Valve timing adjusting apparatus

Information

  • Patent Grant
  • 6655332
  • Patent Number
    6,655,332
  • Date Filed
    Friday, February 21, 2003
    21 years ago
  • Date Issued
    Tuesday, December 2, 2003
    20 years ago
Abstract
Upon transmission of a first torque from a first brake portion to a first eccentric shaft, the first eccentric shaft rotates in a retarding direction relative to a rotating member. This causes a first planetary gear to rotate in an advancing direction together with a first output shaft and a driven shaft. Upon transmission of a second torque from a second brake portion to a second eccentric shaft, the second eccentric shaft rotates in a retarding direction relative to the rotating member. This causes a second planetary gear to rotate in the advancing direction together with a second output shaft and the first eccentric shaft, relative to the rotating member, while maintaining rotation in the advancing direction relative to the second eccentric shaft and causes the first planetary gear to rotate in the retarding direction together with the first output shaft and the driven shaft relative to the rotating member.
Description




BACKGROUND OF THE INVENTION




1. Field of the Invention




The present invention relates to a valve timing adjusting apparatus of an internal combustion engine (hereinafter, referred to simply as the engine) for adjusting an opening and closing timing (hereinafter, referred to as the valve timing) of at least one of an exhaust valve and an intake valve of the engine.




2. Description of the Related Art




Conventionally, a valve timing adjusting apparatus for adjusting valve timing of valves is known. Such an apparatus is provided to a transmission system that transmits driving torque of a crankshaft to a camshaft, where the crankshaft serves as an engine driving shaft and the camshaft serves as a driven shaft that opens and closes the exhaust valve or the intake valve of the engine. The valve timing adjusting apparatus adjusts the valve timing by changing a relative rotational phase (hereinafter, referred to simply as the phase) of the camshaft with respect to the crankshaft, thereby enhancing engine output and improving fuel consumption.




An apparatus that changes the phase of the camshaft through the use of oil pressure is one type of valve timing adjusting apparatus. In the case of using oil pressure, however, it is difficult to control a phase change of the camshaft with accuracy when the oil-pressure control conditions are strict, for example, during an operation under low-temperature circumstances, in a period immediately after engine start-up, etc.




In order to eliminate such an inconvenience, Japanese Patent Laid-Open Publication No. Hei. 10-153104 discloses a valve timing adjusting apparatus that changes the phase of the camshaft by making use of an electromagnetic force of an electromagnetic solenoid instead of using oil pressure. This apparatus, however, changes a phase by converting an electromagnetic-induced displacement of a piston member in the axial direction into rotational motions of the camshaft through a helical mechanism. Hence, when a larger width is given to a phase change, a large displacement in the axial direction is experienced by the piston member. This undesirably increases the size of the apparatus. Further, although this apparatus uses an electromagnetic force of the electromagnetic solenoid during an advancing operation that causes a phase change of the camshaft to an advancing side, it uses a biasing force of a biasing member by switching OFF the electromagnetic solenoid during a retarding operation that causes a phase change of the camshaft to a retarding side. This gives rise to a noticeable change in elastic modulus of the biasing member under low-temperature circumstances or the like, and the accuracy of the phase-change control is reduced. Also, because the phase change during the retarding operation depends on a biasing force of the biasing member, there is a limit to improving a response of the phase change. Moreover, energy is lost during the advancing operation for extra work needed to wind a helical spring used as the biasing member.




SUMMARY OF THE INVENTION




The invention therefore has an object to provide a valve timing adjusting apparatus of a compact size, capable of ensuring a width of a phase change of the driven shaft with respect to the driving shaft.




The invention has another object to provide a valve timing adjusting apparatus having an excellent phase change response of the driven shaft with respect to the driving shaft.




The invention has yet another object to provide a valve timing adjusting apparatus capable of constantly and accurately controlling a phase change of the driven shaft with respect to the driving shaft.




According to a valve timing adjusting apparatus of a first aspect of the invention, a first brake portion transmits a first torque to a first eccentric shaft that is off-center from a driven axis. The first eccentric shaft rotates around the driven axis in a direction opposite to the rotational direction of the driven axis. The first eccentric shaft then starts to rotate in a retarding direction relative with respect to a rotating member. Accordingly, a first planetary gear, which is supported on an outside wall of the first eccentric shaft to enable a relative rotation and rotates around the driven axis through engagement with a first internal gear of the rotating member, starts to rotate in an advancing direction together with a first output shaft and the driven shaft engaged therewith relative to the rotating member while rotating in the advancing direction relative to the first eccentric shaft. It is thus possible to change, while the first torque is transmitted, the phase of the driven shaft with respect to the rotating member, that is, the phase of the driven shaft with respect to the driving shaft that rotates the rotating member with driving torque, to an advancing side.




Also, according to the valve timing adjusting apparatus of the first aspect of the invention, a second brake portion transmits a second torque to a second eccentric shaft off-center from the driven axis and rotating around the driving axis, in a direction opposite to the rotational direction thereof. The second eccentric shaft then starts to rotate in the retarding direction relative to the rotating member. Accordingly, a second planetary gear, which is supported on an outside wall of the second eccentric shaft to enable relative rotation and rotation around the driven axis through engagement with a second internal gear of the rotating member, starts to rotate in the advancing direction. The second planetary gear rotates together with a second output shaft and the first eccentric shaft engaged therewith relative to the rotating member while maintaining rotation in the advancing direction relative to the second eccentric shaft. The first planetary gear thus starts to rotate in the retarding direction together with the first output shaft and the driven shaft relative to the rotating member while maintaining rotation in the retarding direction relative to the first eccentric shaft. It is thus possible to change, while the second torque is transmitted, the phase of the driven shaft with respect to the rotating member, that is, the phase of the driven shaft with respect to the driving shaft, to a retarding side.




