The present invention relates to a camshaft phaser for varying the phase relationship between a crankshaft and a camshaft in an internal combustion engine; more particularly to such a camshaft phaser which is a vane-type camshaft phaser; still even more particularly to such a camshaft phaser which includes a camshaft phaser attachment bolt which both clamps the camshaft phaser to camshaft and includes a valve spool therein for controlling the flow of oil used to rotate a rotor of the camshaft phaser relative to a stator of the camshaft phaser; and yet even more particularly to such a camshaft phaser which isolates the valve spool from radial inward expansion of the camshaft phaser attachment bolt when the camshaft phaser bolt is tightened to the camshaft.
A typical vane-type camshaft phaser for changing the phase relationship between a crankshaft and a camshaft of an internal combustion engine generally comprises a plurality of outwardly-extending vanes on a rotor interspersed with a plurality of inwardly-extending lobes on a stator, forming alternating advance and retard chambers between the vanes and lobes. Engine oil is selectively supplied to one of the advance and retard chambers and vacated from the other of the advance and retard chambers by a phasing oil control valve in order to rotate the rotor within the stator and thereby change the phase relationship between the camshaft and the crankshaft. Some camshaft phasers incorporate a valve spool within a camshaft phaser attachment bolt which is used to secure the camshaft phaser to the camshaft. The valve spool is moved axially within the camshaft phaser attachment bolt to open and close passages which results in oil being directed to and from the advance and retard chambers as needed in order to rotate the rotor within the stator. The clearance between the valve spool and the camshaft phaser attachment bolt must be minimized in order to control leakage between the corresponding interface; however, the clearance between the valve spool and the camshaft phaser attachment bolt must be sufficiently great to accommodate radially inward expansion of the camshaft phaser attachment bolt when the camshaft phaser attachment bolt is tightened to the camshaft in order to avoid binding of the valve spool within the camshaft phaser attachment bolt. The camshaft phaser attachment bolt may typically expand radially inward by 0.010 mm diametrically with great variability. Consequently, in order accommodate radially inward expansion of camshaft phaser attachment bolt and variability thereof, a larger clearance than desired to minimize leakage may need to be provided in order to ensure proper movement of the valve spool after the camshaft phaser attachment bolt is tightened to the camshaft.
What is needed is camshaft phaser which minimizes or eliminates one or more the shortcomings as set forth above.
Briefly described, a camshaft phaser is provided for use with an internal combustion engine for controllably varying the phase relationship between a crankshaft and a camshaft in the internal combustion engine. The camshaft phaser includes an input member connectable to the crankshaft of the internal combustion engine to provide a fixed ratio of rotation between the input member and the crankshaft; an output member connectable to the camshaft of the internal combustion engine and defining an advance chamber and a retard chamber with the input member; a camshaft phaser attachment bolt which clamps the camshaft phaser to the camshaft, the camshaft phaser attachment bolt having a bolt valve bore extending along an axis, a bolt advance passage providing fluid communication between the advance chamber and the bolt valve bore, and a bolt retard passage providing fluid communication between the retard chamber and the bolt valve bore; a valve sleeve coaxially within the bolt valve bore such that an annular clearance is defined radially between the valve sleeve and the bolt valve bore, the valve sleeve having a sleeve bore, a sleeve advance passage proving fluid communication between the bolt advance passage and the sleeve bore, and a sleeve retard passage providing fluid communication between the bolt retard passage and the sleeve bore; a valve spool within the sleeve bore, the valve spool being displaced axially within the sleeve bore between 1) an advance position which directs oil into the retard chamber and vents oil from the advance chamber, thereby causing the output member to rotate relative to the input member in an advance direction and 2) a retard position which directs oil into the advance chamber and vents oil from the retard chamber, thereby causing the output member to rotate relative to the input member in a retard direction; and a compliant sealing ring radially between the bolt valve bore and the valve sleeve which engages the bolt valve bore and the valve sleeve, the sealing ring preventing fluid communication through the annular clearance axially between opposing axial sides of the sealing ring and the sealing ring also accommodating radially inward expansion of the camshaft phaser attachment bolt within the annular clearance such that the sealing ring isolates the valve sleeve from radial expansion of the camshaft phaser attachment bolt.
Further features and advantages of the invention will appear more clearly on a reading of the following detailed description of the preferred embodiment of the invention, which is given by way of non-limiting example only and with reference to the accompanying drawings.
