The present invention relates to a valve timing control device for an internal combustion engine, which varies and controls the open/close timing of intake or exhaust valves in accordance with a vehicle operation condition.
One known valve timing control device for an internal combustion engine is described in the after-mentioned Patent Document-1.
The known device will be briefly described in the following. The device comprises a housing member that receives a torque from a crankshaft and has therein a plurality of operation oil chambers extending around an inner cylindrical surface of the housing, a front plate that includes a plate part closing at its rear surface a front open part of the housing member and a cylindrical part formed on a central portion of a front surface (outer end surface) of the plate part, a vane rotor that is received in the housing member and rotatable in a given range in both the most delayed angle side and most advanced angle side relative to the housing member and has four vanes for grouping the operation oil chambers into delayed angle operation oil chambers and advanced angle operation oil chambers, and a torsion spring that is partially received in the cylindrical part of the front plate and has one end engaged to a front edge of the cylindrical part and the other end engaged to the vane rotor.
The torsion spring is arranged to bias the vane rotor in the advanced angle side by its biasing force, and by controlling the open/close timing of the exhaust valves in the advanced angle side for improving the engine startability.
Patent Document-1: Japanese Laid-open Patent Application (tokkai) 2012-132404
In the known valve timing control devices such as one mentioned hereinabove, the front open part of the housing member is dosed by the rear surface of the plate part of the front plate for sealing the plurality of operation oil chambers. However, it is difficult to sufficiently increase the accuracy of a side clearance between the rear surface of the plate part of the front plate and a counterface surface of the vane rotor that axially faces the rear surface of the plate part.
That is, when the front plate with the cylindrical part is formed entirely by press-forming, shaping the cylindrical part by applying a burring press to a central portion of the plate part inevitably brings about production of so-called sagging between a base part of the cylindrical part and the central portion of the plate part. With such sagging, a central portion of the rear surface of the plate part is rippled or bent, which may cause deterioration in accuracy of the side clearance and increase leakage of the operation oil from the operation oil chambers.
The present invention is provided by taking the drawback of the known valve timing control devices into consideration and provides a valve timing control device for an internal combustion engine, which is constructed to have a high sealing accuracy by increasing a surface area of a circular central part of the rear surface of the plate part of the front plate.
The invention defined by claim 1 is a valve timing control device for an internal combustion engine, which comprises a housing body to which a torque is transmitted from a crankshaft, at least one of axial ends of the housing body being opened; a vane rotor that includes a rotor fixed to the camshaft, a plurality of vanes provided on the rotor, the vanes being operatively engageable with a plurality of shoes projected from an inner cylindrical surface of the housing body thereby to constitute delayed angle operation chambers and advanced angle operation chambers, the vane rotor being selectively rotated in a delayed angle side or an advanced angle side relative to the housing body in response to charging or discharging of an operation oil to or from the delayed and advanced angle io operation chambers; a front plate including a discal plate part that closes the axial open end of the housing body at its rear surface thereby sealing all of the delayed and advanced angle operation chambers and a cylindrical part that is integrally projected outward from a peripheral edge of a through opening formed in a central portion of the discal plate part; and a torsion spring that has one end engaged to the rotor and the other end engaged to the cylindrical part thereby to constantly bias the vane rotor in one of opposed rotation directions relative to the housing body, the valve timing control device being characterized in that an annular part of a front surface of the plate part near a root portion of the cylindrical part is pressed toward the rear surface of the plate part to produce a recess and during the pressing, an inner area of the rear surface of the plate part, which is placed at a position corresponding to the position where the recess is produced, is supported against the pressing force, so that the annular area and an inner cylindrical surface of the cylindrical part are shaped to have a generally right angled cross section.
According to the invention, the sealing accuracy of the rear surface of the plate part can be increased by increasing a surface area of the circular central part of the rear surface of the plate part by suppressing production of the sagging at the circular central part of the rear surface of the plate part. As a result, undesired leakage of the operation oil from the operation oil chambers can be suppressed.
In the following, an embodiment of the valve timing control device for an internal combustion engine according to the present invention will be described in detail with reference to the accompanying drawings. In the illustrated embodiment, there is employed a type in which the control device is applied to a valve actuating device for exhaust valves.
