Ducted combustion system for an internal combustion engine

Patent metadata

Field	Value
Publication number	US-10151235-B2
Application number	US-201715451823-A
Country	US
Kind code	B2
Filing date	Mar 7, 2017
Priority date	Mar 7, 2017
Publication date	Dec 11, 2018
Grant date	Dec 11, 2018

Abstract

A ducted combustion system for an internal combustion engine includes a combustion chamber, a fuel injector, and a plurality of ducts. The combustion chamber is defined between a flame deck surface of a cylinder head and a piston crown of a piston disposed within a cylinder bore. Further, the fuel injector is configured to inject fuel into the combustion chamber as a plurality of fuel jets. The plurality of ducts is disposed within the combustion chamber between the flame deck surface and the piston crown. The plurality of ducts is disposed such that each of the plurality of fuel jets at least partially enters one of the plurality of ducts. The at least one of the plurality of ducts is configured to move to vary an angle of a corresponding at least one of the plurality of fuel jets relative to a longitudinal axis of the fuel injector.

First claim

What is claimed is:

1. A ducted combustion system for an internal combustion engine, the ducted combustion system comprising:
a combustion chamber defined between a flame deck surface of a cylinder head of the internal combustion engine and a piston crown of a piston disposed within a cylinder bore of the internal combustion engine;
a fuel injector configured to inject fuel into the combustion chamber as a plurality of fuel jets; and
a plurality of ducts disposed within the combustion chamber between the flame deck surface and the piston crown, the plurality of ducts being disposed such that each of the plurality of fuel jets at least partially enters one of the plurality of ducts, at least one of the plurality of ducts being configured to move to vary an angle of a corresponding at least one of the plurality of fuel jets relative to a longitudinal axis of the fuel injector.

2. The ducted combustion system of claim 1 further including at least one actuator to move the at least one of the plurality of ducts.

3. The ducted combustion system of claim 1 further including a support structure to support each of the plurality of ducts in the combustion chamber, each duct being defined by a tubular structure pivotably coupled to the support structure about a pivot axis.

4. The ducted combustion system of claim 3 further including at least one actuator configured to rotate each duct about the pivot axis.

5. The ducted combustion system of claim 4 , wherein each duct includes a first end pivotably coupled to the support structure, and a second end coupled to the at least one actuator.

6. The ducted combustion system of claim 1 , wherein the plurality of ducts includes a first set of ducts and a second set of ducts, wherein each of the first set of ducts defines a first axis and each of the second set of ducts defines a second axis, an angle of the first axis relative to the longitudinal axis of the fuel injector being different from an angle of the second axis relative to the longitudinal axis of the fuel injector.

7. The ducted combustion system of claim 6 , wherein the plurality of ducts is defined by a plurality of passages formed in a frusto-conical disc structure.

8. The ducted combustion system of claim 6 , wherein each of the plurality of ducts is defined by a tubular structure.

9. The ducted combustion system of claim 6 , wherein the fuel injector includes a plurality of orifices to discharge the plurality of fuel jets, the plurality of ducts being configured to rotate about the longitudinal axis of the fuel injector, wherein the plurality of ducts is rotated to align either the first set of ducts or the second set of ducts with the plurality of orifices.

10. An internal combustion engine, comprising:
a combustion chamber defined between a flame deck surface of a cylinder head of the internal combustion engine and a piston crown of a piston disposed within a cylinder bore of the internal combustion engine;
a fuel injector configured to inject fuel into the combustion chamber as a plurality of fuel jets;
a plurality of ducts disposed within the combustion chamber between the flame deck surface and the piston crown, the plurality of ducts being disposed such that each of the plurality of fuel jets at least partially enters one of the plurality of ducts; and
at least one actuator configured to selectively move at least one of the plurality of ducts to vary an angle of a corresponding at least one of the plurality of fuel jets relative to a longitudinal axis of the fuel injector.

11. The internal combustion engine of claim 10 further including a support structure to support each of the plurality of ducts in the combustion chamber, each duct being defined by a tubular structure pivotably coupled to the support structure about a pivot axis.

12. The internal combustion engine of claim 11 , wherein the at least one actuator is configured to move each duct about the pivot axis.

13. The internal combustion engine of claim 12 , wherein each duct includes a first end pivotably coupled to the support structure, and a second end coupled to the at least one actuator.

14. The internal combustion engine of claim 13 , wherein the at least one actuator includes a spring actuator, the spring actuator configured to pivot the corresponding duct about the pivot axis based on a fuel flow force acting on the corresponding duct.

15. The internal combustion engine of claim 10 , wherein the plurality of ducts includes a first set of ducts and a second set of ducts, wherein each of the first set of ducts defines a first axis and each of the second set of ducts defines a second axis, an angle of the first axis relative to the longitudinal axis of the fuel injector being different from an angle of the second axis relative to the longitudinal axis of the fuel injector.

16. The internal combustion engine of claim 15 , wherein the plurality of ducts is defined by a plurality of passages formed in a frusto-conical disc structure.

17. The internal combustion engine of claim 15 , wherein the fuel injector includes a plurality of orifices to discharge the plurality of fuel jets, the plurality of ducts being configured to rotate about the longitudinal axis of the fuel injector, wherein the plurality of ducts is rotated to align either the first set of ducts or the second set of ducts with the plurality of orifices.

18. A method for operating a ducted combustion system, comprising:
injecting a plurality of fuel jets from a fuel injector into a combustion chamber;
directing each of the plurality of fuel jets into a corresponding one of a plurality of ducts disposed within the combustion chamber; and
selectively moving at least one of the plurality of ducts to adjust an angle of a corresponding at least one of the plurality of fuel jets relative to a longitudinal axis of the fuel injector.

19. The method of claim 18 , wherein moving the at least one of the plurality of ducts includes moving at least one of the plurality of ducts about a pivot axis of each corresponding duct, wherein the pivot axis of each duct is defined by a pivotable connection of each duct with a support structure.

20. The method of claim 18 , wherein moving the at least one of the plurality of ducts includes moving at least one of the plurality of ducts about the longitudinal axis of the fuel injector to align one of a first set of ducts or a second set of ducts with the plurality of fuel jets, wherein each of the first set of ducts defines a first axis and each of the second set of ducts defines a second axis, an angle of the first axis relative to the longitudinal axis of the fuel injector being different from an angle of the second axis relative to the longitudinal axis of the fuel injector.

Assignees

• Caterpillar Inc

Inventors

• Anders Jonathan W
• Svensson Kenth I

Classifications

• F02B23/0651

  the fuel spray impinging on reflecting surfaces or being specially guided throughout the combustion space · CPC title

• F02M61/182

  Discharge orifices being situated in different transversal planes with respect to valve member direction of movement · CPC title

• F02M61/1813

  Discharge orifices having different orientations with respect to valve member direction of movement, e.g. orientations being such that fuel jets emerging from discharge orifices collide with each other · CPC title

• F02B23/00 Primary

  Other engines characterised by special shape or construction of combustion chambers to improve operation (engines with incandescent chambers F02B9/08) · CPC title

• F02F3/28

  Other pistons with specially-shaped head · CPC title