This invention will be further described with reference to the accompanying drawings in which:
In accordance with a preferred embodiment of this invention and referring to
Camshaft phaser 12 generally includes a stator 18 which acts as an input member, a rotor 20 disposed coaxially within stator 18 which acts as an output member, a back cover 22 closing off one end of stator 18, a front cover 24 closing off the other end of stator 18, a camshaft phaser attachment bolt 26 for attaching camshaft phaser 12 to camshaft 14, a valve sleeve 28 within camshaft phaser attachment bolt 26, and a valve spool 30 within valve sleeve 28. The various elements of camshaft phaser 12 will be described in greater detail in the paragraphs that follow.
Stator 18 is generally cylindrical and includes a plurality of radial chambers 32 defined by a plurality of lobes 34 extending radially inward. In the embodiment shown, there are four lobes 34 defining four radial chambers 32, however, it is to be understood that a different number of lobes 34 may be provided to define radial chambers 32 equal in quantity to the number of lobes 34. Stator 18 may include a sprocket 54 formed integrally therewith or otherwise fixed thereto. Sprocket 54 is configured to be driven by a chain that is driven by the crankshaft of internal combustion engine 10. Alternatively, sprocket 54 may be a pulley driven by a belt or any other known drive member known for driving camshaft phaser 12 by the crankshaft. In an alternative arrangement, sprocket 54 may be integrally formed or otherwise attached to back cover 22 rather than stator 18.
Rotor 20 includes a central hub 36 with a plurality of vanes 38 extending radially outward therefrom and a rotor central through bore 40 extending axially therethrough. The number of vanes 38 is equal to the number of radial chambers 32 provided in stator 18. Rotor 20 is coaxially disposed within stator 18 such that each vane 38 divides each radial chamber 32 into advance chambers 42 and retard chambers 44. The radial tips of lobes 34 are mateable with central hub 36 in order to separate radial chambers 32 from each other. Each of the radial tips of vanes 38 may include one of a plurality of wiper seals 46 to substantially seal adjacent advance chambers 42 and retard chambers 44 from each other. While not shown, each of the radial tips of lobes 34 may also include one of a plurality of wiper seals 46.
Back cover 22 is sealingly secured, using cover bolts 48, to the axial end of stator 18 that is proximal to camshaft 14. Tightening of cover bolts 48 prevents relative rotation between back cover 22 and stator 18. Back cover 22 includes a back cover central bore 52 extending coaxially therethrough. The end of camshaft 14 is received coaxially within back cover central bore 52 such that camshaft 14 is allowed to rotate relative to back cover 22.
Similarly, front cover 24 is sealingly secured, using cover bolts 48, to the axial end of stator 18 that is opposite back cover 22. Cover bolts 48 pass through back cover 22 and stator 18 and threadably engage front cover 24; thereby clamping stator 18 between back cover 22 and front cover 24 to prevent relative rotation between stator 18, back cover 22, and front cover 24. In this way, advance chambers 42 and retard chambers 44 are defined axially between back cover 22 and front cover 24.
Camshaft phaser 12 is attached to camshaft 14 with camshaft phaser attachment bolt 26 which extends coaxially through rotor central through bore 40 of rotor 20 and threadably engages camshaft 14, thereby by clamping rotor 20 securely to camshaft 14. In this way, relative rotation between stator 18 and rotor 20 results in a change is phase or timing between the crankshaft of internal combustion engine 10 and camshaft 14.
Oil is selectively supplied to advance chambers 42 from an oil source 55, for example an oil pump of internal combustion engine 10 which may also provide lubrication to various elements of internal combustion engine 10, in order to cause relative rotation between stator 18 and rotor 20 which results in retarding the timing of camshaft 14 relative to the crankshaft of internal combustion engine 10. When oil is supplied to advance chambers 42 in order to retard the timing of camshaft 14, oil is also vented from retard chambers 44. Conversely, oil is selectively supplied to retard chambers 44 from oil source 55 in order to cause relative rotation between stator 18 and rotor 20 which results in advancing the timing of camshaft 14 relative to the crankshaft of internal combustion engine 10. When oil is supplied to retard chambers 44 in order to advance the timing of camshaft 14, oil is also vented from advance chambers 42. Rotor advance passages 56 may be provided in rotor 20 for supplying and venting oil to and from advance chambers 42 while rotor retard passages 58 may be provided in rotor 20 for supplying and venting oil to and from retard chambers 44. Supplying and venting oil to and from advance chambers 42 and retard chambers 44 is controlled by valve spool 30, as will be described in detail later, such that valve spool 30 is coaxially disposed slidably within a sleeve bore 60, centered about camshaft axis 16, of valve sleeve 28 and such that valve sleeve 28 is disposed coaxially within a bolt valve bore 64, centered about camshaft axis 16, of camshaft phaser attachment bolt 26.
