a is a view showing general shape of the forefront part of a needle valve,
a is a view showing the shape of the forefront part of the insert tool used in the first embodiment,
a is a view showing the shape of the forefront part of the insert tool having a spacer part used in the first embodiment,
a is a view showing the shape of the forefront part of the insert tool used in the second embodiment,
a is a view showing the shape of the forefront part of the insert tool used in the third embodiment,
a is a sectional view of the forefront part (part near the injection holes) of the nozzle body processed by the processing method of the third embodiment, and
Preferred embodiments of the present invention will now be detailed with reference to
First, the first embodiment of the invention will be explained referring to
The apparatus comprised mainly of an abrasive fluid supply section 1, a mounting platform 10, a nozzle body 20 to be processed, an insert tool 30 for abrasive fluid flowing processing, processing end detection sections 40, flow blocking sections 50, and a controller 60.
The abrasive fluid supply section 1 is composed of a barrel 2, a piston 3, a load detector 4, a displacement detector 5, and a piston drive device not shown in the drawing. The barrel 2 has an inside space in which abrasive fluid 7 is contained. A passage 6 for the abrasive fluid to flow through that has a diameter approximately as same as a diameter of fuel passage 21 of the nozzle body to be processed, is provided at the lower end of the inside space of the barrel 2. The piston 3 is placed in the inside space of the barrel 2 slidable with a small clearance to seal the abrasive fluid in the inner space. Driving force F is applied to the piston 3 by the piston drive device to push out the abrasive fluid 7 in the barrel 2 through the passage 6.
The load detector 4 and displacement detector 5 are provided to the piston 3. The load detector 4 serves to monitor so that pressure of abrasive fluid is maintained constant during abrasive fluid flowing processing and the displacement detector 5 serves to monitor piston displacement so that flow rate of abrasive fluid is calculated. The two detectors are connected to the controller 60 and to the piston drive device not shown in the drawing for closed-loop controlling.
The controller 60 controls so that pressure of abrasive fluid calculated by the two detectors is maintained constant.
The nozzle body 20 to be processed has a central hollow for accommodating a needle valve, and a tapered seat face 23 is formed in the central hollow at its forefront part. Six injection holes 24 are located at equal spacing in circumferential direction on the seat face 23. The six injection holes are drilled or formed by laser processing to communicate the central hollow with the outside of the nozzle body 20 beforehand. The nozzle body 20 has a fuel passage 21 extending from the rear end thereof to an annular space 22 provided in the central hollow at a central part thereof so that fuel is introduced from the annular space 22 to the injection holes 24 to be injected there through.
The nozzle body 20 is fixed to the mounting platform 10 by means not shown in the drawing, the insert tool 30 is inserted into the central hollow of the nozzle body 20, and the insert tool 30 is retained in position for abrasive fluid flowing processing.
Here, before explaining the insert tool used in abrasive fluid flowing processing of the first embodiment, opening and closing of a fuel injection nozzle will be explained briefly.
In this specification, the fuel injection nozzle means a combination of a nozzle body and a needle valve. A needle valve 100 having a two-stage-tapered pointed end part as shown in
The insert tool 30 is inserted into the central hollow of the nozzle body 20 for the purpose of performing abrasive fluid flowing processing under a condition of actual fuel flow as shown in
a is a view showing the shape of the forefront part of the insert tool used in the first embodiment,
An insert tool 30 having a pointed end part similar in shape to the needle valve 100 as shown in
The insert tool 30 is inserted into the central hollow of the nozzle body 20 such that the central axis of the insert tool coincides with that of the central hollow of the nozzle body 20 and the insert tool 30 is retained at a position at which the seat part of the conical surface of the insert tool departs from the conical seat face in the nozzle body 20 by a height of h along the central axis. The height h may be the maximum lift of the needle valve 100 in engine operation or smaller, however, it is more preferable that the height h is a half lift (half of the maximum lift of the needle valve 100) in point of view of reducing processing period. In
By retaining the insert tool 30 in position, conical annular channel is formed and the abrasive fluid can flow through the passage space surrounding the conical surface of the insert tool 30 to be introduced to the injection holes 24 as shown in
Another adjusting means of axial position of the insert tool 30 is shown in
As mentioned above, the insert tool 30 is inserted into the central hollow of the nozzle body 20, the insert tool 30 is retained in position, then the barrel 2 is attached so that the abrasive fluid flow passage 6 of the barrel 2 is communicated with the fuel passage 21 of the nozzle body 20, and the barrel 2 is fixed to the nozzle body concerning rotation position by a dowel pin 70. The abrasive fluid 7 in the barrel 2 pushed out by moving down the piston 3 through the flow passage 6 to the fuel passage 21 of the nozzle body 20 and introduced to the nozzle holes 24 through the annular channel 22 between the cylindrical part of the central hollow of the nozzle body and the cylindrical part of the insert tool and through the conical annular channel between the conical seat face 23 and the conical surface shaped similar to the conical surface of the needle valve 100.
