The present invention relates to a fuel injector or fuel injection valve.
A fuel injector of one known type includes a valve seat member formed with a valve seat; a valve element slidably received in a tube member and driven by a drive section to move to and from the valve seat; and a nozzle plate formed with one or more injection holes to inject fuel after passage through the interspace opened between the valve element and valve seat in a valve open state. Fuel injectors of such a type are disclosed in Published Japanese Patent Application Publication No. H03-130571published on Jun. 4, 1991; Published Japanese Utility Model Application Publication No. H03-108855published on Nov. 8, 1991; and Published Japanese Patent Application Publication No. 2005-155547 published on Jun. 16, 2005. Fuel supplied into the tube member is conveyed through a hollow portion between the inside circumferential surface of the tube member and the valve element, thereafter guided to the nozzle plate and injected through the injection holes. In the fuel injector of Published Japanese Patent Application Publication No. 2005-155547, the valve element includes a spherical valve body and a sliding portion slidably supported by the tube member.
In a fuel injector of such a type, the sliding portion of the valve element tends to disturb the flow of fuel during the flow between the side surface of the valve element and the inside circumferential surface of the tube member, and thereby to exert adverse influence on the atomization of injected fuel.
It is therefore an object of the present invention to provide a fuel injector to promote the atomization of injected fuel.
According to one aspect of the present invention, a fuel injector comprises: a tube member including an inside bore for passage of a fuel; a valve seat provided in a downstream end portion of the tube member; a valve element arranged to slide axially in the tube member to and away from the valve seat; a plurality of plate portions provided in the valve element and arranged to slide on an inside circumference surface of the tube member, the plate portions projecting radially with respect to an axis of the tube member, each of the plate portions including a side surface extending along the axis of the tube member; a drive section to move the valve element to and away from the valve seat; a nozzle member including at least one injection hole located on an inner side of the valve seat within the tube member and arranged to inject the fuel allowed to pass through a clearance formed between the valve element and the valve seat; and a guide portion to bend the flow of the fuel allowed to flow along the plate portions, toward the axis of the tube member and thereby to guide the fuel to the injection hole.
According to another aspect of the invention, a fuel injector comprises: a tube member including an inside bore for passage of a fuel; a valve element arranged to slide axially in the tube member between a valve close position, and a valve open position, the valve element including a center portion; and a plurality of plate portions projecting radially from the center portion and fitting slidably in the tube member(; and a guide section including an outer portion defining a valve seat provided at a downstream end of the tube member, and an inner portion which is located on a radial inner side of the outer portion, and which is formed with at least one injection hole arranged to inject the fuel conveyed through an interspace formed between the valve seat and the valve element, the guide section being arranged to divert the flow of the fuel conveyed along the plate portions, to a radial inward direction toward the injection hole.
A first embodiment of the present invention is illustrated in
A fuel injector 1 shown in
As shown in
The tube member 3 is a stepped thin-wall metal tube of a magnetic material such as stainless material or stainless alloy, formed by press forming such as deep drawing. Tube member 3 of this example extends axially from a first end (upper end or upstream end) to a second end (lower end or downstream end), and includes a large diameter section 3a extending from the first end toward the second end and a small diameter section 3b extending from the second end to a step formed between the large and small diameter sections 3a and 3b. The first (upstream) end of tube member 3 is adapted to be inserted in a boss portion of a fuel pipe and thereby connected with the fuel pipe.
An O-ring 18 is fit over the outside circumference of the first end of tube member 3 to secure a liquid-tight connection between tube member 3 and the boss portion of the fuel pipe. A filter 21 is fit in the upstream end of tube member 3. Filter 21 includes a tubular portion 21a press-fit in the large diameter section of tube member 3; a frame portion 21b of a resin material (such as nylon or fluoroplastics) softer than the material of tube member 3, formed integrally with the tubular portion 21a (by injection molding, in this example); and a mesh element 21cinstalled in frame portion 21b and arranged to allow the fuel to pass through.