As has been described, according to the valve timing adjusting apparatus of the first aspect of the invention, a displacement of each of the first and second eccentric shafts, the first and second planetary gears, and the first and second output shafts needed for a phase change of the driven shaft with respect to the driving shaft is obtained from a relative rotation around the driven axis with respect to the rotating member. For this reason, a larger quantity can be secured around the driven axis for the displacement of the foregoing components needed for a phase change of the driven shaft. It is thus possible to reduce the apparatus in size while ensuring a width of a phase change of the driven shaft.




According to a valve timing adjusting apparatus of a second aspect of the invention, one of the rotating member and the first output shaft is provided with a stopper slot that extends arc-wise around the driven axis. Further, the other one of the rotating member and the first output shaft is provided with a stopper protrusion that protrudes into the stopper slot and is allowed to rotate around the driven axis relative to the stopper slot. Hence, by allowing the stopper protrusion to abut against one or the other end portion of the stopper slot, it is possible to limit relative rotations of the first output shaft and the driven shaft with respect to the rotating member. In short, a length of the arc of the stopper slot can limit a width of a phase change of the driven shaft. It is thus possible to set a wider width to a phase change of the driven shaft by forming the stopper slot longer around the driven axis.




According to a valve timing adjusting apparatus of a third aspect of the invention, a first cyclone deceleration mechanism composed of the first internal gear, the first eccentric shaft, the first planetary gear, and the first output shaft, and a second cyclone deceleration mechanism composed of the second internal gear, the second eccentric shaft, the second planetary gear, and the second output shaft are provided adjacently to each other on the driven axis. Hence, the first cyclone deceleration mechanism and the second cyclone deceleration mechanism can be provided so as to superimpose in at least one of a direction parallel to and a direction perpendicular to the driven axis. It is thus possible to reduce the apparatus in size.




According to a valve timing adjusting apparatus of a fourth aspect of the invention, the first torque and the second torque are obtained by making use of electromagnetic forces induced from the first brake portion and the second brake portion, respectively. Hence, because an electromagnetic force is used in either case of causing a phase change of the driven shaft with respect to the driving shaft to the advancing side or to the retarding side, a response of the phase change can be improved. Moreover, by making use of an electromagnetic force that is hardly influenced by operating conditions, such as a surrounding temperature and an elapsed time since the start of the operation, it is possible to constantly and accurately control a phase change of the driven shaft.




According to a valve timing adjusting apparatus of a fifth aspect of the invention, each of the first eccentric shaft and the second eccentric shaft is provided with a function portion fixed thereto so as to rotate together, and each of the first brake portion and the second brake portion includes a solenoid. Also, each of the first torque and the second torque is obtained from a magnetic attraction force induced between the function portion fixed to corresponding one of the first eccentric shaft and the second eccentric shaft, and the solenoid in a switched-ON state included in corresponding one of the first brake portion and the second brake portion. It is thus possible to transmit the first and second torque with a relatively simple arrangement in a reliable manner.




According to a valve timing adjusting apparatus of a sixth aspect of the invention, the solenoid in each of the first brake portion and the second brake portion is provided so as to enable a displacement toward the function portion by the magnetic attraction force and so as to be attracted to the function portion. Because the solenoid is magnetically attracted to the function portion that rotates together with the first or second eccentric shaft, the first or second torque in large magnitude can be readily obtained. Further, each of the first brake portion and the second brake portion is provided with a biasing means for pushing the solenoid in a direction to move apart from the corresponding function portion. This arrangement makes it possible to stop transmission of the first or second torque by releasing the solenoid from the function portion with a biasing force of the biasing means while a magnetic attraction force is lowered by switching OFF the solenoid. As has been described, according to the valve timing adjusting apparatus of the sixth aspect of the invention, it is possible to allow each of the first torque and the second torque to act on their respective function portions only when needed in a sufficiently large magnitude.




According to a valve timing adjusting apparatus of a seventh aspect of the invention, the solenoid in the first brake portion and the solenoid in the second brake portion are formed into cylindrical shapes having different diameters, one of which is provided at an inner radius of the other. It is thus possible to reduce the apparatus in size.




Further areas of applicability of the present invention will become apparent from the detailed description provided hereinafter. It should be understood that the detailed description and specific examples, while indicating the preferred embodiment of the invention, are intended for purposes of illustration only and are not intended to limit the scope of the invention.











BRIEF DESCRIPTION OF THE DRAWINGS




The present invention will become more fully understood from the detailed description and the accompanying drawings, wherein:





FIG. 1

is a cross-sectional view showing one example of a valve timing adjusting apparatus of the invention;





FIG. 2

is a cross-sectional view taken along the line II—II of

FIG. 1

;





FIG. 3

is a cross-sectional view taken along the line III—III of

FIG. 1

; and





FIG. 4

is a cross-sectional view taken along the line IV—IV of FIG.


1


.











DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS




The following description will describe one example of a preferred embodiment of the invention with reference to the accompanying drawings.




FIG.


1


through

FIG. 4

show an example of a valve timing adjusting apparatus for an engine of the invention. A valve timing adjusting apparatus


10


of this example controls the valve timing of an illustrated intake valve of an engine


2


.