As abrasive grains, silicon carbide, aluminum oxide, diamond, etc. may be used as has been used conventionally, and grain size is selected in accordance with the targeted diameter of injection hole. As to the medium for carrying abrasive grains, it is preferable to select a fluid having viscosity characteristic similar to that of fuel actually used so that abrasive fluid flowing processing is performed in a flow condition similar to that in the actual fuel flow when the abrasive fluid is flowed under pressure under which the abrasive fluid flow becomes a turbulent flow.
Each of the processing end detection sections 40 includes an abrasive fluid receiver 41, a load detector 42, and a computing unit not shown in the drawing. Each of the processing end detection section 40 is provided at the outlet side of each of the injection holes 24 so that weight of abrasive fluid passed through each injection hole can be measured independently. The detected weight of the abrasive fluid detected by the load detector 42 is inputted to the computing unit. Each of the computing unit sends a signal to the controller 60 when the mass flow rate of the abrasive fluid computed by each computing unit reaches a predetermined value, and the controller 60 connected to each load detector 42 sends a demand signal to each flow blocking section 50.
Each of the flow blocking sections 50 includes an air cylinder 51 and a blocking member 52 and provided near the outlet of each injection hole 24. The flow blocking sections 50 are connected to the controller 60. The air cylinder 51 pushes the blocking member 52 to block the outlet opening of a relevant injection hole upon receiving demand signal from the controller 60 to stop abrasive fluid flowing processing of the relevant injection hole. At the same time, the controller controls to reduce downward moving velocity of the piston so that pressure of the abrasive fluid in the barrel 2 is maintained constant. Abrasive fluid flowing processing ends when all of the holes are blocked.
The processing end detection sections 40 provided at the outlet side of each of the injection holes 24 use the load detectors 42 for detecting flow rate of abrasive fluid flowing out through each of the injection holes 24 in the embodiment, flow meters of any type which can measure flow rate of abrasive fluid flowing out through the each of the injection holes may be used. Any devices that can measure weight or volume per unit time of abrasive fluid flowing out through each of the injection holes can be adopted.
A nozzle body processed by the method and apparatus of the embodiment will have injection holes of which the entrance corner of each hole is rounded with a larger curvature radius in the upstream side of fuel in actual operation of engines than in the entrance corner other than the upstream side, because the sectional area of conical flow passage is reduced from the seat part toward the injection holes and the abrasive fluid flow is flexed larger at the entrance corner of upstream side as compared with the case the insert tool is not inserted into the central hollow of the nozzle body. When fuel is injected through the holes in actual operation of engines, a large part of fuel flows into the injection holes via the upstream side entrance corner of the holes, so the nozzle body with injection holes rounded with a larger curvature radius in the upstream side entrance corner where resistance for the flow entering the injection hole is particularly large is advantageous for fuel atomization and occurrence of cavitation erosion is reduced. Further, as abrasive fluid flowing processing for each injection hole is stopped independently when flow rate in weight or volume of abrasive fluid through the relevant injection hole reaches a predetermined rate, fuel atomization characteristic of each injection hole is evened.
