Dynamic seal for fuel injector needle check

Patent metadata

Field	Value
Publication number	US-9995261-B2
Application number	US-201514689307-A
Country	US
Kind code	B2
Filing date	Apr 17, 2015
Priority date	Apr 17, 2015
Publication date	Jun 12, 2018
Grant date	Jun 12, 2018

Abstract

A fuel injector includes an injector body defining a liquid fuel passage, a gaseous fuel passage, and a first guide bore; a gaseous fuel check guided within the first guide bore between a retracted position and an advanced position to selectively open and block, respectively, fluid communication between the gaseous fuel passage and a gaseous fuel nozzle outlet; and a sleeve seal seated within the first guide bore, the sleeve seal having an inner surface defining a sleeve seal bore therethrough, and at least a portion of the gaseous fuel check is disposed within the sleeve seal bore; an outer surface of the sleeve seal including a first portion and a second portion, the first portion being disposed closer to a longitudinal axis of the sleeve seal bore along a radial direction than the second portion.

First claim

I claim:

1. A fuel injector for an internal combustion engine, the fuel injector comprising:
an injector body defining a liquid fuel passage extending between a liquid fuel inlet and a liquid fuel outlet, a gaseous fuel passage extending between a gaseous fuel inlet and a gaseous fuel nozzle outlet, and a first guide bore;
a gaseous fuel check guided within the first guide bore between a retracted position and an advanced position to selectively open and block, respectively, fluid communication between the gaseous fuel passage and the gaseous fuel nozzle outlet; and
a sleeve seal seated within the first guide bore, the sleeve seal having an inner surface defining a sleeve seal bore therethrough, and at least a portion of the gaseous fuel check is disposed within the sleeve seal bore,
an outer surface of the sleeve seal including a first portion and a second portion, the first portion being disposed closer to a longitudinal axis of the sleeve seal bore along a radial direction than the second portion, the radial direction being perpendicular to the longitudinal axis, wherein the outer surface of the sleeve seal defines a plurality of grooves and a plurality of lands, each groove of the plurality of grooves being defined between adjacent lands of the plurality of lands, the plurality of grooves including the first portion of the sleeve seal, and the plurality of lands including the second portion of the sleeve seal, and wherein fluid pressure from the liquid fuel inlet applies at least a radially inward pressure on the plurality of grooves to increase sealing contact between the sleeve seal bore and an outer surface of the gaseous fuel check,
the first portion of the outer surface of the sleeve seal being in fluid communication with the liquid fuel passage,
a distal portion of the gaseous fuel check extending along the longitudinal axis on a first side of the sleeve seal, and being in fluid communication with the gaseous fuel inlet, and
a proximal portion of the gaseous fuel check extending along the longitudinal axis on a second side of the sleeve seal, opposite of the first side of the sleeve seal, and being in fluid communication with the liquid fuel inlet.

2. The fuel injector of claim 1 , wherein the second portion of the outer surface of the sleeve seal bears upon the first guide bore.

3. The fuel injector of claim 1 , wherein the plurality of grooves extend at least partly in a longitudinal direction from a proximal end of the sleeve seal toward a distal end of the sleeve seal, the longitudinal direction being parallel to the longitudinal axis of the sleeve seal.

4. The fuel injector of claim 1 , wherein the plurality of grooves are evenly distributed circumferentially about the outer surface of the sleeve seal.

5. The fuel injector of claim 1 , wherein a radial depth between one land of the plurality of lands and an adjacent groove of the plurality of grooves is between 20 to 40 micrometers.

6. The fuel injector of claim 1 , wherein the first guide bore of the injector body includes a first section, a second section, and a seat portion located between the first section and the second section, and
wherein the first section has a diameter that is larger than a diameter of the second section.

7. The fuel injector of claim 1 , wherein the sleeve seal includes at least one material selected from the group consisting of a 50100 alloy steel, a 52100 alloy steel, and a high density polyethylene.