As is seen from
The sprocket 1 is made of an iron-based metal and shaped like a thicker disc, and has on a periphery thereof a gear portion 1a around which the above-mentioned timing chain is wound, and has at a central portion thereof a supporting opening 1b through which an outer cylindrical surface of the camshaft 2 is rotatably supported. Furthermore, the sprocket 1 is formed at four equally spaced radially outer portions thereof with respective internally threaded openings lc to which after-mentioned four bolts 9 are engaged. The sprocket 1 can serve as a rear cover that closes a rear opening of an after-mentioned housing 5.
The camshaft 2 is rotatably supported by a cylinder head (not shown) through camshaft bearings and integrally formed at given axial portions thereof with egg-shaped cams for making open/close operation of the exhaust valves, and the camshaft 2 is formed at one axial end 2a thereof with a bolt inserting hole 2b into which a shaft portion 6a of a cam bolt 6 is inserted in an axial direction to fix an after-mentioned vane rotor 7 to the camshaft 2. A leading end of the bolt inserting hole 2b is formed with an internal thread (not shown) to which an external thread formed on a leading end of the cam bolt 6 is engaged.
As is seen from
The housing 5 comprises the cylindrical housing body 5a that is made of a sintered metal, a front plate 12 that closes a front opening of the housing body 5a, and the sprocket 1 that closes a rear opening of the housing body 5a to serve as a rear cover. The housing body 5a, the front plate 12 and the sprocket 1 are tightly joined together by the four bolts 9 that pass through bolt openings 8e respectively formed in the shoes 8a to 8d.
The front plate 12 is integrally produced by pressing a carbon steel plate with a press machine and a specialized press method, and as is seen from
The plate part 13 is formed at a central part thereof with a relatively large through opening 13a that forms a part of the cylindrical part 14, and to a hole edge of the through opening 13a provided at a front surface 13d, there is integrally connected the cylindrical part 14. That is, the cylindrical part 14 is projected forward from a rear surface side 13e of the plate part 13 while being bent, and an inner diameter of the through opening 13a is the same as that of an inner cylindrical surface 14a of the cylindrical part 14, and the through opening 13a and the cylindrical part 13 are coaxially and continuously connected.
The plate part 13 is formed at equally spaced four peripheral portions thereof with respective bolt openings 13b through which the bolts 9 pass, and each bolt opening 13b is formed, at a hole edge thereof on the front surface 13d, with a tapered annular recess with which a base part of the shaft of the bolt 9 is engaged. Furthermore, around the tapered annular recess of each bolt opening, there is formed an annular seat surface 13c onto which a rear surface of a head 9a of the bolt 9 is seated.
The cylindrical part 14 is projected forward from the front surface 13d of the plate part 13 by a given distance, and a leading end 14b of the cylindrical part 14 has a tapered surface 14c the vertical section of which is circular-arc in shape, and the cylindrical part 14 is provided with a circular-arc shaped cut 14d at a position that corresponds to a position taken by an after-mentioned widest first vane 18a when it is turned in a circumferential direction within a given range. The cylindrical part 14 is further provided at a circumferentially opposed end of the cut 14d with a first spring engaging groove 14e that is an engaging portion.
As is seen from
As is seen from
As is seen from
That is, by pressing a root portion of the cylindrical part 14 relative to the plate part 13 toward the rear surface side 13e by an after-mentioned pressing punch, there is produced an annular recess 16 around an annular area of the front surface 13d of the plate part 13. During this pressing, the rear surface 13e of the plate part 13 is entirely supported by an after-mentioned cylindrical supporting tool 41 against the pressing force.
With the above-mentioned process, an annular area 13f of the rear surface 13e is pressed or shifted toward the axis of cylindrical part 14 (viz., in the direction of the arrow of
Although the above-mentioned annular recess 16 is of an endless type provided around the outer surface of the root of the cylindrical part 14, the annular recess 16 is not always necessary to extend entirely around the root. That is, the annular recess 16 may have a cut portion or cut portions in the entire length.
The vane rotor 7 is integrally constructed of for example a sintered metal, and as is seen from
The rotor 17 is shaped generally cylindrical and has at a radially outer part of a front surface of the rotor an annular groove 17a and at a rear surface of the rotor a circular engaging bore 17b to which a leading end 2b of the camshaft 2 is tightly engaged. An inner surface of the annular groove 17b is formed with a second spring engaging groove 17c that extends (radially) toward the axis of the bolt inserting bore 7a.