Next, the second embodiment will be explained. In this embodiment, procedure in abrasion fluid processing in the second embodiment is the same as that in the first embodiment, an insert tool 30 different in shape from the insert tool 30 in the first embodiment is used in the second embodiment, because the insert tool in the second embodiment must be fixed in rotation position relative to the nozzle body. The injection hole processing apparatus shown in
a is a view showing the shape of the forefront part of the insert tool used in the second embodiment,
As shown in
Therefore, as shown in
The width of each passage groove 31 preferably wider than the diameter of injection hole 24 so that rounding of the entrance corner of the injection hole 24 is affected all around the corner by abrasive fluid flowing through the injection hole 24. It is also preferable that the passage grooves 31 extend below the lower side entrance corner of the injection holes 24 when the insert tool 30 is in position.
By supplying abrasive fluid through the fuel passage 21 of the nozzle body 20 with pressure of the abrasive fluid 7 maintained at a constant pressure as is in the first embodiment, the abrasive fluid flows to the injection holes 24 via the annular channel 22 and the passage grooves 31 with the insert tool 30 retained in position, and abrasive fluid flowing processing of the injection holes is performed in the same way as in the first embodiment. Stopping of the processing of each of the injection holes 24 is done in the same way as in the first embodiment.
A nozzle body processed by the method and apparatus of the embodiment will have injection holes of which the entrance corner of each injection hole is rounded with a larger curvature radius in the upstream side than in the entrance corner other than the upstream side, because abrasive fluid flows only through the passage grooves 31 extending along the along the generation lines of the conical surface, so the abrasive fluid flows into each injection hole 24 concentrically from the entrance thereof and the flow is flexed large at the upstream side corner of the entrance of the injection hole. When fuel is injected through the holes in actual operation of engines, a large part of fuel flows into the injection holes via the upstream side entrance corner rounded with a larger curvature radius where resistance for the flow entering the injection holes is particularly large, so the nozzle body with injection holes rounded with a larger curvature radius in the upstream side corner than in the downstream side corner is advantageous for fuel atomization and occurrence of cavitation erosion is reduced. Further, as abrasive fluid flowing processing for each injection hole is stopped independently when flow rate in weight or volume of abrasive fluid through the relevant injection hole reaches a predetermined rate, fuel atomization characteristic of each injection hole is evened.
Further, as abrasive fluid flows through the straight passage grooves 31, concave portions of very small depth not shown in the drawings are formed in the conical seat face 23 in the nozzle body 20 extending downstream along generation lines of the conical seat face to the injection holes 24. That is, the concave portions are formed to reach the injection holes 24 by the most direct way. Therefore, in actual operation of engines, fuel flows to the injection holes 24 easier taking the shortest way, and it is advantageous for increased fuel flow through the injection holes 24.
When the needle valve 100 is inserted into the central hollow of the nozzle body processed by the method and apparatus of the embodiment in actual operation of engines, fuel leak through the concave portions when the needle valve 100 is seated on the conical seat face 23 is prevented by designing so that proper elastic deformation occurs in the seating portion of the conical surface of the needle on the conical seat face in the nozzle body.
Next, the third embodiment will be explained. This embodiment differs from the first and second embodiments in that the insert tool is differently shaped and that abrasive fluid flowing processing of one injection hole is performed at a time.
As shown in
As shown in
Abrasive fluid flowing processing is performed by supplying the abrasive fluid 7 in the barrel 2 with pressure maintained at a constant pressure to the nozzle body 20 in the same way as in the first and second embodiment.
In the embodiment, when volume flow rate of abrasive fluid_calculated from displacement of the piston 3 detected by the displacement detector 5 reaches a predetermined value to stop abrasive fluid flowing processing, the controller 60 connected to the displacement detector 5 sends a demand signal to the piston 3 to stop its actuation. The load detector 4 and displacement detector 5 serve respectively as a monitoring sensor for maintaining pressure of abrasive fluid constant and a monitor sensor for determining timing of stopping abrasive fluid flowing processing. It is suitable of course to provide a processing end detection section separately as in the first and second embodiment.