The valve timing adjusting apparatus


10


is provided to a transmission system that transmits driving torque of an unillustrated crankshaft of the engine


2


to a camshaft


4


of the engine


2


. As shown in FIG.


2


through

FIG. 4

, the camshaft


4


opens and closes the intake valve of the engine


2


by rotating around its axis (hereinafter, referred to as the cam axis)


0


. The crankshaft and the camshaft


4


of the engine


2


form the driving shaft and the driven shaft, respectively. The valve timing adjusting apparatus


10


includes a housing


11


, and the housing


11


is fixed to the engine


2


through a stay


6


.




A sprocket


12


is supported on the outside walls of the camshaft


4


at one end portion


5


and of a first output shaft


22


at first end portion


23




a


to enable a relative rotation around the cam axis


0


. A chain belt (not shown) is pulled across the sprocket


12


and the crankshaft of the engine


2


. The sprocket


12


rotates around the cam axis


0


with driving torque of the crankshaft transmitted through the chain belt.




A first ring gear


14


and a second ring gear


15


are fixed to the inside wall of the sprocket


12


. Each of the first ring gear


14


and the second ring gear


15


is an internal gear whose top curved surface is present at the inner radius of the bottom curved surface. The first ring gear


14


and the second ring gear


15


are aligned on the cam axis


0


in such a manner that their respective rotational center lines coincide with the cam axis


0


. The first ring gear


14


and the second ring gear


15


are allowed to rotate around the cam axis


0


together with the sprocket


12


. The first ring gear


14


and the second ring gear


15


form a first internal gear and a second internal gear, respectively, and the ring gears


14


and


15


and the sprocket


12


together form a rotating member.




A first transmission shaft


16


is supported on the outside wall of the first output shaft


22


at the second end portion


23


b to enable a relative rotation around the cam axis


0


. A first eccentric shaft


18


, which is off-center with respect to the cam axis


0


, is fixed to the outside wall of the first transmission shaft


16


at one end. Herein, e


1


of

FIG. 2

indicates an eccentric quantity of an axis (hereinafter, referred to as the first eccentric axis) P of the first eccentric shaft


18


with respect to the cam axis


0


. An annular plate of a first function portion


20


using the cam axis


0


as its rotational symmetry axis is provided at the other end of the first transmission shaft


16


. The first transmission shaft


16


, the first eccentric shaft


18


, and the first function portion


20


are all allowed to rotate together around the cam axis


0


.




The first end portion


23




a


of the first output shaft


22


has a lager diameter than the second end portion


23




b


, and the end portion


5


of the camshaft


4


is fit therein concentrically at the inner radius. The first output shaft


22


and the camshaft


4


are fixedly coupled to each other through a fixing bolt


25


screwed from the second end portion


23




b


side of the first output shaft


22


. The first output shaft


22


is allowed to rotate around the cam axis


0


together with the camshaft


4


.




A first planetary gear


30


is provided so as to enable a planetary motion at the outer radius of the center portion of the first output shaft


22


. To be more specific, the first planetary gear


30


is an external gear whose top curved surface is present at the outer radius of the bottom curved surface. The radius of curvature of the top curved surface of the first planetary gear


30


is set smaller than the radius of curvature of the bottom curved surface of the first ring gear


14


, and the number of teeth of the first planetary gear


30


is one less than that of the first ring gear


14


. The first planetary gear


30


is provided with a fitting hole


32


having a circular cross section. The center line of the fitting hole


32


coincides with the rotational center line of the first planetary gear


30


. The first eccentric shaft


18


is fit into the fitting hole


32


through a bearing (not shown), and the first planetary gear


30


is supported on the outside wall of the first eccentric shaft


18


to enable relative rotation around the first eccentric axis P. Here, the first eccentric axis P coincides with the rotational center line of the first planetary gear


30


. When being supported in this manner, part of a plurality of teeth of the first planetary gear


30


engage with part of a plurality of teeth of the first ring gear


14


.




When the first planetary gear


30


is not rotating around the first eccentric axis P relative to the first eccentric shaft


18


, the first planetary gear


30


, together with the sprocket


12


and the first eccentric shaft


18


, rotates around the cam axis


0


while being engaged with the first ring gear


14


without changing the relative positional relationship. In a case where the first eccentric shaft


18


rotates around the cam axis


0


in a retarding direction Y relative to the sprocket


12


while the first planetary gear


30


is rotating as above, the first planetary gear


30


, pressed against by the outside wall of the first eccentric shaft


18


, is activated by the first ring gear


14


engaged with the first planetary gear


30


. Then, the first planetary gear


30


starts to rotate around the first eccentric axis P in an advancing direction X relative to the first eccentric shaft


18


. In this case, the first planetary gear


30


rotates around the cam axis


0


in the advancing direction X relative to the sprocket


12


while being engaged with part of the first ring gear


14


. On the other hand, in a case where the first eccentric shaft


18


rotates around the cam axis


0


in the advancing direction X relative to the sprocket


12


, the first planetary gear


30


, pressed against by the outside wall of the first eccentric shaft


18


, is activated by the first ring gear


14


. Then, the first planetary gear


30


starts to rotate around the first eccentric axis P in the retarding direction Y relative to the first eccentric shaft


18


. In this case, the first planetary gear


30


rotates around the cam axis


0


in the retarding direction Y relative to the sprocket


12


while being engaged with part of the first ring gear


14


.