Inside the tube member 3, there are provided the core tube 5; a valve element 6 on the downstream side of core tube 5; and a nozzle member 9 on the downstream side of valve element 6. Nozzle member 9 is a single integral (jointless) member. Valve element 6 is slidable axially between the core tube 5 and nozzle member 9 which are fixed in tube member 3.
Core tube 5 is a member to form a closed magnetic circuit with an outer tube portion 8 of valve element 6 and yoke 13, and to define a valve open position of valve element 6 by limiting the axial movement of valve element 6. Core tube 5 is installed in the small diameter section 3b of tube member 3 by press fitting.
Nozzle member 9 is located in a downstream end portion of tube member 3 so as to close the downstream end of tube member 3. As shown in
The disk-shaped end portion 9a of nozzle member 9 includes an inner portion formed with a plurality of injection holes 9e; an outer portion surrounding the inner portion and defining a valve seat 9f; and an outermost guide portion surrounding the valve seat 9f of the outer portion. In this example, the inner portion formed with injection holes 9e is a center portion, the outer portion of the valve seat 9f is an annular portion surrounding the inner portion including injection holes 9e, and the outermost guide portion is an annular portion surrounding the outer portion of the valve seat 9f. In this example, the inner and outer portions are inner and outer regions of a domed portion 9d bulging upward toward valve element 6 on the upstream side. The outermost guide portion is an annular flat portion which surrounds the domed portion 9d and which is shaped like a circular ring bounded between two concentric circles, as shown in
Each of injection holes 9e is a through hole passing through the wall of disk-shaped end portion 9a. In this example, each injection hole 9e is slightly inclined so as to inject fuel in a direction slightly inclined toward the radial outward side with respect to the axial direction. In this example, each injection hole 9e is tapered. For example, each injection hole 9e is tapered in the downstream direction so that the diameter or cross sectional size of the injection hole 9e becomes gradually smaller from the upstream open end of the injection hole to the downstream open end. Alternatively, each injection hole 9e may be tapered in the upstream direction or flared in the downstream direction so that the diameter or cross sectional size of the injection hole 9e becomes gradually greater from the upstream open end of the injection hole to the downstream open end.
The annular outer portion of disk-shaped end portion 9a of nozzle member 9 has an upstream surface facing toward valve element 6 and serving as the annular valve seat 9f on which valve portion 7 of valve element 6 rests when closed. The annular valve seat 9f of the annular outer portion surrounds all the injection holes 9eformed in the central inner portion which is located on the radial inner side of the annular valve seat 9f of the outer portion. Preferably, the outer portion 9f defining the valve seat is thicker than the inner portion formed with the injection holes, so that the wall thickness of the outer portion is greater than the wall thickness of the inner portion.
The nozzle member 9 serves as a guide section for guiding the flow of the fuel to injection holes 9e by bending the flow direction of the fuel from the axial flow along plate portions 7p of valve element 6, to the radial inward direction toward the center axis of tube member 3.
The valve element 6 is received slidably in small diameter section 3b of tube member 3, and arranged to move axially between core tube 5 and nozzle member 9, toward and away from the valve seat 9f of nozzle member 9. In this embodiment, valve element 6 includes an outer tube portion 8 of a magnetic metallic material in the form of a tube extending axially; and a valve portion 7 which is made of a resin, which is fixed in the outer portion 8, and which is arranged to rest on the valve seat 9f and to rise from valve seat 9f. In this example, the outer tube portion 8 and valve portion 7 are joined together by an interdigitating structure of an outside portion 7d formed in the outside wall surface of valve portion 7 and composes of a projection and a depression, and an inside portion 8dformed in the inside wall surface of outer tube portion 8 and composed of a projection fit in the depression of the outside portion 7d, and a depression fitting over the projection of the outside portion 7d of valve portion 7. This interdigitating structure can be formed by insert molding.
