IP Library Granted Patent US 7,472,844
Granted Patent B2
US 7,472,844 · App. 11/313,415 · Granted Jan 6, 2009

Fuel injector nozzle with tip alignment apparatus

Assignee: Caterpillar Inc.
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Quick Facts
Patent No.
US 7,472,844
App. No.
11/313,415
Granted
Jan 6, 2009
Kind
B2
Abstract

A fuel injector nozzle assembly is disclosed. The assembly may include a nozzle casing, a first tip member, and a second tip member. The first tip member may extend longitudinally within the nozzle casing and may define first and second shoulders on the first tip member. The second tip member may extend longitudinally within the nozzle casing and may be arranged in predetermined rotational alignment with the first tip member. The second tip member may define a third shoulder on the second tip member configured to interact with the first shoulder to oppose rotation of the first tip member relative the second tip member in a first direction about a longitudinal axis of the first tip member. The second tip member may further define a fourth shoulder on the second tip member configured to interact with the second shoulder to oppose rotation of the first tip member relative the second tip member in a second direction about a longitudinal axis of the first tip member.

Claims (64)

1. A fuel injector nozzle assembly, comprising:

a nozzle casing;

a first tip member extending longitudinally within the nozzle casing and defining first and second shoulders on the first tip member and also defining a plurality of injection holes; and

a second tip member extending longitudinally within the nozzle casing and being arranged in predetermined rotational alignment with the first tip member, the second tip member defining: (i) a third shoulder on the second tip member configured to interact with the first shoulder to oppose rotation of the first tip member relative the second tip member in a first direction about a longitudinal axis of the first tip member; and (ii) a fourth shoulder on the second tip member configured to interact with the second shoulder to oppose rotation of the first tip member relative the second tip member in a second direction about a longitudinal axis of the first tip member.

2. The assembly of claim 1 , wherein:

the first tip member defines an annular wall at a longitudinal end portion of the first tip member; and

the first and second shoulders are defined by the wall.

3. The assembly of claim 2 , wherein:

the annular wall includes a first wall portion having a first outer radius and a second wall portion having a second outer radius, at least one of the first and second shoulders being arranged at a position on the annular wall having an outer radius less than the first outer radius and greater than the second outer radius.

4. The assembly of claim 2 , wherein the annular wall extends longitudinally away from a section of the first tip member having a greater outer diameter than the wall.

5. The assembly of claim 1 , wherein:

the second tip member defines a curved wall at a longitudinal end portion of the second tip member; and

the third and fourth shoulders are defined by the wall.

6. The assembly of claim 5 , wherein the curved wall extends greater than 180 degrees around a longitudinal axis of the second tip member.

7. The assembly of claim 5 , wherein the curved wall extends less than or equal to 180 degrees around a longitudinal axis of the second tip member.

8. The assembly of claim 7 , wherein the curved wall extends greater than or equal to 5 degrees around a longitudinal axis of the second tip member.

9. The assembly of claim 5 , wherein the curved wall forms a counterbore at the longitudinal end portion of the second tip member.

10. The assembly of claim 1 , wherein:

the first tip member has a first bore therein;

the second tip member has a second bore therein; and

the assembly includes a valve member slidably arranged within the first and second bores.

11. The assembly of claim 1 , wherein:

the first tip member has a first bore therein;

the second tip member has a second bore therein, the second bore being arranged in fluid communication with the first bore; and

the first and second tip members are disposed and arranged in abutment to provide a substantially sealed fluid path between the first and second bores.

12. The assembly of claim 11 , wherein:

abutting ends of the first and second bores have substantially the same diameter and are joined to form a substantially continuous channel.

13. The assembly of claim 1 , wherein:

the nozzle casing has an internal wall;

the first tip member has a first outer surface in abutting engagement with the internal wall of the nozzle casing; and the second tip member has a second outer surface in abutting engagement with the internal wall of the nozzle casing.