An annular plate of a first engagement portion


24


, using the cam axis


0


as its rotational symmetry axis, is formed at the center portion of the first output shaft


22


. The first engagement portion


24


is provided with engagement concave portions


26


at more than one point (in this example, nine points). The plurality of engagement concave portions


26


are provided at regular intervals around the cam axis


0


. Each engagement concave portion


26


is a concave portion of the first engagement portion


24


recessed in the plate thickness direction and has a circular cross section, and its opening portion faces the first planetary gear


30


. Meanwhile, the first planetary gear


30


is provided with engagement protrusions


34


corresponding to the engagement concave portions


26


at more than one point on the outside wall that directly opposes the first engagement portion


24


. The plurality of engagement protrusions


34


are provided at regular intervals around the first eccentric axis P off-center from the cam axis


0


by an eccentric quantity e


1


. Each engagement protrusion


34


is shaped like a pin protruding toward the first engagement portion


24


and has a circular cross section, and is inserted into the corresponding engagement concave portion


26


. The outside diameter of each engagement protrusion


34


is set smaller than the inside diameter of the corresponding engagement concave portion


26


.




When the first planetary gear


30


and the sprocket


12


are rotating together, the respective engagement protrusions


34


of the first planetary gear


30


engage with the inner walls of the corresponding engagement concave portions


26


of the first engagement portion


24


, and press the inner walls in the rotational direction (herein, the advancing direction X). The first output shaft


22


and the camshaft


4


fixed thereto thus rotate around the cam axis


0


while maintaining a constant phase relation with respect to the sprocket


12


. In a case where the first planetary gear


30


rotates in the advancing direction X relative to the sprocket


12


while the first output shaft


22


and the camshaft


4


are rotating as above, the respective engagement protrusions


34


further press the inner walls of the engagement concave portions


26


they are engaging with in the rotational direction. This causes the first output shaft


22


and the camshaft


4


to rotate around the cam axis


0


in the advancing direction X relative to the sprocket


12


. On the other hand, in a case where the first planetary gear


30


rotates in the retarding direction Y relative to the sprocket


12


, the respective engagement protrusions


34


press the inner walls of the engagement concave portions


26


they are engaging with in a direction opposite to the rotational direction. This causes the first output shaft


22


and the camshaft


4


to rotate around the cam axis


0


in the retarding direction Y relative to the sprocket


12


.




As shown in FIG.


1


and

FIG. 3

, a stopper slot


35


is formed in the outer edge portion of the first engagement portion


24


of the first output shaft


22


. The stopper slot


35


extends arc-wise about the cam axis


0


in a certain length, and is opened toward the inner wall of the sprocket


12


. A stopper protrusion


37


is formed as an integral part of the inner wall of the sprocket


12


facing the opening portion of the stopper slot


35


. The stopper protrusion


37


protrudes into the stopper slot


35


and extends arc-wise about the cam axis


0


in a length shorter than that of the stopper slot


35


.




When the first output shaft


22


rotates relative to the sprocket


12


, the stopper protrusion


37


rotates relatively around the cam axis


0


within the stopper slot


35


. In this instance, an end portion


38




a


of the stopper protrusion


37


on the retarding direction side abuts against an end portion


36




a


of the stopper slot


35


on the retarding direction side, thereby limiting a relative rotation of the first output shaft


22


in the advancing direction X. The limited position is the maximum advancing position of the first output shaft


22


. Also, when an end portion


38




b


of the stopper protrusion


37


on the advancing direction side abuts against an end portion


36




b


of the stopper slot


35


on the advancing direction side, a relative rotation of the first output shaft


22


in the retarding direction Y is limited. The limited position is the maximum retarding position of the first output shaft


22


. As has been described, in this example, the range of a relative rotation for the first output shaft


22


and hence the camshaft


4


is limited by the length of the arc of each of the stopper slot


35


and the stopper protrusion


37


. For example, by giving a relatively long arc to the stopper slot


35


and a relatively short arc to the stopper protrusion


37


, it is possible to secure a wider range of a relative rotation for the camshaft


4


.




In this example, the first ring gear


14


, the first transmission shaft


16


, the first eccentric shaft


18


, the first function portion


20


, the first output shaft


22


, the first planetary gear


30


, etc. together form a first cyclone deceleration mechanism. A first brake portion


40


is provided in response to the first cyclone deceleration mechanism. The first brake portion


40


includes a first solenoid


42


and a first coil spring


48


as a biasing means.




The first solenoid


42


is formed into a cylindrical shape enclosing a wound coil


43


, and is provided concentrically with the cam axis


0


. The end surface at one end portion of the first solenoid


42


directly opposes a function surface


21


of the first function portion


20


, and a frictional member


45


is fixed thereto. A first supporting shaft


46


protrudes toward the opposite side of the first function portion


20


which is fixed to the second end portion of the first solenoid


42


. The first supporting shaft


46


is supported by the housing


11


to enable a displacement only in the axial direction. This arrangement inhibits the first solenoid


42


from rotating around the cam axis


0


. A first coil spring


48


is disposed between the first supporting shaft


46


and the housing


11


. The first coil spring


48


pushes the first supporting shaft


46


in a direction (direction a of

FIG. 1

) in which the first solenoid


42


moves apart from the first function portion


20


.