Camshaft phaser attachment bolt 26, valve sleeve 28, and valve spool 30, which act together to function as a valve, will now be described in greater detail with continued reference to
Bolt valve bore 64 preferably includes five sections, each of which has a distinct diameter such that each section is progressively smaller than the previous section from the end of camshaft phaser attachment bolt 26 that is distal from camshaft 14 to the end of camshaft phaser attachment bolt 26 that is proximate to camshaft 14. A bolt valve bore supply section 64a of bolt valve bore 64 is immediately adjacent to bolt supply passage 66. A bolt valve bore sealing section 64b is immediately adjacent to bolt valve bore supply section 64a such that bolt valve bore supply section 64a is between bolt valve bore sealing section 64b and bolt supply passage 66. The transition between bolt valve bore supply section 64a and bolt valve bore sealing section 64b may form a shoulder that is perpendicular to camshaft axis 16 as shown. A bolt valve bore advance section 64c is immediately adjacent to bolt valve bore sealing section 64b such that bolt valve bore sealing section 64b is between bolt valve bore advance section 64c and bolt valve bore supply section 64a. The transition between bolt valve bore advance section 64c and bolt valve bore sealing section 64b is preferably oblique to camshaft axis 16. A bolt valve bore retard section 64d is immediately adjacent to bolt valve bore advance section 64c such that bolt valve bore advance section 64c is between bolt valve bore retard section 64d and bolt valve bore sealing section 64b. The transition between bolt valve bore retard section 64d and bolt valve bore advance section 64c is preferably oblique to camshaft axis 16. A bolt valve bore retention section 64e is immediately adjacent to bolt valve bore retard section 64d such that bolt valve bore retard section 64d is between bolt valve bore retention section 64e and bolt valve bore advance section 64c. The transition between bolt valve bore retention section 64e and bolt valve bore retard section 64d is preferably oblique to camshaft axis 16.
For clarity, it should now be understood that bolt valve bore retard section 64d is smaller in diameter than bolt valve bore retention section 64e, bolt valve bore advance section 64c is smaller in diameter than bolt valve bore retard section 64d, bolt valve bore sealing section 64b is smaller in diameter than bolt valve bore advance section 64c, and bolt valve bore supply section 64a is smaller in diameter than bolt valve bore sealing section 64b.
Camshaft phaser attachment bolt 26 also includes bolt advance passages 78 which extend radially outward from bolt valve bore 64, and more specifically bolt valve bore advance section 64c, to the outer periphery of camshaft phaser attachment bolt 26 such that bolt advance passages 78 are centered about a circular centerline that is perpendicular to camshaft axis 16. Bolt advance passages 78 are aligned with a rotor annular advance groove 80 which extends radially outward from rotor central through bore 40 such that rotor advance passages 56 extend from rotor annular advance groove 80 to advance chambers 42. In this way, fluid communication is provided between bolt valve bore 64 and advance chambers 42.
Camshaft phaser attachment bolt 26 also includes bolt retard passages 82 which extend radially outward from bolt valve bore 64, more specifically bolt valve bore retard section 64d, to the outer periphery of camshaft phaser attachment bolt 26 such that bolt retard passages 82 are centered about a circular centerline that is perpendicular to camshaft axis 16 and such that bolt retard passages 82 are offset from bolt advance passages 78 in the direction of camshaft axis 16 away from camshaft 14. Bolt retard passages 82 are aligned with a rotor annular retard groove 84 which extends radially outward from rotor central through bore 40 such that rotor retard passages 58 extend from rotor annular retard groove 84 to retard chambers 44. In this way, fluid communication is provided between bolt valve bore 64 and retard chambers 44.
Valve sleeve 28 preferably includes four sections, each of which has a distinct external diameter such that each section is progressively smaller than the previous section from the end of the end of valve sleeve 28 that is distal from camshaft 14 to the end of valve sleeve 28 that is proximate to camshaft 14. A sleeve supply section 28a of valve sleeve 28 is provided at the end of valve sleeve 28 that is proximate to bolt supply passage 66. Sleeve supply section 28a is located within bolt valve bore supply section 64a such that an annular space 86 is defined radially between sleeve supply section 28a and bolt valve bore supply section 64a. Annular space 86 provides a diametric clearance which provides supply flow to accommodate the phasing rate of camshaft phaser 12, and by way of non-limiting example only, is a diametric clearance in the range of 1 mm to 3 mm.
