comprises combusting the rich air-fuel mixture while directing air downstream of a turbocharger compressor to generate the pressurized air supply.

12. The method of claim 9 , wherein injecting air from the pressurized air supply into the first cylinder's exhaust port further comprises injecting air from the pressurized air supply into the first cylinder's exhaust port only during a first half of the first cylinder's exhaust stroke.

13. A system for an engine, comprising:
a first cylinder having a first exhaust port and a second cylinder having a second exhaust port, each exhaust port coupled to an exhaust including an emission control device;
a rotating disc coupled to an engine camshaft, the rotating disc comprising a single cut-out opening, the cut-out opening being a circular sector with a central angle less than 180 degrees; and
an air pump injecting air sequentially to the first and second exhaust ports, the sequential injection from the air pump controlled via the rotating disc.

14. The system of claim 13 , wherein the sequential injection occurs only during rich air/fuel combustion in the engine.

15. The system of claim 13 , wherein the sequential injection occurs in response to a temperature of the emission control device being below a threshold, and wherein the sequential injection occurs only during an exhaust stroke of each respective cylinder.

16. The system of claim 15 , further comprising a third exhaust port coupled to the first cylinder, and wherein air is injected to both the first and third exhaust ports during the exhaust stroke of the first cylinder.

17. The system of claim 13 , wherein the air pump includes a first connection coupled to the first exhaust port and a second connection coupled to the second exhaust port, and wherein the rotating disc rotates to open the first connection during injection to the first exhaust port while blocking the second connection.

18. The system of claim 17 , wherein the rotating disc rotates to open the second connection during injection to the second exhaust port while blocking the first connection.

Assignees

• Sharma Manish
• Surnilla Gopichandra
• Ford Global Tech Llc

Inventors

• Sharma Manish
• Surnilla Gopichandra

Classifications

• F01N3/32 Primary

  using air pump (using jet air pumps F01N3/34; pumps in general F04) · CPC title

• Y02T10/20

  Cross-Sectional Technologies · mapped topic

• F01L2001/0537

  Double overhead camshafts [DOHC] · CPC title

• F01N3/34 Primary

  using air conduits or jet air pumps, e.g. near the engine exhaust port · CPC title

• F01N3/22

  Control of additional air supply only, e.g. using by-passes or variable air pump drives · CPC title