The first solenoid


42


is excited when a current passes through the coil


43


, and induces a magnetic attraction force across a space defined by the first solenoid


42


and the first function portion


20


. The magnetic attraction force thus induced causes the first solenoid


42


to be displaced toward the first function portion


20


against a biasing force of the first coil spring


48


, so that the first solenoid


42


is attracted to the first function portion


20


through the frictional member


45


. In a case where the first solenoid


42


is attracted to the first function portion


20


that is rotating, friction between the first function portion


20


and the frictional member


45


produces a first torque in a direction (herein, the retarding direction Y) opposite to the rotational direction of the first function portion


20


. Then, the first torque is transmitted to the first eccentric shaft


18


from the first function portion


20


through the first transmission shaft


16


. Upon transmission of the first torque, the first eccentric shaft


18


starts to rotate around the cam axis


0


in the retarding direction Y relative to the sprocket


12


. On the other hand, the first solenoid


42


in a switched-OFF state is pushed in the direction α of

FIG. 1

by a biasing force of the first coil spring


48


, and is thereby released from the first function portion


20


in a reliable manner.




A second transmission shaft


50


is supported on the outside wall of the first transmission shaft


16


at the center portion to enable relative rotation around the cam axis


0


. A second eccentric shaft


52


, which is off-center with respect to the cam axis


0


, is formed at one end portion of the second transmission shaft


50


. Herein, e


2


of

FIG. 4

indicates an eccentric quantity of an axis (hereinafter, referred to as the second eccentric axis) Q of the second eccentric shaft


52


with respect to the cam axis


0


. An annular plate of a second function portion


54


using the cam axis


0


as its rotational symmetry axis is provided to the center portion of the second transmission shaft


50


. The second transmission shaft


50


, the second eccentric shaft


52


, and the second function portion


54


are allowed to rotate together around the cam axis


0


.




A second output shaft


56


is fixedly coupled and concentric to the outside wall of the first transmission shaft


16


at the center portion. The second output shaft


56


is allowed to rotate around the cam axis


0


together with the first transmission shaft


16


and the first eccentric shaft


18


.




A second planetary gear


64


is provided so as to enable planetary motion at the outer radius of the center portion of the second output shaft


56


. To be more specific, the second planetary gear


64


is an external gear whose top curved surface is present at the outer radius of the bottom curved surface. The radius of curvature of the top curved surface of the second planetary gear


64


is set smaller than the radius of curvature of the bottom curved surface of the second ring gear


15


, and the number of teeth of the second planetary gear


64


is one less than that of the second ring gear


15


. The second planetary gear


64


is provided with a fitting hole


66


having a circular cross section. The center line of the fitting hole


66


coincides with the rotational center line of the second planetary gear


64


. The second eccentric shaft


52


fits into the fitting hole


66


through a bearing (not shown), and the second planetary gear


64


is supported on the outside wall of the second eccentric shaft


52


to enable a relative rotation around the second eccentric axis Q. Here, the second eccentric axis Q coincides with the rotational center line of the second planetary gear


64


. When being supported in this manner, part of a plurality of teeth of the second planetary gear


64


engages with part of a plurality of teeth of the second ring gear


15


.




When the second planetary gear


64


is not rotating around the second eccentric axis Q relative to the second eccentric shaft


52


, the second planetary gear


64


, together with the sprocket


12


and the second eccentric shaft


52


, rotates around the cam axis


0


while being engaged with the second ring gear


15


without changing the relative positional relationship. In a case where the second eccentric shaft


52


rotates around the cam axis


0


in the retarding direction Y relative to the sprocket


12


while the second planetary gear


64


is rotating as above, the second planetary gear


64


, pressed against by the outside wall of the second eccentric shaft


52


, is activated by the second ring gear


15


engaged with the second planetary gear


64


. Then, the second planetary gear


64


starts to rotate around the second eccentric axis Q in the advancing direction X relative to the second eccentric shaft


52


. In this case, the second planetary gear


64


rotates around the cam axis


0


in the advancing direction X relative to the sprocket


12


while being engaged with part of the second ring gear


15


. Herein, an explanation is omitted as to a case where the second eccentric shaft


52


rotates around the cam axis


0


in the advancing direction X relative to the sprocket


12


, because it is not necessary for the description of the invention.




An annular plate of a second engagement portion


60


using the cam axis


0


as its rotational symmetry axis is formed at one end portion of the second output shaft


56


. The second engagement portion


60


is provided with engagement holes


62


at more than one point (in this example, nine points). The plurality of engagement holes


62


are provided at regular intervals around the cam axis


0


. Each engagement hole


62


is a hole penetrating through the second engagement portion


60


in the plate thickness direction and having a circular cross section, and its one opening portion faces the second planetary gear


64


. Meanwhile, the second planetary gear


64


is provided with engagement protrusions


68


corresponding to the engagement holes


62


at more than one point on the outside wall that directly opposes the second engagement portion


60


. The plurality of engagement protrusions


68


are provided at regular intervals around the second eccentric axis Q off-center from the cam axis


0


by an eccentric quantity e


2


. Each engagement protrusion


68


is shaped like a pin protruding toward the second engagement portion


60


and has a circular cross section, and is inserted into the corresponding engagement hole


62


. The outside diameter of each engagement protrusion


68


is set smaller than the inside diameter of the corresponding engagement hole


62


.