A sleeve advance section 28b is immediately adjacent to sleeve supply section 28a and is located partially within bolt valve bore sealing section 64b and partially within bolt valve bore advance section 64c. Sleeve advance section 28b and bolt valve bore sealing section 64b are sized to provide an annular clearance therebetween which accommodates radially inward expansion of camshaft phaser attachment bolt 26 when camshaft phaser attachment bolt 26 is tightened to camshaft 14, i.e. the annular clearance is greater than the extent to which camshaft phaser attachment bolt 26 will expand radially inward. By way of non-limiting example only, the annular clearance between sleeve advance section 28b and bolt valve bore sealing section 64b is at least 0.050 mm and is preferably at least 0.200 mm. As used herein, the annular clearance is defined to be the difference between the two diameters being compared, i.e. diametric clearance. Sleeve advance section 28b defines a first sealing ring groove 88 extending radially inward from sleeve advance section 28b such that first sealing ring groove 88 is annular in shape and centered about camshaft axis 16. A first sealing ring, illustrated as first O-ring 90, is located within first sealing ring groove 88 such that first O-ring 90 is compressed radially between sleeve advance section 28b and bolt valve bore sealing section 64b, thereby preventing oil from migrating from one axial side of first O-ring 90 to the other axial side of first O-ring 90. The oblique nature of the transition between bolt valve bore advance section 64c and bolt valve bore sealing section 64b allows for compression of first O-ring 90 when valve sleeve 28 is inserted into bolt valve bore 64. First O-ring 90 is resilient and compliant and may be, by way of non-limiting example only, an elastomeric or rubber-like material, for example only, Nitrile Butadiene Rubber (NBR), Viton®, or silicone. Consequently, when camshaft phaser attachment bolt 26 is tightened, the radially inward expansion of camshaft phaser attachment bolt 26 is taken up by first O-ring 90, thereby preventing valve sleeve 28 from expanding radially inward.
A sleeve retard section 28c is immediately adjacent to sleeve advance section 28b such that sleeve advance section 28b is located between sleeve retard section 28c and sleeve supply section 28a and such that sleeve retard section 28c is located partially within bolt valve bore advance section 64c and partially within bolt valve bore retard section 64d. Sleeve retard section 28c and bolt valve bore advance section 64c are sized to provide a diametric clearance therebetween which accommodates radially inward expansion of camshaft phaser attachment bolt 26 when camshaft phaser attachment bolt 26 is tightened to camshaft 14, i.e. the diametric clearance is greater than the extent to which camshaft phaser attachment bolt 26 will expand radially inward. By way of non-limiting example only, the diametric clearance between sleeve retard section 28c and bolt valve bore advance section 64c is at least 0.050 mm and is preferably at least 0.200 mm. Sleeve retard section 28c defines a second sealing ring groove 92 extending radially inward from sleeve retard section 28c such that second sealing ring groove 92 is annular in shape and centered about camshaft axis 16. A second sealing ring, illustrated as second O-ring 94, is located within second sealing ring groove 92 such that second O-ring 94 is compressed radially between sleeve retard section 28c and bolt valve bore advance section 64c, thereby preventing oil from migrating from one axial side of second O-ring 94 to the other axial side of second O-ring 94. The oblique nature of the transition between bolt valve bore retard section 64d and bolt valve bore advance section 64c allows for compression of second O-ring 94 when valve sleeve 28 is inserted into bolt valve bore 64. Second O-ring 94 is resilient and compliant and may be, by way of non-limiting example only, an elastomeric or rubber-like material, for example only, Nitrile Butadiene Rubber (NBR), Viton®, or silicone. Consequently, when camshaft phaser attachment bolt 26 is tightened, the radially inward expansion of camshaft phaser attachment bolt 26 is taken up by second O-ring 94, thereby preventing valve sleeve 28 from expanding radially inward.