As shown in
Upstream enlarge portion 7a of valve portion 7 is cup-shaped, and includes a cylindrical wall opening upstream and a bottom closing a downstream end of the cylindrical wall. Upstream enlarge portion 7a includes an inside cavity 7e defined by the cylindrical wall and the bottom, and arranged to receive a part of a coil spring 12. A plurality of through holes 7f are formed in the bottom of upstream enlarge portion 7a. These through holes 7ffluidly connect the inside cavity 7e of upstream enlarged portion 7a to fuel chamber 10 formed around the intermediate narrow portion 7b. A blind hole 7g is formed in valve portion 7 to reduce the weight and improve the formability of valve element 6. The blind hole 7g extends along the center line of valve element 6 from the bottom of upstream enlarged portion 7a, through intermediate narrow portion 7b to downstream enlarged portion 7c.
The downstream enlarged portion 7c includes a center portion and a plurality of plate portions 7p projecting radially outwards from the center portion, and defining a plurality of fuel passages 7h in the form of guide grooves for conducing the fuel from fuel chamber 10 toward the nozzle member 9. Preferably, fuel passages 7h are formed at regular angular intervals or with a predetermined pitch in the outer circumference of downstream enlarged portion 7c. Each fuel passage 7h is formed between adjacent two of the plate portions 7p and the inside circumferential (cylindrical) wall surface of tube member 3. In this embodiment, as shown in
In the illustrated example, the six plate portions 7p are arranged at regular angular intervals of 60 degrees.
The bottom of downstream enlarged portion 7c of valve portion 7 (that is, the forward end portion of the valve element) is formed with a spherical depression 7j depressed approximately in conformity with the dome shape of the domed portion 9d of nozzle member 9, around the center axis of the valve element 6. The bending radius of this spherical depression 7j is smaller than the bending radius of domed portion 9d. An annular abutting projection 7k is formed so as to fringe the outer circumference of the spherical depression 7j, and adapted to abut fittingly on the annular valve seat 9f of nozzle member 9. In the valve close state shown in
Valve element 6 of this example is slidably supported, at both of the upstream end portion and the downstream end portion, in the small diameter section 3b of tube member 3. That is, the outer tube portion 8 of valve element 6 is slidably fit in the small diameter portion 3b of tube member 3, and at the same time the radially arranged plate portions 7p of downstream enlarged portion 7c are slidably fit in the small diameter portion 3b of tube member 3. Thus, valve element 6 is supported at two separate positions of valve element, in tube member 3 so that valve element 6 can slide axially in (the small diameter portion 3b of) tube member 3.
A drive section 24 shown in
The upper end of coil spring 12 abuts against the lower end of a tubular adjuster 19 fit in core tube 5. The lower end of coil spring 12 is received in the inside cavity 7e of valve element 6. Coil spring 12 is thus disposed under compression, as a compression spring, between the core tube 5 and valve element 6, so as to urge the valve element 6 in a valve closing direction away from core tube 5, toward the valve seat 9f.
The yoke 13 is a stepped tubular member mounted on tube member 3. In this example, yoke 13 is forcibly fit over the small diameter portion 3b of tube member 3, and thereby fixedly mounted on the small diameter portion 3b. A connection core 14 is provided between yoke 13 and the small diameter portion 3b of tube member 3. In this example, connection core 14 is an approximately C-shaped magnetic member surrounding the small diameter portion 3b of tube member 3. A resin cap 11 is fixed to a lower end portion of yoke 13, and arranged to define a groove for receiving an O-ring 23.
The magnetic coil 15 is disposed between the yoke 13 and tube member 3. Magnetic coil 15 includes a tubular bobbin 15a of resin material mounted on the small diameter portion 3a of tube member 3; and a wire 15b wound around bobbin 15a. Magnetic coil 15 is energized through at least one pin 20 of a connector 17, and conductor 22 formed in a resin cover 16.