When processing of one of the injection holes is finished, the insert tool 30 is rotated by a rotating means 80 so that the lower end part of the curved part of the passage groove 32 is brought into communication with one of other unprocessed injection holes and abrasive fluid flowing processing is performed for the injection hole. This process is repeated until all of the injection holes are processed.
The rotating device 80 includes a rack 81, a pinion 82, and a linear motor 83. The linear motor 83 is connected to the controller 60. The linear motor 83 shifts the rack 81, which is provided to the barrel 2 so that the rack 81 does not interfere the abrasive fluid in the barrel 2, by a predetermined distance in a determined direction upon recognizing a demand signal to shift the rack 81 sent from the controller 60. The pinion 82 is fixed to the upper end of the insert tool 30 and engaged with the rack 81, so the insert tool 30 is rotated by the circumferential angle between the injection holes so that the next injection hole to be processed is communicated with the passage groove 32 by shifting the rack 81 by the predetermined distance. When the injection holes are not formed at equal spacing to each other, shifting distance is determined in accordance with each circumferential pitch of the injection holes.
In the embodiment, although insert tool 30 is rotated, it is possible to compose such that the mounting platform 10 to which the nozzle body 20 is fixed is rotated about the central axis of the passage 6 of the barrel 2.
a is a sectional view of the forefront part (part near the injection holes) of the nozzle body processed by the processing method of the third embodiment, and
A nozzle body processed by the method and apparatus of the embodiment will have concave portions 26 of very small depth in the conical seat face 23 in the nozzle body 20 in the range below the seat position indicated by the broken line as shown in
In the case of processing the nozzle body by the method and apparatus of the embodiment, abrasive fluid is introduced to each injection hole 24 through the passage groove 32 and the entrance corner of the injection hole is ground by abrasive fluid concentrically at its corner connecting to the passage groove 32, so the entrance corner of the injection hole 24 is rounded large at one side and rounded small at the other side, and in actual operation of engines fuel tends to flow into each of the injection holes 24 via the entrance corner side rounded large. As a result, there occurs difference in fuel flow velocity between at the entrance corner rounded with a large radius and that rounded with a small radius, swirling flow is generated, and atomization of a larger angle of spray can be obtained.
Further, in the embodiment, as abrasive fluid flowing processing is performed for one injection hole at a time, only one processing end detection means is needed, and timing of stopping abrasive fluid flowing processing for all of the injection holes can be detected by one processing end detection means. In this case, it is also suitable to provide a means to rotate the mounting platform 10 to which the nozzle body 20 is fixed on the central axis of the passage 6 of the barrel 2 so that the fluid flowing out from one injection hole is received in the fluid receiver of the one processing end detection means every time abrasive fluid flowing processing for one injection hole is finished. Therefore, variation in accuracy of the processing end detection means does not occur, which may occur when plural injection holes are processed at the same time, and processing can be performed with higher accuracy.
While explanation has been done based on three embodiments, it is suitable to combine for example the second embodiment with the third embodiment such that an insert tool having one straight passage groove is used for processing injection holes one by one. It is suitable also to combine the third embodiment with the first and second embodiment such that an insert tool having a plurality of passage grooves each of which has a straight part and a curved part is used for processing all of the injection holes at the same time.
Further, when using an insert tool having a plurality of passage grooves, it is sufficient to use an insert tool that has passage grooves to correspond with injection holes, and shape of the grooves is not limited to be as described in the explanation of the first to third embodiments. Of course, the invention can be applied to the case of single injection hole.