14. The assembly of claim 1 , wherein:

the first and second tip members are arranged in longitudinal alignment within the nozzle casing; and

the nozzle casing interacts with outer surfaces of the first and second tip members to at least inhibit longitudinal disalignment of the first and second tip members with respect to each other.

15. The assembly of claim 14 , wherein:

the first tip member has a first generally cylindrical outer surface with a first diameter, the first generally cylindrical outer surface engaging an inner wall of the nozzle casing; and

the second tip member has a second generally cylindrical outer surface with a second diameter substantially the same as the first diameter, the second generally cylindrical outer surface engaging an inner wall of the nozzle casing.

16. The assembly of claim 1 , wherein:

the nozzle casing has a nozzle aperture therein; and

the first tip member extends out of the nozzle casing through the nozzle aperture.

17. The assembly of claim 1 , wherein:

the first and second shoulders extend longitudinally at least 3 mm.

18. The assembly of claim 17 , wherein: the third and fourth shoulders extend longitudinally at least 3 mm.

19. The assembly of claim 18 , wherein:

the first and second shoulders overlap longitudinally with the third and fourth shoulders, respectively, for lengths greater than or equal to 3 mm.

20. The assembly of claim 1 , wherein:

the first tip member defines: (i) a first, generally cylindrical portion having an outer diameter and (ii) a second portion extending longitudinally away from the first portion and having a reduced outer diameter relative the outer diameter of the first portion; and

the second tip member defines a wall extending longitudinally on the second tip member and at least partially surrounding the second portion of the first tip member; the first and second shoulders are formed on the second portion of the first tip member; and the third and fourth shoulders are formed on the wall of the second tip member.

21. The assembly of claim 1 , wherein:

the first tip member includes a first annular portion with a first locating surface thereon and defining the first and second shoulders; and

the second tip member includes a second annular portion with a second locating surface thereon and defining the third and fourth shoulders, the second locating surface interacting with the first locating surface to facilitate longitudinal alignment of the first and second tip members.

22. The assembly of claim 21 , wherein:

the first annular portion includes an annular wall at least partially surrounding a longitudinal axis of the first tip member; and

the second annular portion includes an annular wall at least partially surrounding a longitudinal axis of the second tip member.

23. A fuel injector nozzle assembly, comprising:

a nozzle casing;

a first tip member extending longitudinally within the nozzle casing and defining first and second shoulders on the first tip member; and

a second tip member extending longitudinally within the nozzle casing and being arranged in predetermined rotational alignment with the first tip member, the second tip member defining: (i) a third shoulder on the second tip member configured to interact with the first shoulder to oppose rotation of the first tip member relative the second tip member in a first direction about a longitudinal axis of the first tip member; and (ii) a fourth shoulder on the second tip member configured to interact with the second shoulder to oppose rotation of the first tip member relative the second tip member in a second direction about a longitudinal axis of the first tip member;

the first tip member has one or more injection holes formed therein; and

the injection holes are arranged on the first tip member in a predetermined orientation relative the first and second shoulders.

24. The assembly of claim 1 , wherein at least one of the first and second shoulders has a curved cross-section.

25. A method of assembling a fuel injector nozzle assembly, including the steps of:

arranging a plurality of injections holes defined in a first tip member in a predetermined orientation relative to first and second shoulders of the first tip member;

aligning a second tip member relative to the first tip member to inhibit rotation between the first tip member and the second tip member via an interaction between the first and second shoulders of the first tip member and first and second shoulders of the second tip member.

26. The method of assembling a fuel injector nozzle assembly of claim 25 , further including a step of aligning the second tip member relative to a nozzle casing such that the plurality of injection holes defined in the first tip member have a predetermined orientation relative to the nozzle casing.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 14, 2006
From: MANUBOLU, AVINASH R.; SANDHU, AVTAR S.; GREER, CHRISTOPHER A.; GARIMIDI, VENU G.
To: CATERPILLAR INC.
Reel/Frame 017661/0007 →
Continuity (1)
Related Publication 20070145163A1 · Jun 28, 2007