The resin cover 16 encloses the tube member 3. Resin cover 16 of this example is formed by an injection molding in the state of a subassembly of tube member 3 including yoke 13, connecting core 14 and magnetic coil 15 mounted on tube member 3. Connector 17 and resin cover 16 are integral parts of a single resin molding.
The thus-constructed fuel injector is held, by the urging force of coil spring 12, normally in the close state shown in
When magnetic coil 15 is energized, the core tube 5, outer tube portion 8 of valve element 6 and yoke 13 form a closed magnetic circuit producing, in the outer tube portion 8, a magnetic force toward the core tube 5. Since the setting is such that the magnetic force (attraction force) becomes greater than the urging force of coil spring 15, the valve element 6 is attracted by the magnetic force against the urging force of coil spring 15, toward the core tube 5 away from the valve seat 9f, and the fuel injector is brought to the valve open state of
In this open state, the fuel flows down the fuel passage 4 in tube member 3 and core tube 5, and flows into fuel chamber 10 through the inside cavities of adjuster 19 and core tube 5, the depressed portion 7e and the through holes 7f of valve element 6. From fuel chamber 10, the fuel flows through the fuel passages 7h formed around the downstream enlarged portion 7c of valve element 6, and the gap or clearance formed between the abutting portion 7k of valve element 6 and valve seat 9f, and gushes out of injection holes 9e.
In this fuel injector, the fuel flow Fa in each fuel passage 7h is regulated in the axial direction by the axially extending plate portions 7p serving as means for regulating a fluid flow. Then, the flow is bent largely so as to form an approximately right angle or a sharp angle from the axial direction of the flow Fa to the radial direction of fuel flow Fb through the clearance between the abutting portion 7k and the valve seat 9f, by the guide of nozzle member 9 serving as guide section. Thereafter, the direction of fuel flow is changed again largely from the fuel flow Fb to a fuel flow Fc through each injection hole 9e, sharply so as to form an approximately right angle or a sharp angle. By changing the flow direction in this way, the fuel injector can cause separation of fuel from a wall surface and turbulent flow; thereby produce disturbance in the fuel flow injected from each injection hole 9e; and consequently promote the agitation with air and atomization of the fuel spray.
With the plate portions 7p and nozzle member 9 serving as the guide section, the thus-constructed fuel injector according to the first embodiment can change the direction of the fuel flow flowing from the plate portions 7p, to the valve seat 9f sharply, and thereby promote the atomization of injected fuel by causing separation of fuel from a wall surface, and turbulent flow.
In the first embodiment, the injection holes 9eand valve seat 9f are both formed in the nozzle member 9. This structure can decrease the number of required parts; facilitate the assembly process; and hence reduce the production cost of the fuel injector by decreasing the cost of component parts and the cost of the production process, as compared to the conventional structure having a member for defining a valve seat and a distinct member formed with injection holes.
As compared to the conventional structure having a member defining a valve seat and a distinct member formed with one or more injection holes, the single nozzle member 9 including both the valve seat 9f and one or more injection holes 9e makes it possible to decrease the size of the forward end portion of the fuel injector, and hence increase the degree of freedom in the layout of a mounting portion of the fuel injector in an internal combustion engine.
In this embodiment, the injection holes 9e are opened in the disk-shaped end portion 9a of nozzle member 9. Therefore, it is easy to adjust the direction of fuel flow toward the injection holes 9e by adjusting the shape of disk-shaped end portion 9a, and thereby to promote the atomization of fuel.
In the nozzle member 9 according to this embodiment, the outer portion in which valve seat 9f is formed is thicker in wall thickness than the inner portion in which one or more injection holes 9e are formed. Therefore, the rigidity of valve seat 9f is increased, and the durability of the fuel injector is improved.
