Partial Travel Solenoid Valve Actuation Arrangement

Patent metadata

Field	Value
Publication number	US-2018163677-A1
Application number	US-201615375551-A
Country	US
Kind code	A1
Filing date	Dec 12, 2016
Priority date	Dec 12, 2016
Publication date	Jun 14, 2018
Grant date	—

Abstract

A valve assembly for a fuel pump is provided. The valve assembly may include an inlet valve limited to a first range of travel extending between a fully closed position and a fully opened position of the inlet valve, a valve pin coupled to the inlet valve, an armature pin selectively engaging the valve pin, and an armature coupled to the armature pin and limited to a second range of travel extending between an engaged position and a disengaged position that is less than the first range of travel.

First claim

What is claimed is:

1 . A valve assembly for a fuel pump, the valve assembly comprising:
an inlet valve limited to a first range of travel extending between a fully closed position and a fully opened position of the inlet valve; a valve pin coupled to the inlet valve; an armature pin selectively engaging the valve pin; and an armature coupled to the armature pin and limited to a second range of travel extending between an engaged position and a disengaged position that is less than the first range of travel.

2 . The valve assembly of claim 1 , wherein the inlet valve is limited to the first range of travel by one or more valve retainers and one or more valve stops, and the armature is limited to the second range of travel by one or more armature shims and one or more armature pin stops.

3 . The valve assembly of claim 2 , wherein the one or more valve retainers are coupled to the inlet valve and arranged to interface with the one or more valve stops to prevent the inlet valve from travelling beyond the fully opened position.

4 . The valve assembly of claim 2 , wherein the one or more armature shims are arranged to interface with the armature to prevent the armature from travelling beyond the engaged position, and the one or more armature pin stops are arranged to interface with the armature pin to prevent the armature pin from travelling beyond the disengaged position.

5 . The valve assembly of claim 1 , wherein the armature pin in the engaged position is arranged to at least partially open the inlet valve and prevent the inlet valve from fully closing.

6 . The valve assembly of claim 1 , wherein the inlet valve is biased in the fully closed position by a return spring, and the armature is biased in the engaged position by a solenoid spring.

7 . An actuation arrangement for a fuel pump having a pump housing, a passageway and a pump chamber, the actuation arrangement comprising:
an inlet valve disposed in communication between the passageway and the pump chamber and limited to a first range of travel extending between a fully closed position and a fully opened position; a valve pin disposed within the passageway and coupled to the inlet valve; an armature pin selectively engaging the valve pin; an armature coupled to the armature pin and limited to a second range of travel extending between an engaged position and a disengaged position that is less than the first range of travel; and a solenoid operatively coupled to the armature and configured to selectively adjust the armature between the engaged position and the disengaged position.

8 . The actuation arrangement of claim 7 , wherein the inlet valve is limited to the first range of travel by one or more valve retainers and one or more valve stops, and the armature is limited to the second range of travel by one or more armature shims and one or more armature pin stops.

9 . The actuation arrangement of claim 7 , wherein the solenoid includes a solenoid spring and a solenoid coil, the solenoid spring being configured to maintain the armature in the engaged position when the solenoid coil is not energized, and the solenoid coil being configured to electromagnetically actuate the armature into the disengaged position when energized.

10 . The actuation arrangement of claim 9 , wherein the armature pin is arranged to abut the valve pin to at least partially open the inlet valve and prevent the inlet valve from fully closing when the solenoid is not energized, and release the valve pin to enable the inlet valve to fully close when the solenoid is energized.

11 . The actuation arrangement of claim 7 , wherein the inlet valve is biased in the fully closed position by a return spring, and the armature is biased in the engaged position by a solenoid spring.

12 . The actuation arrangement of claim 11 , wherein the return spring is provided with a spring force sized to be overcome by forces associated with one or more of the solenoid spring and pressure differentials across the inlet valve, and the solenoid spring is provided with a spring force sized to withstand forces associated with one or more of the return spring and pressure differentials across the inlet valve.

13 . A fuel pump, comprising:
a pump housing; a pump chamber disposed within the pump housing and in communication with the fuel pump; a passageway disposed within the pump housing and in communication with the pump chamber; an inlet valve disposed in communication between the pump chamber and the passageway and limited to a first range of travel; a valve pin disposed within the passageway and coupled to the inlet valve; an armature pin selectively engaging the valve pin; an armature coupled to the armature pin and limited to a second range of travel that is less than the first range of travel and extends between an engaged position and a disengaged position; and a solenoid operatively coupled to the armature and configured to selectively adjust the armature between the engaged position and the disengaged position.

14 . The fuel pump of claim 13 , further comprising one or more valve retainers disposed on the inlet valve arranged to interface with one or more valve stops disposed within the passageway to prevent the inlet valve from travelling beyond a fully opened position.

15 . The fuel pump of claim 13 , further comprising one or more armature shims and one or more armature pin stops, the one or more armature shims being disposed on the pump housing and configured to interface with the armature to prevent the armature from travelling beyond the engaged position, and the one or more armature pin stops being disposed within the passageway and configured to interface with the armature pin to prevent the armature pin from travelling beyond the disengaged position.

16 . The fuel pump of claim 13 , further comprising one or more shims disposed between the armature and the solenoid and arranged to maintain a predefined minimum air gap therebetween.

17 . The fuel pump of claim 13 , wherein the solenoid is configured to maintain the armature in the engaged position when the solenoid is not energized, and electromagnetically actuate the armature into the disengaged position when the solenoid is energized.

18 . The fuel pump of claim 17 , wherein the armature pin is arranged to abut the valve pin to at least partially open the inlet valve and prevent the inlet valve from fully closing when the solenoid is not energized, and release the valve pin to enable the inlet valve to fully close when the solenoid is energized.

19 . The fuel pump of claim 13 , wherein the inlet valve is biased in a fully closed position by a return spring, and the armature is biased in the engaged position by a solenoid spring.

20 . The fuel pump of claim 19 , wherein the return spring is provided with a spring force sized to be overcome by forces associated with one or more of the solenoid spring and pressure differentials across the inlet valve, and the solenoid spring is provided with a spring force sized to withstand forces associated with one or more of the return spring and pressure differentials across the inlet valve.

Assignees

• Caterpillar Inc

Inventors

• Cox Glenn B
• Lewis Stephen R
• Brasche Adrienne M
• Tatikonda Venkata R

Classifications

• F02M63/0075

  Stop members in valves, e.g. plates or disks limiting the movement of armature, valve or spring · CPC title

• F02M37/0023 Primary

  Valves in the fuel supply and return system · CPC title

• F16K31/06

  using a magnet {, e.g. diaphragm valves, cutting off by means of a liquid} · CPC title

• F02M59/368 Primary

  Pump inlet valves being closed when actuated · CPC title