8. The fuel injector of claim 1 , wherein the injector body defines a second guide bore therein, and the liquid fuel outlet includes a liquid fuel nozzle outlet,
the fuel injector further comprising a liquid fuel check guided within the second guide bore between retracted and advanced positions to selectively open and block, respectively, fluid communication between the liquid fuel passage and the liquid fuel nozzle outlet.

9. The fuel injector of claim 8 , wherein the injector body further includes a tip piece defining the first guide bore and the second guide bore receiving the gaseous fuel check and the liquid fuel check, respectively, the tip piece having the liquid fuel nozzle outlet and the gaseous fuel nozzle outlet formed thereon.

10. A dual fuel system for an internal combustion engine, the dual fuel system comprising:
a liquid fuel supply;
a gaseous fuel supply; and
a plurality of fuel injectors for supplying liquid fuel from the liquid fuel supply and supplying gaseous fuel from the gaseous fuel supply into cylinders of the internal combustion engine, each fuel injector of the plurality of fuel injectors comprising
an injector body defining a liquid fuel passage extending between a liquid fuel inlet and a liquid fuel outlet, a gaseous fuel passage extending between a gaseous fuel inlet and a gaseous fuel nozzle outlet, and a first guide bore,
a gaseous fuel check guided within the first guide bore between a retracted position and an advanced position to selectively open and block, respectively, fluid communication between the gaseous fuel passage and the gaseous fuel nozzle outlet, and
a sleeve seal seated within the first guide bore, the sleeve seal having an inner surface defining a sleeve seal bore therethrough, and at least a portion of the gaseous fuel check is disposed within the sleeve seal bore,
an outer surface of the sleeve seal including a first portion and a second portion, the first portion being disposed closer to a longitudinal axis of the sleeve seal bore along a radial direction than the second portion, the radial direction being perpendicular to the longitudinal axis, wherein the outer surface of the sleeve seal defines a plurality of grooves and a plurality of lands, each groove of the plurality of grooves being defined between adjacent lands of the plurality of lands, the plurality of grooves including the first portion of the sleeve seal, and the plurality of lands including the second portion of the sleeve seal, and wherein fluid pressure from the liquid fuel inlet applies at least a radially inward pressure on the plurality of grooves to increase sealing contact between the sleeve seal bore and an outer surface of the gaseous fuel check,
the first portion of the outer surface of the sleeve seal being in fluid communication with the liquid fuel passage,
a distal portion of the gaseous fuel check extending along the longitudinal axis on a first side of the sleeve seal, and being in fluid communication with the gaseous fuel inlet, and
a proximal portion of the gaseous fuel check extending along the longitudinal axis on a second side of the sleeve seal, opposite of the first side of the sleeve seal, and being in fluid communication with the liquid fuel passage.

11. The dual fuel system of claim 10 , wherein the second portion of the outer surface of the sleeve seal bears upon the first guide bore.

12. The dual fuel system of claim 10 , wherein the plurality of grooves extend at least partly in a longitudinal direction from a proximal end of the sleeve seal toward a distal end of the sleeve seal, the longitudinal direction being parallel to the longitudinal axis of the sleeve seal.

13. The dual fuel system of claim 10 , wherein the plurality of grooves are evenly distributed circumferentially about the outer surface of the sleeve seal.

14. The dual fuel system of claim 10 , wherein a radial depth between one land of the plurality of lands and an adjacent groove of the plurality of grooves is between 20 to 40 micrometers.

15. The dual fuel system of claim 10 , wherein the first guide bore of the injector body includes a first section, a second section, and a seat portion between the firs

Assignees

• Caterpillar Inc

Inventors

• Kim Hoisan

Classifications

• F02M61/10

  Other injectors with elongated valve bodies, i.e. of needle-valve type · CPC title

• F02M21/0251

  Details of actuators therefor · CPC title

• F02M2200/16

  Sealing of fuel injection apparatus not otherwise provided for · CPC title

• F02M47/027

  Electrically actuated valves draining the chamber to release the closing pressure · CPC title

• F02D19/10

  peculiar to compression-ignition engines in which the main fuel is gaseous · CPC title