As is seen from
While, as is seen from
The first vane 18a in the vanes 18a to 18d is shaped like a fan with a largest width when viewed from the side and has the largest weight, and the three vanes 18b to 18d other than the first vane 18a have each a width smaller than that of the first vane 18a. Because the first vane 18a is largest in weight, the center Y of gravity (viz., the oval illustrated by hatched line) of the vane rotor 7 is placed at a position shifted toward the first vane 18a from the center point P1.
As will be understood from the dot-dash line of
During the above-mentioned movement of the vane rotor, the second to fourth vanes 18b to 18d are kept away from their opposing surfaces of the shoes 8c and 8d without contacting the same. Accordingly, a so-called contact accuracy between the first vane 18a and each of the first and second shoes 8a and 8b is increased and since the speed in feeding the hydraulic pressure to the delayed and advanced angle hydraulic chambers 10 and 11 is increased, the rotation responsiveness of the vane rotor 7 in normal and reverse directions is increased.
The delayed angle hydraulic chambers 10 and the advanced angle hydraulic chambers 11 are respectively connected to the hydraulic circuit 4 through first and second connecting holes 10a and 11a that extend in the rotor 17 in radial direction.
The hydraulic circuit 4 is a circuit that selectively feeds or discharges the hydraulic oil to or from the delayed and to advanced angle hydraulic chambers 10 and 11, and as is seen from
The delayed angle oil passage 19 and the advanced angle oil passage 20 have respective ends connected to passage ports of the electromagnetic switch valve 22, and the other ends of the passages 19 and 20 are connected through a cylinder head (not shown) and a cylinder block (not shown) to an interior of the camshaft 2 constituting delayed and advanced angle passage portions 19a and 20a that extend axially in parallel with each other.
The delayed angle passage portion 19a is connected to the delayed angle hydraulic chambers 10 through the first connecting holes 10a, and the advanced angle passage portion 20a is connected to the advanced angle hydraulic chambers 11 through the connecting holes 11a.
As is seen from
An intake passage 21b of the oil pump 21 and the drain passage 23 are connected to interior of an oil pan 24. The discharge passage 21a of the oil pump 21 has at its downstream portion a filtration filter 25 and is connected at the downstream portion to a main oil gallery M/G that feeds the oil to mutually sliding and contacting portions of the internal combustion engine. The oil pump 21 is equipped with a flow rate control valve 26 that controls the oil discharged from the discharge passage 21a to a suitable amount by discharging an excessive part of the oil to the oil pan 24.
The electronic controller is equipped with a computer which, by receiving information signals from a crank angle sensor (not shown), an air flow meter, an engine cooling water temperature sensor, a throttle valve open degree sensor, and a cam angle sensor that detects a current rotation phase of the camshaft, estimates the current operation condition of the engine, and by outputting a control pulse signal to an electromagnetic coil of the electromagnetic switch valve 22, controls the shift position of a spool valve of the electromagnetic switch valve 22 thereby to carry out a desired switching of the above-mentioned passages.
Between the first vane 18a and a rear cover 1b of the sprocket 1, there is arranged a lock mechanism that is able to lock the vane rotor 7 at the most advanced angle position relative to the housing 5.
As is seen from
The lock pin 28 with the leading end 28a is entirely shaped cylindrical so that engagement of the lock pin 28 with the lock opening 29 in the axial direction is easily made, and a coil spring 30 is provided and compressed between a bottom of an axially extending bore formed in the lock pin 28 and the rear surface 13e of the front plate 12 for biasing the lock pin 28 in a projecting direction (viz., the direction for establishing the engagement).
The lock opening 29 is sized larger in diameter than the leading end portion of the lock pin 28 and placed at a position circumferentially eccentric toward the advanced angle hydraulic chamber 11, so that upon engagement with the lock pin 28, a relative converting angle between the housing 5 and the vane rotor 7 takes a value that corresponds to the most advanced angle position. At a side portion of the lock opening 29, that is, at a position that is one stage lower than the position of the lock opening 29, there is formed a circular-arc shaped pressure receiving chamber 31 that is smaller in diameter than the lock pin 28.
The engaging/disengaging mechanism comprises the above-mentioned coil spring 30 that biases the lock pin 28 in the projecting direction, and a disengagement hydraulic circuit (not shown) that feeds the pressure receiving chamber 31 with a hydraulic pressure to move back the lock pin 28. In the disengagement hydraulic circuit, there is arranged a system by which the hydraulic pressure selectively fed to the delayed and advanced angle hydraulic chambers 10 and 11 is led to the pressure receiving chamber 31 through given oil holes for moving or biasing the lock pin 28 in a backward direction.
