Fuel injector for common rail

Patent metadata

Field	Value
Publication number	US-10077748-B2
Application number	US-201414580820-A
Country	US
Kind code	B2
Filing date	Dec 23, 2014
Priority date	Dec 23, 2014
Publication date	Sep 18, 2018
Grant date	Sep 18, 2018

Abstract

A fuel injector, comprising an injector body having a longitudinal axis, an injector cavity, an injector orifice at a distal end of the injector cavity, and an inlet conduit configured to supply fuel into the injector cavity, a nozzle valve in the injector cavity, a drain circuit configured to drain fuel from the injector cavity to a low pressure drain, a pilot valve in flow communication with the drain circuit, a chamber housing having an inlet passage to receive fuel from the injector cavity, a return port in flow communication with the pilot valve to drain fuel to the drain circuit, and an abutting surface surrounding the return port, and a control body slidably disposed in the chamber housing, the control body having, a distal end, a proximal end, and a longitudinal axis parallel with the injector body longitudinal axis, a first depression at the distal end defining a first control chamber in which one end of the nozzle valve is guided, a second depression at the proximal end defining a second control chamber in flow communication with the return port, and an annular seal disposed radially of the second depression having a first diameter at an inner surface and a second diameter at an outer surface, wherein the first diameter is smaller than the second diameter.

First claim

The invention claimed is:

1. A fuel injector, comprising:
an injector body having a longitudinal axis, an injector cavity, an injector orifice at a distal end of the injector cavity, and an inlet conduit configured to supply fuel into the injector cavity;
a nozzle valve in the injector cavity;
a drain circuit configured to drain fuel from the injector cavity to a low pressure drain;
a pilot valve in flow communication with the drain circuit;
a chamber housing having an inlet passage to receive fuel from the injector cavity, a return port in flow communication with the pilot valve to drain fuel to the drain circuit, and an abutting surface surrounding the return port; and
a control body slidably disposed in the chamber housing, the control body having,
a distal end, a proximal end, and a longitudinal axis parallel with the injector body longitudinal axis,
a first depression at the distal end of the control body defining a first control chamber in which one end of the nozzle valve is guided,
a second depression at the proximal end of the control body defining a second control chamber in flow communication with the return port, and
an annular seal disposed radially of the second depression having a first diameter at an inner surface and a second diameter at an outer surface, wherein the first diameter is smaller than the second diameter, wherein the annular seal of the control body seals against a support body when the control body is in a closed position and the control body disengages from the support body in an open position.

2. The fuel injector of claim 1 , wherein the control body further includes a throttled passage extending from the distal end of the control body to the proximal end of the control body connecting the first control chamber with the second control chamber.

3. The fuel injector of claim 2 , wherein the throttled passage further includes a control body orifice configured to control a closing rate of the control body and a closing rate of the nozzle valve.

4. The fuel injector of claim 1 , wherein the control body further includes a protrusion on an outer surface of the control body configured to control axial movement of the control body along the injector body.

5. The fuel injector of claim 4 , wherein an inner surface of the chamber housing further includes a shoulder below the protrusion of the control body and the inlet passage, the shoulder configured to control the movement of the control body along the longitudinal axis.

6. The fuel injector of claim 5 , further including a spring positioned in the chamber housing between the protrusion and the shoulder.

7. The fuel injector of claim 1 , wherein the chamber housing is disposed between a nozzle sleeve, the nozzle valve, and the pilot valve, the chamber housing being positioned in abutment against the nozzle sleeve restricting fuel flow, and the nozzle valve having a close sliding fit with an inside surface of the nozzle sleeve.

8. The fuel injector of claim 1 , wherein the control body defines an annular guiding clearance at the distal end of the control body between an outer surface of the control body and an inner surface of the chamber housing.

9. The fuel injector of claim 1 , wherein the control body has a third diameter at the distal end of the control body which is greater than the second diameter.