In this embodiment, each of the injection holes 9e is tapered. Therefore, when fuel is injected through the injection hole 9e, the tapered injection hole tends to cause the fuel to form a liquid film on a circumferential surface of the injection hole 9e, and thereby promote the atomization.
In this embodiment, tube member 3 supports the valve element 6 slidably at the upstream and downstream end portions spaced along the axis of tube member 3. This structure is effective to prevent inclination of the valve element 6 and to improve the assembly accuracy of valve element 6, as compared to the structure in which the valve element is slidably supported at one end portion.
In this embodiment, the plate portions 7p are arranged radially at regular intervals around the center axis of tube member 3. This arrangement is effective to prevent inclination of the valve element 6, and to improve the accuracy in assemblage of valve element 6.
In this embodiment, with the upstream and downstream end portions being both slidably fit in tube member 3, the valve element 6 can slide in tube member 3 smoothly, and increase the dynamic flow rate. In the case of the support structure in which the upstream and downstream end portion of the valve elements are supported, respectively, by two different members, it is necessary to increase the accuracy in shape of the two members, and the accuracy in position of the two members in order to ensure the smooth movement of the valve member. By contrast to this, in the support structure according to this embodiment, it suffices to improve the accuracy in shape of tube member 3.
In this embodiment, the domed portion 9d of nozzle member 9 can improve the rigidity of nozzle member 9 and thereby improve the durability of nozzle member 9 against the fuel pressure and load applied from valve element 6, as compared to a nozzle member having an entirely flat end portion. Furthermore, one or more ribs 9c can further improve the rigidity and durability of nozzle member 9.
In this embodiment, the fuel injector has a self aligning or centering structure formed by the domed portion 9d of nozzle member 9 and the mating spherical depression 7j of valve element 6, to align the valve element 6 with the center axis of valve seat 9f when valve element 6 is seated on valve seat 9f. By preventing positional deviation between valve element 6 and nozzle member 9, this structure can ensure the sealing between valve element 6 and nozzle member 9, and reliably prevent leakage of fuel in the valve close state.
In this embodiment, the valve element 6 includes the valve portion 7 made of resin material. Therefore, the valve element 6 is lighter in weight as compared to a valve element made entirely of metallic material, and advantageous to lower the sound pressure level of noise produced by the abutment of the valve element on the valve seat.
As a variation of this embodiment, it is optional to form the fuel passages 7h in a helical shape so as to produce swirling flow.
A second embodiment of the present invention is illustrated in
The nozzle member 9A is a cup-shaped single member including a circular-disk-shaped end portion 9Aa and a cylindrical portion 9b extending axially from the circumference of end portion 9Aa like the nozzle member 9 according to the first embodiment. Unlike nozzle member 9, however, the end portion 9Aa is bulged entirely toward valve element 6, and shaped entirely in the form of a dome. Cylindrical portion 9b extends axially from the rim of the dome-shaped end portion 9Aa. In the example shown in
The dome-shaped end portion 9Aa functions to increase the rigidity of nozzle member 9A, and thereby to improve the durability of nozzle member 9A to bear the fuel pressure and load applied from valve element 6.
A third embodiment is illustrated in
The fuel injector 1B according to the third embodiment is different, in the shape of the valve element 6B, from the valve element 6 of the preceding embodiments. A valve portion 7B of valve element 6B includes a downstream end portion which includes a cylindrical center portion 7Bn and a plurality of plate portions 7Bp. Cylindrical center portion 7Bn extends in the axial direction of tube member 3 in alignment with the intermediate portion 7Bb of the valve portion 7b of valve element 6, and has a diameter substantially equal to the diameter of intermediate portion 7Bb. Plate portions 7Bp project radially from the cylindrical center portion 7Bn, and define a plurality of groove-shaped fuel passages 7h, each between two adjacent plate portions 7Bp.