According to the injection hole machining methods of claims 1-2 and according to the injection hole machining apparatuses of claims 7-8, the injection hole side end part of the insert tool is shaped similar to that of the needle valve and the insert tool is retained at a position that the needle valve is lifted in actual operation of engines when abrasive fluid flowing processing is performed, abrasive fluid flows through a space very similar to that when fuel flows in actual operation of engines at least upstream of the injection holes. As a result, the entrance corner of each injection hole is rounded with a larger radius of curvature particularly in the upstream region of fuel flow than other regions, and a nozzle body claimed in claim 13 can be obtained. In actual operation of engines, a large part of fuel flows concentrically from the upstream side entrance corner into the injection hole, so it is very important to be able to round the upstream side entrance corner with a large radius curvature. That is, the entrance corner of the injection hole can be effectively rounded with a large radius of curvature in a region where flow resistance is large for fuel entering the injection hole, and occurrence of cavitation erosion due to occurrence of separation of fuel flow near the needle valve and injection holes is suppressed and variation in fuel injection characteristic is reduced.
According to the injection hole machining methods of claims 3, 5 and according to the injection hole machining apparatuses according to claims 9, 11, abrasive fluid flows through the passage groove or grooves formed on the conical surface of the insert tool to the injection holes, the entrance corner of each of the injection holes is ground by abrasive fluid concentrically at its corner connecting to the passage groove or grooves, so the entrance corner of the injection hole is rounded large at one side and rounded small at the other side, concave portions of very small depth are formed on conical seat face in the nozzle body, and a nozzle body claimed in claim 14 can be obtained. In actual operation of engines, a large part of fuel flows concentrically from the upstream side entrance corner into the injection hole, so it is very important to be able to round the upstream side entrance corner with a large radius curvature. That is, the entrance corner of the injection hole can be effectively rounded with a large radius of curvature in a region where flow resistance is large for fuel entering the injection hole, and occurrence of cavitation erosion due to occurrence of separation of fuel flow near the needle valve and injection holes is suppressed.
Further, as abrasive fluid flows through the passage groove or grooves, concave portions of very small depth are formed in the conical seat face in the nozzle body extending downstream along generation lines of the conical seat face to the injection holes. That is, the concave portions are formed to reach the injection holes by the most direct way. Therefore, in actual operation of engines, fuel flows to the injection holes easier taking the shortest way, and it is advantageous for increased fuel flow through the injection holes.
According to the injection hole machining methods of claims 4, 6 and according to the injection hole machining apparatuses of claims 10, 12, concave portions of very small depth each of which consists of a straight part and a curved part continuing to the straight part are formed on the conical seat face in the nozzle body in the downstream range from seating position of the conical surface of the needle valve on the conical seat face in the nozzle body in actual operation of engines, and an injection nozzle claimed in claim 15 is obtained. When fuel flows in actual operation of engines, the fuel tends to flow swirling influenced by the concave portions to the injection holes, and atomization of a larger angle of spray can be obtained.
Further, according to the injection hole machining methods of claims 2-4 and according to the injection hole machining apparatuses of claims 8-10, abrasive fluid flowing processing is performed for plural injection holes concurrently while measuring mass flow rate or volume flow rate of abrasive fluid flowing through each of the injection holes independently, processing is stopped for any one of the injection holes when flow rate of abrasive fluid flowing through the relevant injection hole reaches a predetermined value by blocking the relevant injection hole, and processing finished when all of the injection holes are blocked.
By the way, abrasive fluid in the barrel of the abrasive fluid supply section is agitated enough to be homogeneous fluid, so volume flow rate can be converted to mass flow rates imply by multiplying density thereof.
According to the injection hole machining methods of claims 5, 6 and according to the injection hole machining apparatuses of claims 11, 12, the injection holes are processed one by one, so only one processing end detection means is required. Therefore, flow rate of abrasive fluid flowing through each of the injection holes is measured by a single processing end detection means, and variation in flow rate measurement due to variation in accuracy of plural processing end detection means which may occur when performing processing of plural injection holes concurrently is eliminated. So, it is suitable to adopt a method and apparatus with which processing of injection holes is performed one by one when it is required to achieve equalization in flow characteristic rigorously, and to adopt a method and apparatus with which the processing of plural injection holes is performed concurrently and in shorter time period when requirement for exactness of equalization in flow characteristic is not so rigorous.
Number | Date | Country | Kind |
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2006-248979 | Sep 2006 | JP | national |