Electromagnetic actuator and stator design in a fuel injector assembly

• US 6,565,020 B1
• Filed: 07/16/2002
• Issued: 05/20/2003
• Est. Priority Date: 07/16/2002
• Status: Expired due to Term

• Current Assignee: Robert Bosch GmbH
• Original Assignee: Detroit Diesel Technology
• Inventors: Helsel, Todd, Eickholt, David, Fischer, W. Scott
• Primary Examiner(s): Maust, Timothy L.
• Assistant Examiner(s): Kontos, Lina R
• Application Number:
  US10/197,317
• Time in Patent Office: 308 Days
• Field of Search: 239/585.1, 239/585.5, 239/88, 239/96
• US Class Current: 239/585.1
• CPC Class Codes: F02M 51/005 Arrangement of electrical wires and connections, e.g. wire harness, sockets, plugs; Arrangement of electronic control circuits in or on fuel injection apparatus
• CPC Class Codes: F02M 57/023 mechanical
• CPC Class Codes: F02M 59/366 Valves being actuated electrically
• CPC Class Codes: F02M 59/466 Electrically operated valves, e.g. using electromagnetic or piezoelectric operating means

Abstract

An electromagnetic actuator for a control valve module in an engine fuel injector, the module being a replaceable, independent element of the injector. The actuator has a stator with electromagnetic coil windings on a bobbin located within the control valve module. An armature is connected to a control valve in the module. The bobbin supports and precisely positions connector pins for the coil windings for registry with an external electrical wire harness.

Claims

1. An electromagnetic actuator for a fluid pressure control valve in a fuel injector for an internal combustion engine, the injector having a control module subassembly, a pump body defining a fuel pumping cylinder, an engine driven plunger in the cylinder, a fuel nozzle assembly comprising a nozzle control valve spring and spring cage subassembly, the module subassembly being disposed between the spring cage subassembly and the pump body;

the control module subassembly including a fuel pressure control valve, the electromagnetic actuator having an armature connected to the fuel pressure control valve, the control valve having a centerline extending in the direction of movement of the armature;

a stator assembly adjacent to the armature including an electric coil bobbin, coil windings supported on the bobbin, the bobbin having an extension disposed radially outward relative to the control valve;

electrical connector pins secured to the bobbin extension and connected to wire leads at ends of the coil windings, the connector pins extending in the direction of the centerline and into the pump body; and

an external connector assembly secured to the pump body comprising electrical conductors for establishing a connection with an engine controller, the connector assembly establishing an electrical connection between the pins and the electrical conductors as the control module subassembly is assembled in place adjacent to the pump body.

2. The electromagnetic actuator set forth in claim 1 wherein wire leads at the ends of the coil windings are trained over the bobbin extension at a side of the bobbin directly adjacent the armature, the bobbin being disposed within the control module subassembly and the armature being disposed between the bobbin and the pump body.

3. The electromagnetic actuator set forth in claim 1 wherein the bobbin extension maintains the connector pins at a radial position relative to the control valve centerline to establish registry of the connector pins with respect to the electrical conductors in the connector assembly.

4. The electromagnetic actuator set forth in claim 1 wherein the pump body is provided with a recess, the connector assembly being secured in the recess with the electrical conductors aligned with the connector pins on the bobbin extension whereby the connector pins and the electrical conductors are electrically connected as the fuel injector is assembled with the pump body, the control module subassembly and the fuel nozzle subassembly in stacked, abutting relationship.

5. The electromagnetic actuator set forth in claim 2 wherein the coil windings may be wound on the bobbin without interference with the connector pins and the length of the pins may be a minimum.

6. The electromagnetic actuator set forth in claim 2 wherein the pump body is provided with a recess, the connector assembly being secured in the recess with the electrical conductors aligned with the connector pins on the bobbin extension whereby the connector pins and the electrical conductors are electrically connected as the fuel injector is assembled with the pump body, the control module subassembly and the fuel nozzle subassembly in stacked, abutting relationship.

7. The electromagnetic actuator set forth in claim 1 wherein the bobbin, the coil windings and the bobbin extension are encased in an electrical insulator over-mold, the over-mold forming a reinforced riser from which the connector pins extend.

8. The electromagnetic actuator set forth in claim 2 wherein the extension is located at a side of the bobbin directly adjacent the armature, whereby the pins are of reduced length while establishing an electrical connection with the electrical conductors in the connector assembly.

9. The electromagnetic actuator set forth in claim 7 wherein the stator assembly comprises an electromagnetic core within the bobbin, a radial opening in the core, the radial extension being positioned in the radial opening, the over-mold providing a reinforced subassembly of the bobbin, the extension and the pins.

10. The electromagnetic actuator set forth in claim 9 wherein the stator assembly, including the pins, define a component of the control module subassembly, which is separable from the actuator and interchangeable with a replacement stator assembly.

11. The electromagnetic actuator set forth in claim 9 wherein the radial opening in the core is of a reduced size to provide increased magnetic flux density.

12. The electromagnetic actuator set forth in claim 1 wherein the stator assembly includes a stator core, the electric coil bobbin being received in the stator core, the stator core being received in the control module subassembly.

13. The electromagnetic actuator set forth in claim 12 wherein the stator core has an opening in which the bobbin extension is positioned.

14. The electromagnetic actuator set forth in claim 13 wherein the opening in the stator core is sized to provide for a minimum reduction of core material to effect maximum flux density.