When the second planetary gear


64


and the sprocket


12


are rotating together, the respective engagement protrusions


68


of the second planetary gear


64


engage with the inner walls of the corresponding engagement holes


62


of the second engagement portion


60


, and press the inner walls in the rotational direction (herein, the advancing direction X). The second output shaft


56


and the first eccentric shaft


18


coupled thereto through the first transmission shaft


16


thus rotate around the cam axis


0


while maintaining a constant phase relation with respect to the sprocket


12


. In a case where the second planetary gear


64


rotates in the advancing direction X relative to the sprocket


12


while the second output shaft


56


and the first eccentric shaft


18


are rotating as above, the respective engagement protrusions


68


further press the inner walls of the engagement holes


62


they are engaging with in the rotational direction. This causes the second output shaft


56


and the first eccentric shaft


18


to rotate around the cam axis


0


in the advancing direction X relative to the sprocket


12


.




In this example, the second ring gear


15


, the second transmission shaft


50


, the second eccentric shaft


52


, the second function portion


54


, the second output shaft


56


, the second planetary gear


64


, etc. together form a second cyclone deceleration mechanism. As shown in

FIG. 1

, the second cyclone deceleration mechanism and the first cyclone deceleration mechanism are provided adjacent to each other and superimposed in both a direction parallel to and a direction perpendicular to the cam axis


0


. This arrangement reduces the valve timing adjusting apparatus


10


in size.




A second brake portion


70


is provided in response to the second cyclone deceleration mechanism. The second brake portion


70


includes a second solenoid


72


and a second coil spring


78


as a biasing means. The second solenoid


72


is formed into a cylindrical shape enclosing a wound coil


73


, and is provided concentrically with the cam axis


0


. The second solenoid


72


of this example has a larger diameter than the first solenoid


42


, so that part of the first solenoid


42


is inserted at the inner radius of the second solenoid


72


. This arrangement makes it possible to utilize a space at the inner radius of the second solenoid


72


effectively, and the valve timing adjusting apparatus


10


can be thus reduced in size.




The end surface at one end portion of the second solenoid


72


directly opposes a function surface


55


of the second function portion


54


, and a frictional member


75


is fixed thereto. A second supporting shaft


76


protruding toward the opposite side of the second function portion


54


is fixed to the second end portion (far portion) of the second solenoid


72


. The second supporting shaft


76


is supported by the housing


11


to enable a displacement only in the axial direction. This arrangement inhibits the second solenoid


72


from rotating around the cam axis


0


. A second coil spring


78


is disposed between the second supporting shaft


76


and the housing


11


. The second coil spring


78


pushes the second supporting shaft


76


in a direction (direction β of

FIG. 1

) in which the second solenoid


72


is moved apart from the second function portion


54


.




The second solenoid


72


is excited when a current passes through the coil


73


, and induces a magnetic attraction force across a space defined by the second solenoid


72


and the second function portion


54


. The magnetic attraction force thus induced causes the second solenoid


72


to be displaced toward the second function portion


54


against a biasing force of the second coil spring


78


so that the second solenoid


72


is attracted to the second function portion


54


through the frictional member


75


.




In a case where the second solenoid


72


is attracted to the second function portion


54


that is rotating, friction between the second function portion


54


and the frictional member


75


produces a second torque in a direction (herein, the retarding direction Y) opposite to the rotational direction of the second function portion


54


. Then, the second torque is transmitted to the second eccentric shaft


52


from the second function portion


54


through the second transmission shaft


50


. Upon transmission of the second torque, the second eccentric shaft


52


starts to rotate around the cam axis


0


in the retarding direction Y relative to the sprocket


12


. On the other hand, the second solenoid


72


in a switched-OFF state is pushed in the direction β of

FIG. 1

by a biasing force of the second coil spring


78


, and is thereby reliably released from the second function portion


54


.




An operation of the valve timing adjusting apparatus


10


will now be explained. When the crankshaft of the engine


2


is driven to rotate while the first solenoid


42


of the first brake portion


40


and the second solenoid


72


of the second brake portion


70


are both in a switched-OFF state, driving torque of the crankshaft is transmitted to the sprocket


12


. The sprocket


12


and the first and second ring gears


14


and


15


, fixed thereto, then start to rotate together. It should be noted that the phase of the sprocket


12


with respect to the crankshaft is maintained as a constant. In this instance, because the first solenoid


42


in the switched-OFF state is released from the first function portion


20


, the first torque is not transmitted to the first eccentric shaft


18


, and therefore, the first eccentric shaft


18


will not rotate relative to the sprocket


12


. Hence, the first planetary gear


30


and the first eccentric shaft


18


start to rotate together with the sprocket


12


in association with a rotation of the sprocket


12


. The first output shaft


22


and the camshaft


4


engaged with the first planetary gear


30


thus start to rotate at a certain phase with respect to the sprocket


12


.




Also, while the sprocket


12


is rotating, the second solenoid


72


in the switched-OFF state is released from the second function portion


54


, and the second torque is not transmitted to the second eccentric shaft


52


. The second eccentric shaft


52


, therefore, will not rotate relative to the sprocket


12


. Hence, in this instance, the second planetary gear


64


and the second eccentric shaft


52


start to rotate together with the sprocket


12


. The second output shaft


56


engaged with the second planetary gear


64


thus start to rotate together with the first transmission shaft


16


and the first eccentric shaft


18


.