Plate portions 7Bp project from the cylindrical center portion 7Bn radially in the manner of radial symmetry, to respective projecting ends adapted to slide on the inside circumferential (cylindrical) wall surface of the small diameter portion 3b of tube member 3. Each plate portion 7Bp has side surfaces extending axially in the axial direction of tube member 3.
With the plate portions 7Bp, the fuel injector according to the third embodiment can change the direction of the fuel flow from the plate portions 7Bp toward valve seat 9f as in the first embodiment largely, and thereby promote the atomization of injected fuel by separation of fuel from a wall surface and turbulence flow.
As shown in
As shown in
A fourth embodiment of the present invention is illustrated in
The fuel injector according to the fourth embodiment includes a valve seat member 41C in addition to a nozzle member 9C; and the forward end of a valve element 6C is formed in a shape different from that of the third embodiment. Nozzle member 9C of the fourth embodiment includes no valve seat.
The valve seat member 41C is annular and fixed in the downstream end portion of tube member 3. Valve seat member 41C includes upstream and downstream surfaces which are flat and parallel to each other in this example, and a tapered opening extending axially from an upstream end opened in the upstream surface to a downstream end opened in the downstream surface. The tapered opening is tapered to the downstream end, and defined by an inside circumferential wall surface which, in this example, is a conical surface so that the inside diameter becomes smaller toward the downstream end of the tapered hole. A valve seat 41Ca is defined in the inside circumferential wall surface of the tapered opening.
Nozzle member 9C is disposed on the downstream surface of valve seat member 41C so as to close the downstream end of the tapered opening. Nozzle member 9C of this example is in the form of a flat thin plate. Nozzle member 9C is fixed to tube member 3. A plurality of injection holes 9e are formed in a center region of nozzle member 9C so as to open into the tapered opening. In this example, the valve seat member 41C and nozzle member 9C constitute a guide section 30C.
The valve portion 7C of valve element 6 of this example has a flat downstream end surface whose circumference is adapted to abut on the valve seat 41Ca. With the flat downstream end, the valve element 6C of this example is simplified in construction.
A fifth embodiment of the present invention is illustrated in
In the fifth embodiment, a valve element 6D includes a spherical body or ball 7Dq provided at the lower end of a valve portion 7D unlike the valve element of the fourth embodiment. The plate portions 7Bp are located on the upstream side of the spherical body 7Dq.
In the valve close state, the spherical body 7Dq is seated on the valve seat 41Ca. Preferably, the diameter of spherical body 7Dq is substantially equal to or smaller than the diameter of center cylindrical portion 7Bn of valve portion 7D. The thus-constructed spherical body 7Dq is effective to prevent turbulence of the flow of fuel after passage through passages formed among plate portions 7Bp.
After passage through the fuel passages 7h defined by plate portions 7Bp, the fuel flow in the axial direction of tube member 3, at the side of spherical body 7Dq. Therefore, the fuel injector according to the fifth embodiment can change the flow direction from the axial direction to the direction toward the valve seat 9f around the spherical body 7Dq, and thereby promote the fuel atomization by promoting the separation of fuel from a wall surface and turbulent flow.
Various variations and modifications of the illustrated embodiments are possible.
The nozzle member 9 (or 9A) may be made of resin material.
This application is based on a prior Japanese Patent Application No. 2005-315172 filed on Oct. 28, 2005; and a prior Japanese Patent Application No. 2006-219631 filed on Aug. 11, 2006. The entire contents of these Japanese Patent Applications No. 2005-315172 and No. 2006-219631 are hereby incorporated by reference.
Although the invention has been described above by reference to certain embodiments of the invention, the invention is not limited to the embodiments described above. Modifications and variations of the embodiments described above will occur to those skilled in the art in light of the above teachings. The scope of the invention is defined with reference to the following claims.
Number | Date | Country | Kind |
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2005-315172 | Oct 2005 | JP | national |
2006-219631 | Aug 2006 | JP | national |
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Number | Date | Country | |
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20070095949 A1 | May 2007 | US |