The present invention relates to a method for coupling two components together after positioning thereof, and a fuel injection valve manufactured by utilizing the method.
The method described in JP-B-Hei 7(1995)-10471 (Patent Document 1) is well known as a method for concentric coupling of components made up of a plurality of members. It is described in Patent Document 1 that, in FIG. 1, a tapered hole (valve seat) 10c is formed in the inner bottom of a nozzle body (an outer cylindrical component) 10, provided with an orifice 11, a swirler (an inner cylindrical component) 12 provided with a through-hole 12a is installed inside the nozzle body 10 while securing a clearance therebetween, and the vicinity of a fitting part between the swirler 12 and the nozzle body 10 (a side of the fitting part, adjacent to the swirler 12 ) is pressed down by a punch 16 in such a way as to cause localized plastic flow while centering of the tapered hole 10c and the through-hole 12a of the swirler 12 is maintained by use of a positioning guide pin 14 , thereby causing both the components to undergo concentric plastic coupling by the force of the plastic flow. Further, the method described in Japanese Patent No. 3931143 (Patent Document 2) is also well known. In Patent Document 2, it is described that, in addition to the method according to Patent Document 1, protrusions 10d are provided on the bottom of the nozzle body 10, and the swirler 12 is caused to interlock with the protrusions 10d to thereby mechanically suppress deviation in the radial direction, so that coaxiality is prevented from undergoing deterioration.
With Patent Document 1, if coaxiality of the inside and outside diameters of the swirler is 0, and coaxiality of the inside diameter of the nozzle body, and the tapered hole is 0 when the swirler and the nozzle body are caused to undergo concentric coupling by the force of the plastic flow, a clearance between the inside diameter of the nozzle, and the outside diameter of the swirler will be consistent along the whole circumference. However, if the coaxiality is not 0 with respect to either the nozzle, or the swirler, the clearance between the inside diameter of the nozzle, and the outside diameter of the swirler will be inconsistent, so that stress occurring upon the coupling will be greater on a side where the clearance is smaller while the stress will be smaller on a side where the clearance, which is an axial target, is larger. For this reason, upon removal of the guide pin after the coupling, there occurs springback such that residual stress will become consistent all round. More specifically, the swirler moves from the side of smaller clearance toward the side of larger clearance, whereupon deviation occurs to coaxiality of the tapered hole, and the inside diameter of the swirler. Further, magnitude of the deviation is affected by coaxiality precision of components, and if the magnitude of the deviation reaches a predetermined value or higher, this will interfere with smooth movement of the movable valve, causing fuel leakage from the seat in the worst case.
Meanwhile, with Patent Document 2, the component 12 is caused to interlock with the protrusions 10d, thereby making an attempt for improvement with respect to a problem point of JP-B-Hei 7(1995)-10471. However, if the vicinity of the outer periphery of an upper end surface of the swirler 12 is pressed by protrusions 15 a provided at the tip of a punch 15 in
Thus, with the conventional technology, coaxiality of the inside diameter of the swirler, and the seat surface, after the coupling, is affected by component precision, and unless respective components are worked on with high precision, those components cannot be assembled together with high precision, so that problems have been encountered in that not only a working cost is high but also fuel leakage from the seat occurs, and the movement of the movable valve is adversely affected.
It is therefore an object of the invention to provide a method for coupling two components together, insusceptible to the effect of precision of each of the components, and capable of maintaining coaxiality of the components with high precision, after coupling thereof, and another object of the invention is to provide a fuel injection valve manufactured by utilizing the method, excellent in oil-tight property, and capable of guiding a movable valve with high precision.
To achieve the above objects, with the present invention, a softer member of the two components is subjected to shearing by a corner of a harder member of the two components while respective parts of the two components, positioning thereof being required, are kept in as-positioned state, a side face of the corner is fitted to a sheared surface of the softer member during shearing in progress, and subsequently, the two components are coupled at a fitting surface by plastic coupling, press-fitting, or welding.