When the first solenoid


42


alone is switched ON while the sprocket


12


is rotating, the first solenoid


42


is magnetic attracted to the first function portion


20


that is rotating Then, the first torque, produced by friction between the frictional member


45


at the end portion of the first solenoid


42


and the first function portion


20


, is transmitted to the first eccentric shaft


18


. Upon receipt of the first torque, the first eccentric shaft


18


starts to rotate in the retarding direction Y relative to the sprocket


12


to decelerate. The first planetary gear


30


is activated by this relative rotation of the first eccentric shaft


18


in the retarding direction Y, and starts to rotate in the advancing direction X relative to the sprocket


12


while maintaining rotation in the advancing direction X relative to the first eccentric shaft


18


. The first output shaft


22


and the camshaft


4


, engaged with the first planetary gear


30


, thus start to rotate in the advancing direction X relative to the sprocket


12


in order to accelerate. In other words, the phase of the camshaft


4


with respect to the sprocket


12


changes to the advancing side, and so does the phase of the camshaft


4


with respect to the crankshaft. The relative rotations of the first output shaft


22


and the camshaft


4


in the advancing direction X are limited by abutment of the stopper protrusion end portion


38




a


against the stopper slot end portion


36




a.






On the other hand, when the second solenoid


72


alone is switched ON while the sprocket


12


is rotating, the second solenoid


72


is magnetically attracted to the second function portion


54


that is rotating, and the second torque produced friction between the frictional member


75


at the end portion of the second solenoid


72


and the second function portion


54


is transmitted to the second eccentric shaft


52


. Upon receipt of the second torque, the second eccentric shaft


52


starts to rotate in the retarding direction Y relative to the sprocket


12


for deceleration. The second planetary gear


64


is activated by this relative rotation of the second eccentric shaft


52


in the retarding direction Y, and starts to rotate in the advancing direction X relative to the sprocket


12


while maintaining rotation in the advancing direction X relative to the second eccentric shaft


52


. The second output shaft


56


and the first eccentric shaft


18


engaged with the second planetary gear


64


thus start to rotate in the advancing direction X relative to the sprocket


12


in order to accelerate.




Continuing, the first planetary gear


30


is activated by this relative rotation of the first eccentric shaft


18


in the advancing direction X, and starts to rotate in the retarding direction Y relative to the sprocket


12


while maintaining rotation in the retarding direction Y relative to the first eccentric shaft


18


. The first output shaft


22


and the camshaft


4


engaged with the first planetary gear


30


thus start to rotate in the retarding direction Y relative to the sprocket


12


in order to decelerate. In other words, the phase of the camshaft


4


with respect to the sprocket


12


changes to the retarding side, and so does the phase of the camshaft


4


with respect to the crankshaft. It should be noted that the relative rotations of the first output shaft


22


and the camshaft


4


in the retarding direction Y are limited by abutment of the stopper protrusion end portion


38




b


against the stopper slot end portion


36




b.






As has been described, according to the valve timing adjusting apparatus


10


, a displacement of each component forming the first cyclone deceleration mechanism and the second cyclone deceleration mechanism is achieved by relative rotations around the cam axis


0


with respect to the sprocket


12


. This makes it possible to secure a wider range of relative rotations around the cam axis


0


for the components forming the first and second cyclone deceleration mechanisms that determine a width of a phase change of the camshaft


4


. It is thus possible to extend a width of a phase change of the camshaft


4


without increasing the apparatus in size.




Further, according to the valve timing adjusting apparatus


10


, in either case of causing a phase change of the camshaft


4


to the advancing side or to the retarding side, the first torque and the second torque that induce the phase change are produced by making use of electromagnetic forces of the first solenoid


42


and the second solenoid


72


, respectively. This improves a response of a phase change, that is, since the first and second solenoids


42


and


72


are switched ON until a phase change of the camshaft


4


takes place. Also, in general, the electromagnetic force is hardly influenced by operating conditions, such as the surrounding temperature of the apparatus and the elapsed time since the start of the operation. It is thus possible to control a phase change of the camshaft


4


with accuracy under low-temperature circumstances or during engine start-up.




Furthermore, according to the valve timing adjusting apparatus


10


, in order to obtain the first torque and the second torque, the first solenoid


42


and the second solenoid


72


are attracted to the first function portion


20


and the second function portion


54


, respectively, that are rotating. For this reason, torque in a large magnitude can be obtained from a small magnetic attraction force. It is thus possible not only to compactly form the first and second solenoid


42


and


72


, but also to reduce a quantity of electricity.




In the example above, both the first brake portion


40


and the second brake portion


70


are arranged to obtain the first torque and the second torque, respectively, by making use of an electromagnetic force. However, it may be arranged in such a manner that at least one of the first torque and the second torque is obtained by, for example, making use of an elastic force of an elastic member. Also, in the example above, the first solenoid


42


and the second solenoid


72


are attracted to the first function portion


20


and the second function portion


54


, respectively. However, they are not necessarily attracted to the corresponding function portions.




Moreover, the example above adopts an arrangement that the first eccentric shaft


18


is constantly coupled to the second output shaft


56


through the first transmission shaft


16


. However, a clutch mechanism or the like such that can release the coupling may be provided somewhere between the first eccentric shaft


18


and the second output shaft


56


.




The description of the invention is merely exemplary in nature and, thus, variations that do not depart from the gist of the invention are intended to be within the scope of the invention. Such variations are not to be regarded as a departure from the spirit and scope of the invention.