Within a space defined by the plate part 13, the cylindrical part 14 and the annular groove 17a of the rotor 17, to there is installed a torsion spring 32 that biases the vane rotor 7 in a timing advancing direction relative to the housing 5.
As is seen from
The coiled spring body part is almost entirely received in the through opening 13a and the cylindrical part 14, and an axially inside part of the spring body part is received and arranged in the annular groove 17a of the rotor 17.
The second engaging end portion 32b is engaged to the first spring engaging groove 14e from a circumferential direction and the second engaging end portion 32b is engaged and fixed to the second spring engaging groove 17c of the rotor 17 from an axial direction. Due to the spring force of the torsion spring 32, the vane rotor 7 is constantly biased to rotate in a timing advancing direction.
The torsion spring 32 is constructed to reduce its diameter when the vane rotor 7 is turned in a timing delaying direction relative to the housing 5.
[Method for Producing the Front Plate]
The front plate 12 is produced by carrying out a series of press forming steps depicted by
First, as is seen from
Then, as is seen from
Then, as will be understood from
Then, with the above-mentioned condition being kept, by using a press punch 42 arranged around the supporting tool 41, an outer cylindrical wall 14j of the root of the cylindrical part 14′ is pressed downward as is indicated by the arrows. As is seen from the drawing provided at a right side of
That is, when the pressing force for forming the annular recess 16 is applied to the given portion, the inner cylindrical portion of the plate part 13′ and the root area part of the cylindrical part 14′ are pressed radially inward. During this pressing, the inner cylindrical surface 14a′ of the root portion of the cylindrical part 14′ and an inner cylindrical surface of the plate part 13′ near a through opening 13a′ are intimately supported by an outer cylindrical surface of the supporting tool 41 and an upper surface of the mounting base 40 near the inserting hole 40a against the pressing force.
Accordingly, the material of the plate part 13 placed around the through opening 13a′ is shifted in the direction of the arrow of
Then, as is seen from
Then, the base metal 12′ for the front plate 12 is subjected to a heat treatment at a given temperature for a give time, and then, as is seen from
Then, the rear surface 13e of the plate part 13 and the leading end surface 14b of the cylindrical part 14 are put between front and rear polishing devices 44a and 44b to carry out a so-called double disc polishing. With this polishing, the rear surface 13e can have a high surface roughness for increasing a side clearance accuracy between it and the above-mentioned roller 17.
With the above-mentioned steps, a series of forming work for forming the front plate 12 is completed.
[Operation Effects of the Valve Timing Control Device of the Embodiment]
As is seen from
When, after the engine starting, the engine is operated in a low speed load range, de-energization of the electromagnetic coil of the electromagnetic switching valve 22 is kept by the electronic controller. With this, connection between an exhaust passage 18a of the oil pump 21 and the delayed angle oil passage 19 is established and connection between the advanced angle oil passage 20 and the drain passage 23 is established.
Thus, the operation oil discharged from the oil pump 21 is led into the delayed angle hydraulic chambers 10 through the delayed angle oil passage 19 causing the delayed angle hydraulic chambers 10 to show a higher pressure, and at the is same time, the operation oil in the advanced angle hydraulic chambers 11 is led into the oil pan 22 through the advanced angle oil passage 20 and the drain passage 23 causing the advanced angle hydraulic chambers 11 to show a lower pressure.
At this time, the operation oil led into the delayed angle hydraulic chambers 10 is led into both the pressure receiving chamber 31 and the lock opening 29 through the above-mentioned disengagement hydraulic circuit thereby causing the chamber 31 and the lock opening 29 to have a higher pressure, and thus, the lock pin 28 is moved back to disengage the leading end 28a from the lock opening 29 resulting in a free rotation of the vane rotor 7.
Accordingly, in accordance with increase of the volume of the delayed angle hydraulic chambers 10, the vane rotator 7 is turned left in the drawing (viz., in the delayed angle direction) as is indicated by a dot-dash line in
Due to rotation of the vane rotor 7 in the delayed angle side relative to the housing 5, the torsion spring 32 is deformed in a diameter reducing direction.