Furthermore, a gap is provided between respective side faces of the two components except for at a fitting part as sheared in order to prevent external forces having effects on precision from being applied.
With the method according to the present invention, the two components can be fitted together consistently all round (with zero gap) with reference to the respective parts whose positioning is established, and since coupling is effected at the fitting surface, there occurs no deterioration in precision due to springback, a gap, and so forth, so that the two components can be coupled together with high precision while the respective parts are kept in the as-positioned state. In addition, since coupling is effected without being affected by component precision, precision in assembly of the two components can be obtained.
With a fuel injection valve manufactured by use of the present invention, because coaxiality of a guide, and a seat surface is excellent, a valve body moves smoothly, so that it is possible to stably inject fuel with excellent responsiveness, and at high precision. Further, fuel leakage from a seat part related to assembly precision can be prevented.
Embodiments of the invention are described hereinafter with reference to the accompanying drawings.
(First Embodiment)
A fuel injection valve main body 1 is comprised of a core 2, a yoke 3, a housing 4, a magnetic circuit made up of a movable element 5, a coil 6 for exciting the magnetic circuit, and a terminal block 7 for energizing the coil 6. A seal ring 8 is coupled between the core 2 and the housing 4, thereby preventing fuel from flowing into the coil 6.
Valve components are housed in the housing 4 where there are disposed the movable element 5, a nozzle 9, and a ring 10 for adjusting a stroke amount of the movable element 5. The movable element 5 is formed by coupling a valve body 11 with a movable core 12 at a joint 13. A plate 14 is for suppressing a bound that will occur upon the movable element 5 closing the valve in collaboration with a pipe 18, and the plate 14 is provided between the movable core 12, and the joint 13.
The housing 4, and the nozzle 9, making up an overcoat member, cover up the periphery of the movable element 5, the nozzle 9 has a seat surface 15a, and an orifice 54, at the tip thereof, and the nozzle 9 is provided with a nozzle 15 cup-like in shape, and a guide 17 slidably holding the movable element 5 in collaboration with a guide plate 16.
Disposed inside the core 2 are a spring 19 for pressing down the valve body 11 to the seat surface 15a through the pipe 18 and the plate 14, an adjuster 20 for adjusting a press-down load of the spring 19, and a filter 21 for preventing the ingress of contaminant from outside.
Now, operation of the fuel injection valve main body 1 is described in detail hereinafter.
Upon energization of the coil 6, the movable element 5 is drawn toward the core 2 by suction against the urging of the spring 9, whereupon a gap is formed between a valve seat 11a and the seat surface 15a at the tip of the movable element 5 (a open valve state). Pressurized fuel enters the nozzle 9 first from the core 2, the adjuster 20, and the pipe 18 via a fuel passage 13a inside the movable element 5. Subsequently, the fuel passes through a fuel passage 16a inside the guide plate 16, and a passage 17a inside the guide 17 to be injected through the gap between the valve seat 11a and the seat surface 15a via the orifice 54.
On the other hand, if current to the coil 6 is cut off, the valve seat 11a of the movable element 5 is butted against the seat surface 15a by the force of the spring 19, and a closed-valve state is brought about.
Next, a method for coupling the nozzle 15 with the guide 17 is described hereinafter with reference to
The coupling of the nozzle 15 with the guide 17 has a purpose that the valve body 11 is slidably held in a guide center hole 17b of the guide 17, and further, the valve seat 11a is in intimate contact with the seat surface 15a to thereby seal fuel. Accordingly, the guide center hole 17b need be coupled with the seat surface 15a at concentricity of, for example, not more than 10 μm. Furthermore, the nozzle 15 has hardness not less than HRC 52, and the guide 17 has hardness in a range of 130 to 350 Hv.