Claims
  • 1. A valve timing adjusting apparatus, provided to a transmission system that transmits driving torque of a driving shaft of an internal combustion engine to a driven shaft that opens and closes at least one of an exhaust valve and an intake valve, for adjusting opening and closing timing of at least one of said exhaust valve and said intake valve, said apparatus comprising:a rotating member including a first internal gear and a second internal gear each using a driven axis, which is an axis of said driven shaft, as a rotational center line, and rotating around said driven axis with said driving torque of said driving shaft; a first eccentric shaft off-center with respect to said driven axis and rotating around said driven axis in association with a rotation of said rotating member; a first planetary gear supported on an outside wall of said first eccentric shaft to enable a relative rotation around a first eccentric axis, which is an axis of said first eccentric shaft, and rotating around said driven axis in association with a rotation of said rotating member through engagement with said first internal gear; a first output shaft coupled to said driven shaft that rotates around said driven axis together with said driven shaft in association with a rotation of said first planetary gear through engagement with said first planetary gear; a first brake portion for transmitting a first torque to said first eccentric shaft in a direction opposite to a rotational direction thereof; a second eccentric shaft off-center with respect to said driven axis, which rotates around said driven axis in association with a rotation of said rotating member; a second planetary gear supported on an outside wall of said second eccentric shaft to enable relative rotation around a second eccentric axis, which is an axis of said second eccentric shaft, which rotates around said driven axis in association with a rotation of said rotating member through engagement with said second internal gear; a second output shaft coupled to said first eccentric shaft that rotates around said driven axis together with said first eccentric shaft in association with a rotation of said second planetary gear through engagement with said second planetary gear; and a second brake portion for transmitting a second torque to said second eccentric shaft in a direction opposite to a rotational direction thereof, wherein: upon transmission of said first torque from said first brake portion to said first eccentric shaft while the first eccentric shaft rotates, said first eccentric shaft starts to rotate in a retarding direction relative to said rotating member, which causes said first planetary gear to rotate in an advancing direction together with said first output shaft and said driven shaft relative to said rotating member while maintaining rotation in the advancing direction relative to said first eccentric shaft; and upon transmission of said second torque from said second brake portion to said second eccentric shaft that is rotating, said second eccentric shaft starts to rotate in the retarding direction relative to said rotating member, which causes said second planetary gear to rotate in the advancing direction together with said second output shaft and said first eccentric shaft relative to said rotating member while maintaining rotation in the advancing direction relative to said second eccentric shaft, and causes said first planetary gear to rotate in the retarding direction together with said first output shaft and said driven shaft relative to said rotating member while maintaining rotation in the retarding direction relative to said first eccentric shaft.
  • 2. The valve timing adjusting apparatus according to claim 1, wherein:one of said rotating member and said first output shaft defines a stopper slot that extends arc-wise around said driven axis; and the other one of said rotating member and said first output shaft defines a stopper protrusion that protrudes into said stopper slot and is allowed to rotate around said driven axis relative to said stopper slot.
  • 3. The valve timing adjusting apparatus according to claim 1, wherein a first cyclone deceleration mechanism composed of said first internal gear, said first eccentric shaft, said first planetary gear, and said first output shaft, and a second cyclone deceleration mechanism composed of said second internal gear, said second eccentric shaft, said second planetary gear, and said second output shaft are provided adjacently to each other on said driven axis.
  • 4. The valve timing adjusting apparatus according to claim 2, wherein a first cyclone deceleration mechanism composed of said first internal gear, said first eccentric shaft, said first planetary gear, and said first output shaft, and a second cyclone deceleration mechanism composed of said second internal gear, said second eccentric shaft, said second planetary gear, and said second output shaft are provided adjacently to each other on said driven axis.
  • 5. The valve timing adjusting apparatus according to claim 1, wherein said first torque and said second torque are obtained by making use of electromagnetic forces induced from said first brake portion and said second brake portion, respectively.
  • 6. The valve timing adjusting apparatus according to claim 2, wherein said first torque and said second torque are obtained by making use of electromagnetic forces induced from said first brake portion and said second brake portion, respectively.
  • 7. The valve timing adjusting apparatus according to claim 4, wherein said first torque and said second torque are obtained by making use of electromagnetic forces induced from said first brake portion and said second brake portion, respectively.
  • 8. The valve timing adjusting apparatus according to claim 5, wherein:each of said first eccentric shaft and said second eccentric shaft is provided with a function portion fixed thereto so as to rotate together; each of said first brake portion and said second brake portion includes a solenoid; and each of said first torque and said second torque is obtained from a magnetic attraction force induced between said function portion fixed to one of said first eccentric shaft and said second eccentric shaft, and said solenoid in an ON state included in one of said first brake portion and said second brake portion.
  • 9. The valve timing adjusting apparatus according to claim 8, wherein:said solenoid in each of said first brake portion and said second brake portion is provided so as to enable a displacement toward said function portion by said magnetic attraction force and so as to be attracted to said function portion; and each of said first brake portion and said second brake portion is provided with a biasing means for pushing said solenoid in a direction to move apart from said function portion.
  • 10. The valve timing adjusting apparatus according to claim 8, wherein said solenoid in said first brake portion and said solenoid in said second brake portion are formed into cylindrical shapes having different diameters, one of which is provided at an inner radius of the other.
Priority Claims (1)
Number Date Country Kind
2002-081540 Mar 2002 JP
CROSS REFERENCE TO RELATED APPLICATION

This application is based upon, claims the benefit of priority of, and incorporates by reference the contents of prior Japanese Patent Application No. 2002-81540 filed on Mar. 22, 2002.

US Referenced Citations (3)
Number Name Date Kind
3861243 Fleischer Jan 1975 A
4802376 Stidworthy Feb 1989 A
5040651 Hampton et al. Aug 1991 A
Foreign Referenced Citations (1)
Number Date Country
10-153104 Jun 1998 JP