The invention relates to a closure member for a fuel injector, and more particularly to a closure member that provides straight line fuel flow paths.
It is known to use a two-piece closure member that includes an armature connected to a needle, and to allow fuel flow through the known closure member. In particular, these known closure members are believed to have angled holes drilled through the armature such that fuel flow through the known closure member must make two turns or bends, i.e., at the entrance and exit of the angled holes. It is believed that the circuitous fuel flow path caused by these turns or bends, combined with the heavy armature of the known closure members, slows the movement, and hence response time, of these known closure members.
In order to increase closure member speed and improve fuel injector performance, it is believed that there is a need to eliminate the turns or bends in the fuel flow path and to reduce the weight of known closure members
The present invention provides a fuel injector that includes a housing, a passageway, a coil assembly, a seat, and a closure member. The housing extends along a longitudinal axis between an inlet and an outlet, and fuel flows through the passageway from the inlet to the outlet. The coil assembly is disposed proximate the inlet of the housing, and the seat is disposed proximate the outlet of the housing. The closure member is disposed in the housing and is movable along the longitudinal axis between a first position, which prohibits fuel flow, and a second position, which permits fuel flow. The closure member includes a magnetic member, a needle, and a tubular member. The magnetic member is adapted to cooperate with the coil assembly to move the closure member from the first position to the second position. The needle member occludes the seat in the first position of the closure member. The tubular member couples the magnetic member to the needle member, and defines a portion of the passageway. The tubular member extends between a first end, which defines a first opening, and second end, which defines a second opening. A portion of the first opening is aligned with the second opening such that fuel flow between the first and second openings is along a flow path that is parallel to the longitudinal axis.
The present invention further provides a closure assembly that moves along a longitudinal axis between a first position, which prohibits fuel flow through a fuel injector, and a second position, which permits fuel flow through the fuel injector. The closure member includes an acting member, an occluding member, and a tubular member. The acting member is influenced to cause movement from the first position to the second position. The occluding member prohibits fuel flow in the second position. And the tubular member couples the acting member to the occluding member. The tubular member extends between a first end, which defines a first opening, and second end, which defines a second opening. A portion of the first opening is aligned with the second opening such that fuel flow between the first and second openings is along a flow path that is parallel to the longitudinal axis.
The present invention further provides a method of manufacturing a closure member for a fuel injector. The method includes coupling a magnetic member to a first end of a tubular member, inserting a needle member in a second end of the tubular member, and crimping the second end of the tubular body. The inserting includes positioning an exterior surface of the needle member to confront an interior surface of the tubular member. And the crimping includes contiguously engaging a first portion of the interior surface of the tubular member with a first portion of the exterior surface of the needle member, and includes spacing a second portion of the interior surface of the tubular member with a second portion of the exterior surface of the needle member.
The accompanying drawings, which are incorporated herein and constitute part of this specification, illustrate presently preferred embodiments of the invention, and, together with the general description given above and the detailed description given below, serve to explain features of the invention.
A fuel inlet member 24 with an inlet passage 26 is disposed within the overmolded plastic member 20. The inlet passage 26 serves as part of the fuel passageway 16 of the fuel injector assembly 10. A fuel filter 28 and an adjustable tube 30 are provided in the inlet passage 26. The adjustable tube 30 is positionable along the longitudinal axis A before being secured in place, thereby varying the length of an armature bias spring 32. In combination with other factors, the length of the spring 32, and hence the bias force against the closure member 70, controls the quantity of fuel flow through the injector. The overmolded plastic member 20 also supports a socket 20a that receives a plug (not shown) to operatively connect the fuel injector assembly 10 to an external source of electrical potential, such as an electronic control unit (not shown). An elastomeric O-ring 34 is provided in a groove on an exterior of the inlet member 24 to sealingly secure the inlet member 24 to a fuel supply member (not shown), such as a fuel rail.
The metallic support member 22 encloses an electromagnetic actuator assembly. An example of the actuator is a coil assembly 40. The coil assembly 40 includes a bobbin 42 that retains a coil 44. The ends of the coil assembly 40 are electrically connected to pins 40a mounted within the socket 20a of the overmolded plastic member 20.
A body shell 50 engages a body 52. An armature guide eyelet 56 is located on an inlet portion 60 of the body 52. An axially extending body passage 58 connects the inlet portion 60 of the body 52 with an outlet portion 62 of the body 52. A seat 64, which is preferably a metallic material, is mounted at the outlet portion 62 of the body 52.