First, the guide 17 is set inside the nozzle 15, as shown in
With the components kept in this state, a guide 31a of a mandrel 31 is inserted into the guide center hole 17b, as shown in
Then, a punch 32 is caused to descend, so that the punch 32 is butted against the guide 17. When the punch 32 is caused to further descend, an edge of the guide 17 is interlocked by a step A15c as shown in
As the punch 32 continues to descend, the corner of the guide 17 is interlocked by a step B15e, as shown in
As shown in
As described in the foregoing, two components are coupled together only on a fitting surface with the sheared part 17c kept fitted to the side face of the step A15c without the gap formed therebetween while centering of the seat surface 15a and the guide center hole 17b is maintained, so that the residual stress will be uniform along the whole periphery, and coupling with high precision can be implemented without deviation of the guide 17 even after removal of mandrel 31.
Furthermore, the guide 31a of the mandrel 31 is preferably inserted into the guide center hole 17b without a gap being created therebetween, more preferably press-fitted therein. In addition, the outside diameter of the guide 17 is preferably not butted against the inside diameter 15b of the nozzle 15 except for at coupled parts, and a dimensional relationship between the outside diameter of the guide 17 and the inside diameter 15b of the nozzle 15 is set such that a clearance is provided therebetween.
Referring to
In
A method for coupling the nozzle with the guide is the same as that described with reference to
Further, in
If the undercut portion 15f, or the coupling groove 15g is provided, this will enable the strength of the coupling to be enhanced two to three times greater than the strength of the coupling by the auto-straining, shown in
(Second Embodiment)
In
A bearing A52, and a bearing B53 are coaxially secured inside a holder 51, and an axle 54 is supported at two points.
A method for assembling the bearing structure comprises the process steps of nesting a bearing B53 in an bore 51a of a holder 51 with a bearing A52 securely attached thereto by press-fitting and so forth, as shown in
Subsequently, as is the case with the method described with reference to
In the case of coupling by welding, a prerequisite for prevention of deviation in centering is to execute press-fitting, however, if the press-fitting is executed, centering by use of the mandrel 54 cannot be effected, so that it has been necessary to cause coaxiality of all parts related to coupling to approximate 0.
Having described the method for assembling the bearing structure with reference to
While the embodiments of the present invention have been specifically described as above, it is to be understood that the present invention is not limited thereto, and that various changes and modifications may be made in the present invention without departing from the spirit and scope thereof. With the present invention, for example, coaxiality has been described, however, with respect to positional precision, the same advantageous effect can be obtained, and high-precision positioning and assembling can be attained. Further, the excess metal generated upon shearing can be removed by pushing the bearing B to a greater depth.
Furthermore, with the second embodiment of the invention, the holder that is a hard component is provided with the step, however, if a hard metal is used for a bearing, a soft holder maybe used, and a step maybe provided on the outside diameter of the bearing that is hard.
With the embodiments of the present invention, if two components are coupled together with excellent positional precision, precision of a single component of the components will have no effect on coupling, so that it is possible to maintain precision after coupling, corresponding to the positional precision. Further, in the case of assembling with excellent positional precision by welding, and press-fitting, no means other than enhancement of single component precision have been available, however, with the embodiments of the present invention, precision can be enhanced at the time of assembling. Accordingly, even with the use of inexpensive components poor in single component precision, assembling at high precision can be implemented.
Explanation Of Reference Numerals
Number | Date | Country | Kind |
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2008-227720 | Sep 2008 | JP | national |
This application is a divisional of U.S. patent application Ser. No. 12/866,209, filed Aug. 4, 2010, which is a national stage of PCT International Application No. PCT/JP2009/062024, filed Jun. 24, 2009, which in turn claims the priority of Japanese application 2008-227720, filed Sep. 5, 2008. The entire disclosure of each of the above-identified applications is incorporated herein by reference.
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Number | Date | Country | |
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20120248228 A1 | Oct 2012 | US |
Number | Date | Country | |
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Parent | 12866209 | US | |
Child | 13495136 | US |