Fuel injector assembly having duct structure

Patent metadata

Field	Value
Publication number	US-10711752-B2
Application number	US-201715692408-A
Country	US
Kind code	B2
Filing date	Aug 31, 2017
Priority date	Aug 31, 2017
Publication date	Jul 14, 2020
Grant date	Jul 14, 2020

Abstract

A fuel injector assembly for an engine. The engine includes a cylinder head defining a through-hole. The fuel injector assembly includes an insert, having a first end and a second end, configured to be received within the through-hole and coupled to the cylinder head. The insert defines a bore extending from the first end to the second end. The fuel injector assembly further includes a fuel injector including a plurality of orifices, received within the bore of the insert; and a duct structure including a plurality of ducts, coupled to the insert such that the plurality of ducts align with the plurality of orifices to at least partially receive one or more fuel jets from the plurality of orifices of the fuel injector.

First claim

What is claimed is:

1. A fuel injector assembly for an engine, the engine including a cylinder head defining a through-hole, the fuel injector assembly comprising:
an insert, having a first end and a second end, configured to be received within the through-hole and coupled to the cylinder head, the insert defining a bore extending from the first end to the second end;
a fuel injector including a plurality of orifices at a distal end portion of the fuel injector, the fuel injector being received within the bore of the insert and having a groove provided at the distal end portion; and
a duct structure including a plurality of ducts, the duct structure being coupled to the insert such that the plurality of ducts align with the plurality of orifices to at least partially receive one or more fuel jets from the plurality of orifices of the fuel injector, a length of the groove with respect to a longitudinal axis of the fuel injector being defined such that the groove is configured to axially position the plurality of orifices of the fuel injector in alignment relative to the plurality of ducts, the duct structure being fastened to the first end of the insert, and an outer surface of the insert extends radially outward of the duct structure and is press-fit into the cylinder head.

2. The fuel injector assembly of claim 1 wherein the duct structure is coupled to the first end of the insert such that each duct of the plurality of ducts is axially spaced from the insert.

3. The fuel injector assembly of claim 1 wherein,
the insert defines a protuberance; and
the fuel injector includes a grooved region in which the groove is provided, the groove being configured to abut the protuberance to rotationally align the fuel injector relative to the duct structure.

4. The fuel injector assembly of claim 1 wherein the second end of the insert includes a flanged region, the flanged region configured to abut the cylinder head to restrict axial movement of the insert relative to the cylinder head.

5. The fuel injector assembly of claim 1 wherein each duct of the plurality of ducts is a tubular structure.

6. An engine comprising:
a piston;
a cylinder block defining a piston bore, the piston bore configured to receive the piston;
a cylinder head coupled to the cylinder block, the cylinder head defining a through-hole;
a combustion chamber being defined by the piston, the cylinder block and the cylinder head;
a fuel injector assembly received within the through-hole of the cylinder head, the fuel injector assembly comprising:
an insert, having a first end and a second end, received within the through-hole and coupled to the cylinder head, the insert defining a bore;
a duct structure, including a plurality of ducts, coupled to the insert such that the plurality of ducts extends into the combustion chamber, the duct structure being fastened to the first end of the insert, and an outer surface of the insert extends radially outward of the duct structure and is press-fit into the cylinder head; and
a fuel injector, including a plurality of orifices at a distal end portion of the fuel injector, the fuel injector having a groove at the distal end portion with a length defined with respect to a longitudinal axis of the fuel injector such that the groove is configured to position the plurality of orifices of the fuel injector in alignment with the plurality of ducts, the fuel injector being received within the bore such that the plurality of orifices align with the plurality of ducts to inject one or more fuel jets at least partially into the plurality of ducts, wherein the bore is defined by an inner surface of the insert that contacts the fuel injector at a proximal portion of the insert and has a diameter that increases in a direction opposite to an insertion direction of the fuel injector into the bore.

7. The engine of claim 6 wherein each duct of the plurality of ducts is a tubular structure.

8. The engine of claim 6 wherein, the insert and the duct structure is an integral structure fabricated by using one of additive manufacturing and casting.

9. The engine of claim 6 wherein,
the insert and the cylinder head define a first annular passage configured to carry a coolant fluid therein;
the duct structure defines:
a first passage fluidly coupled to the first annular passage, the first passage is configured to circulate the coolant fluid to each of the plurality of ducts, the coolant fluid configured to absorb heat from each duct; and
a second passage facilitating exit of the heated coolant fluid from the duct structure; and

the insert and the cylinder head define a second annular passage configured to receive the heated coolant fluid from the second passage.

10. The engine of claim 6 wherein the first end of the insert is fastened to the duct structure such that each duct of the plurality of ducts is axially spaced from the first end of the insert.

11. The engine of claim 10 wherein the second end of the insert includes a flanged region abutting the cylinder head.

12. The engine of claim 6 wherein the duct structure is coupled to the insert such that each duct is inclined relative to the longitudinal axis of the fuel injector to align the plurality of ducts with the plurality of orifices of the fuel injector.

13. The engine of claim 6 wherein,
the insert includes a protuberance; and
the fuel injector includes a grooved region in which the groove is provided, the groove being configured to abut the protuberance to rotationally align the fuel injector relative to the duct structure.

14. A method for installing a duct structure and a fuel injector in an engine, the engine comprising a cylinder block, a cylinder head and a piston defining a combustion chamber, the method comprising:
coupling the duct structure, including a plurality of ducts, with an insert;
placing the insert within a through-hole of the cylinder head such that the duct structure extends into the combustion chamber;
receiving the fuel injector, including a plurality of orifices and a groove at a distal end portion of the fuel injector, within a bore defined by the insert that has a diameter that increases in a direction opposite to an insertion direction of the fuel injector,
axially aligning the plurality of orifices with the plurality of ducts with the groove in the distal end portion of the fuel injector; and
rotationally aligning the plurality of orifices with the plurality of ducts with the groove provided in the distal end portion of the fuel injector to inject one or more fuel jets at least partially into the plurality of ducts.

15. The method of claim 14 further including coupling the insert with the cylinder head by one of press-fitting the insert into the through-hole or threadably coupling the insert with the cylinder head.

16. The method of claim 14 wherein the duct structure is coupled to a first end of the insert such that each duct of the plurality of ducts is axially spaced from the insert.

17. The method of claim 14 wherein coupling the duct structure with the insert includes using one of bolts, a brazing process, or a welding process.

18. The fuel injector assembly of claim 1 wherein the bore is defined by an inner surface of the insert that contacts the fuel injector at a proximal portion of the insert and has a diameter that increases in a direction opposite to an insertion direction of the fuel injector into the bore.

19. The fuel injector assembly of claim 1 wherein the groove is provided partially between the first end and the second e

Assignees

• Caterpillar Inc

Inventors

• Martin Glen Clifford
• Koci Chad Palmer
• Svensson Kenth I
• Qi Yongli
• Wiebrecht Eric Donald

Classifications

• F02M53/043

  with cooling means other than air cooling · CPC title

• F02B23/0651 Primary

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

• Y02T10/12

  Improving ICE efficiencies · CPC title

• F02B23/00

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

• F02M2200/852

  provisions for mounting the fuel injection apparatus in a certain orientation, e.g. markings or notches · CPC title