When, then, the engine operation is shifted for example to a high rotation load range, a control current is outputted to the electromagnetic switch valve 22 from the to electronic controller, so that the discharge passage 21a is connected to the advanced angle oil passage 20 and at the same time the delayed angle oil passage 19 is connected to the drain passage 23. With such connection, the operation oil in the delayed angle hydraulic chambers 10 is discharged thereby to cause the chambers 10 to show a lower pressure, and the operation oil is led into the advanced angle hydraulic chambers 11 thereby to cause the chambers 11 to show a higher pressure. During this, due to the flow of the operation oil from the advanced angle hydraulic chambers 11 to the pressure receiving chamber 31 through the above-mentioned disengagement hydraulic circuit, the lock pin 28 is disengaged from the lock opening 29 and keeps the disengaged condition.
Accordingly, as is indicated by the solid line in
At a time just before stopping the engine, the operation oil in the hydraulic chambers 10 and 11 is discharged to the oil pan 22 through the drain passage 23, and thus, the hydraulic pressure in both the pressure receiving chamber 29 and the lock opening 29 is lowered too. Thus, due to the spring force of the torsion spring 32a applied to the camshaft 2, the vane rotor 7 is turned toward the most advanced angle side and due to spring force of the coil spring 30, the lock pin 28 is projected causing its leading end 28a to engaged with the lock opening 29.
Since a relative positioning in a circumferential direction of the housing between the lock pin 28 and the lock opening 29 is assuredly made at the time of assembling the parts, the engagement of the lock pin 28 with the lock opening 29 is smoothly achieved.
Furthermore, since, in the embodiment, the front plate 12 is integrally produced by pressing a relatively thin iron-based metal plate via press forming, a light-weight production of the front plate is assuredly possible and the work for manufacturing the front plate is simple, which can bring about a zo cost reduction.
Furthermore, in the embodiment, for formation of the annular recess 16 on the inner cylindrical part of the front surface 13d of the plate part 13, the root portion of the cylindrical part 14 is pressed by the press punch 42, so that the annular area 13f of the rear surface 13e is shaped to have a right angled cross section increasing its inner outer surface area. With this feature, the sagging is eliminated and thus a sealing surface can be increased, and thus, the sealing accuracy of the side clearance between the plate part and the axially other end surface of the rotor 17 can be sufficiently increased.
Since enlargement of the outer surface area of the annular area 13f of the rear surface 13e is carried out by co-operation work between the press punch 42 and the supporting tool 41 not by abrasive machining, the forming cost can be reduced.
Furthermore, since the inside edge of the first spring engaging groove 14e is shaped to have the arc surface 14g, damages that would appear on the outer surface of the first engaging end portion 32a of the torsion spring 32 when the first engaging end portion 32a is kept engaged with the first spring engaging groove 14e can be eliminated.
Furthermore, because of provision of the tapered to annular surface 13h between the inside hole edge 13g of the annular area 13f and the inner cylindrical surface 14a of the cylindrical part 14, the deformation of the torsion spring 32 in a diameter expanding direction can be neatly received by a space defined by the tapered annular surface 13h, and thus, a is smoothed deformation of the torsion spring 32 is achieved.
Furthermore, due to provision of the space, interference of the outer surface of the torsion spring 32 with the inner cylindrical surface 14a of the cylindrical part 14 is suppressed and thus, damages of the outer surface of the torsion spring and generation of noises can be suppressed.
Furthermore, since the annular seat surface 13c of the plate part 13 is formed also by the press forming, cost can be reduced as compared with that in the abrasive machining.
Furthermore, in the embodiment, due to provision of the widest first vane 18a of the vane rotor 7, the center of gravity of the vane rotor is offset to the side of the first vane 18a, and at the same time due to provision of the cut 14d and the first spring engaging groove 14e of the cylindrical part 14, the center of gravity of the front plate 12 is offset to one side that is opposite to the other side where the cut 14d and the first spring engaging groove 14e are provided, and thus, an excessive weight caused by the first vane 18a is cancelled.
Accordingly, a weight balancing in entire construction of the valve timing control device is sufficiently achieved without providing the third vane 18c with a balancing weight or the like that is positioned opposite to the position where the first vane 18a is provided, and due to provision of the cut 14d and the first spring engaging groove 14e, light weighting of the device is obtained.
It is to be noted that the present invention is not limited to the construction of the above-mentioned embodiment. That is, the construction is changeable within the concept of the invention.
Number | Date | Country | Kind |
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2013-255530 | Dec 2013 | JP | national |
Filing Document | Filing Date | Country | Kind |
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PCT/JP2014/079800 | 11/11/2014 | WO | 00 |