The body 52 includes a neck portion 66 that extends between the inlet portion 60 and the outlet portion 62. The neck portion 66 can be an annulus that surrounds a portion of the closure member 70. Thus, the closure member 70 is supported for relative movement along the longitudinal axis A with respect to the inlet member 24.
Operative performance of the fuel injector assembly 10 is achieved by magnetically coupling the closure member 70 to the end of the inlet member 26 that is closest to the inlet portion 60 of the body 52. Thus, the lower portion of the inlet member 26 that is proximate to the closure member 70 serves as part of the magnetic circuit formed with the coil assembly 40. The closure member 70 is guided by the armature guide eyelet 56 and is responsive to an electromagnetic force generated by the coil assembly 40 for axially reciprocating the closure member 70 along the longitudinal axis A of the fuel injector assembly 10. The electromagnetic force is generated by current flow from the electronic control unit (not shown) through the coil assembly 40. Movement of the closure member 70 opens and closes the seat passage 66 of the seat 64, which permits or prohibits, respectively, fuel from flowing through the fuel outlet 14 of the fuel injector 10. In the open configuration of the fuel injector 10, there exists between the closure member 70 and the coil assembly 40 a working gap, which is preferably less than about 100 microns.
Fuel that is to be injected from the fuel injector 10 is communicated from the fuel inlet source (not shown), to the fuel inlet 12, through the fuel passageway 16, and exits from the fuel outlet 14. The fuel passageway 16 includes the inlet passage 26 of the inlet member 24, the body passage 58 of the body 52, the seat passage 66 of the seat 64, and as will be discussed hereinafter, the closure member 70.
Referring additionally to
The magnetic member 72 provides a working surface for the working gap with the coil assembly 40. While the magnetic member 72 can be any shape, in a preferred embodiment, as shown in the drawings, the sleeve 72 can be an annulus that extends along the longitudinal axis A. Although in a preferred embodiment, as shown in the drawings, the magnetic member 72 is a separate member that is coupled to the tubular member 76, it is to be understood that the magnetic member 72 can be a portion of the tubular member 76.
The needle member 74 can be disposed at an end of the closure member 70 to engage the seat 64, thereby permitting and preventing fuel flow from the fuel outlet 14 of the fuel injector 10. Although in a preferred embodiment, as shown in the drawings, the needle member 74 is a separate member that is coupled to the tubular member 76, it is to be understood that the needle member 74 can be a portion of the tubular member 76.
The tubular member 76 extends along the longitudinal axis A between a first end 76a, which is generally proximate the inlet 12, and a second end 76b, which is generally proximate the outlet 14. The first end 76a defines a first opening 78 and the second end 76b defines a second opening 80 such that fuel flow in the passageway 16 includes passing through the first and second openings 78,80.
With particular reference to
According to a preferred embodiment, the first end 76a of the tubular member 76 has an annular cross-section, and the second end 76b has a multi-lobed cross-section. With particular reference to
Preferably, the first lobes 90 define arcs of a circle that is generally equal to an outside diameter of the needle member 94, and gaps between the needle member 94 and the second lobes 92 define respective ones of the second openings 80.
The magnetic member 72 is coupled to a first portion 76c of the tubular member 76, and the needle member 74 is coupled to a second portion 76d of the tubular member 76. The first portion 76c may be welded, press fit, adhered, or otherwise fastened by any suitable means inside the magnetic member 72. As will be discussed in greater detail hereinafter, the second portion 76d is crimped so as to form the multi-lobed configuration of the second end 76b, and may then be welded, adhered, or otherwise fastened by any suitable means outside the needle member 74.
The tubular member 76 may also include an intermediate portion 76e between the first and second portions 76c,76d. The intermediate portion 76e may be perforated by at least one hole 100, which can provide an alternate flow path for fuel vapors that may arise due to engine heating of the fuel remaining in the fuel injector 10 after the engine is shut-off.
While the present invention has been disclosed with reference to certain preferred embodiments, numerous modifications, alterations, and changes to the described embodiments are possible without departing from the sphere and scope of the present invention, as defined in the appended claims. Accordingly, it is intended that the present invention not be limited to the described embodiments, but that it have the full scope defined by the language of the following claims, and equivalents thereof.
Number | Name | Date | Kind |
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5275341 | Romann et al. | Jan 1994 | A |
5544816 | Nally et al. | Aug 1996 | A |
5692723 | Baxter et al. | Dec 1997 | A |
5996911 | Gesk et al. | Dec 1999 | A |
6173915 | Cohen et al. | Jan 2001 | B1 |
Number | Date | Country | |
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20040195384 A1 | Oct 2004 | US |