10. The fuel injector of claim 1 , wherein the inlet passage is throttled.

11. A fuel system, comprising:
a fuel tank communicating with a high pressure generating module;
a fuel injector;
a fuel supply channel extending between the high pressure generating module and the fuel injector; and
a return channel extending between the fuel injector and the fuel tank;
wherein the fuel injector includes an injector body having a longitudinal axis, an injector cavity, an injector orifice at a distal end of the injector cavity, and an inlet conduit configured to supply fuel into the injector cavity, a nozzle valve in the injector cavity, a drain circuit configured to drain fuel from the injector cavity to a low pressure drain, a pilot valve in flow communication with the drain circuit, a chamber housing having an unrestricted inlet passage to receive fuel from the injector cavity, a return port in flow communication with the pilot valve to drain fuel to the drain circuit, and an abutting surface surrounding the return port, and a control body slidably disposed in the chamber housing, wherein the control body having a distal end, a proximal end, and a longitudinal axis parallel with the injector body longitudinal axis, a first depression at the distal end of the control body defining a first control chamber in which one end of the nozzle valve is received, a second depression at the proximal end defining a second control chamber in flow communication with the return port, and an annular seal disposed radially of the second depression having a first diameter at an inner surface and a second diameter at an outer surface, wherein the first diameter is smaller than the second diameter.

12. The fuel system of claim 11 , wherein the control body further includes a throttled passage extending from the distal end of the control body to the proximal end of the control body connecting the first control chamber with the second control chamber.

13. A method, comprising:
energizing a fuel injector pilot valve thereby causing a sealing element to open resulting in a pressure differential between a first control chamber and an injector cavity to a level which enables a nozzle valve to move upward toward an open position and begin a fuel injection event;
de-energizing the pilot valve thereby causing the sealing element to close while the nozzle valve continues to move upward pressurizing a second control chamber to a level which enables a control body to open relative to the sealing element and permit fuel to flow from the injector cavity to the second control chamber, the control body having a distal end, a proximal end, and a first depression at the distal end of the control body defining the first control chamber in which one end of the nozzle valve is received;
ending the fuel injection event when the nozzle valve closes in response to a pressure differential between the first control chamber, the second control chamber, and the injector cavity; and
closing the control body in response to a drop in pressure differential between the injector cavity and the second control chamber.

14. The method of claim 13 , wherein applying a biasing force to the control body to open relative to the sealing element by providing an annular seal at a proximal end of the control body.

15. A fuel injector, comprising:
an injector body having a longitudinal axis, an injector cavity, an injector orifice at a distal end of the injector cavity, and an inlet conduit configured to supply fuel into the injector cavity;
a nozzle valve in the injector cavity;
a drain circuit configured to drain fuel from the injector cavity to a low pressure drain;
a pilot valve in flow communication with the drain circuit;
a chamber housing having an inlet passage to receive fuel from the injector cavity, a return port in flow communication with the pilot valve to drain fuel to the drain circuit, and an abutting surface surrounding the return port; and
a control body slidably positioned in the chamber housing, the control body having a distal end, a proximal end, and a first depression at the distal end of the control body defining a first control chamber in which one end of the nozzle valve is received the nozzle valve is received; the control body further includes, a longitudinal axis pa

Assignees

• Cummins Inc

Inventors

• Benson Donald J
• Sabri Ahmad M
• Konakanchi Hanumantharao

Classifications

• F02M63/0012

  Valves (for fuel metering see the relevant groups, e.g. F02M59/34; inlet or outlet check valves for fuel injection pumps F02M59/46; for fuel injectors see the relevant groups, e.g. F02M61/00) · CPC title

• F02M47/027

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

• F02M55/002 Primary

  Arrangement of leakage or drain conduits in or from injectors · CPC title

• F02M63/0225

  Fuel-injection apparatus having a common rail feeding several injectors (F02M63/0003 takes precedence); Means for varying pressure in common rails; Pumps feeding common rails · CPC title