A sleeve retention section 28d is immediately adjacent to sleeve retard section 28c such that sleeve retard section 28c is located between sleeve retention section 28d and sleeve advance section 28b and such that sleeve retention section 28d is located at least partially within bolt valve bore retard section 64d. Sleeve retention section 28d and bolt valve bore retard section 64d are sized to provide a diametric clearance therebetween which accommodates radially inward expansion of camshaft phaser attachment bolt 26 when camshaft phaser attachment bolt 26 is tightened to camshaft 14, i.e. the diametric clearance is greater than the extent to which camshaft phaser attachment bolt 26 will expand radially inward. By way of non-limiting example only, the diametric clearance between sleeve retention section 28d and bolt valve bore retard section 64d is at least 0.050 mm and is preferably at least 0.200 mm. Sleeve retention section 28d defines a third sealing ring groove 96 extending radially inward from sleeve retention section 28d such that third sealing ring groove 96 is annular in shape and centered about camshaft axis 16. A third sealing ring, illustrated as third O-ring 98, is located within third sealing ring groove 96 such that third O-ring 98 is compressed radially between sleeve retention section 28d and bolt valve bore retard section 64d, thereby preventing oil from migrating from one axial side of third O-ring 98 to the other axial side of third O-ring 98. The oblique nature of the transition between bolt valve bore retention section 64e and bolt valve bore retard section 64d allows for compression of third O-ring 98 when valve sleeve 28 is inserted into bolt valve bore 64. Third O-ring 98 is resilient and compliant and may be, by way of non-limiting example only, an elastomeric or rubber-like material, for example only, Nitrile Butadiene Rubber (NBR), Viton®, or silicone. Consequently, when camshaft phaser attachment bolt 26 is tightened, the radially inward expansion of camshaft phaser attachment bolt 26 is taken up by third O-ring 98, thereby preventing valve sleeve 28 from expanding radially inward.
For clarity, it should now be understood that sleeve retard section 28c is smaller in diameter than sleeve retention section 28d, sleeve advance section 28b is smaller in diameter than sleeve retard section 28c, and sleeve supply section 28a is smaller in diameter than sleeve advance section 28b.
As shown, valve sleeve 28 may be constructed from a single piece of material, and may be preferably made of a metallic material, for example only, steel. Alternatively, valve sleeve 28 may comprise multiple pieces that are assembled to form valve sleeve 28. For example, an inner cylinder of metal may define a portion of sleeve supply passages 102, sleeve advance passages 104, and sleeve retard and passages 106 while an outer member made of plastic material may circumferentially surround the inner cylinder and may define the remaining portions of sleeve supply passages 102, sleeve advance passages 104, sleeve retard and passages 106 and also define first sealing ring groove 88, second sealing ring groove 92, third sealing ring groove 96, sleeve annular advance groove 104a, and sleeve annular retard groove 106a. Forming valve sleeve 28 from multiple pieces may allow the more complicated geometry of valve sleeve 28 to be formed by plastic injection molding rather than more costly and complex machining operations in a metal component.
The axial position of valve sleeve 28 within bolt valve bore 64 is maintained in one axial direction by valve sleeve 28 abutting the shoulder formed by the transition between bolt valve bore sealing section 64b and bolt valve bore supply section 64a and in the other axial direction by a valve retention member 100, illustrated as a snap ring within a snap ring groove of bolt valve bore retention section 64e. In this way, valve sleeve 28 is prevented from moving axially within bolt valve bore 64.
Valve sleeve 28 includes passages extending radially therethrough which permit oil to enter and exit sleeve bore 60 as will now be described. Valve sleeve 28 includes sleeve supply passages 102 in sleeve supply section 28a. Sleeve supply passages 102 extend radially outward from sleeve bore 60 to the outer periphery of sleeve supply section 28a. As shown, sleeve supply passages 102 are preferably slots which each extend circumferentially to a greater extent than they extend axially. Alternatively, supply passages 102 may be a plurality of drilled holes. Sleeve supply passages 102 provide a path for oil to flow into sleeve bore 60 from annular space 86.
Valve sleeve 28 also includes sleeve advance passages 104 in sleeve advance section 28b. Sleeve advance passages 104 extend radially outward from sleeve bore 60 to the outer periphery of sleeve advance section 28b and are aligned with bolt advance passages 78 of camshaft phaser attachment bolt 26. Sleeve advance passages 104 are preferably slots which open into a sleeve annular advance groove 104a on the outer periphery of valve sleeve 28 to ensure that sleeve advance passages 104 are in continuous fluid communication with bolt advance passages 78 regardless of the radial orientation of valve sleeve 28 within bolt valve bore 64. Alternatively, sleeve advance passages 104 may be a plurality of drilled holes. It should be noted that sleeve advance passages 104 are located axially between first O-ring 90 and second O-ring 94.
Valve sleeve 28 also includes sleeve retard passages 106 in sleeve advance section 28b. Sleeve retard passages 106 extend radially outward from sleeve bore 60 to the outer periphery of sleeve retard section 28c and are aligned with bolt retard passages 82 of camshaft phaser attachment bolt 26. Sleeve retard passages 106 are preferably slots which open into a sleeve annular retard groove 106a on the outer periphery of valve sleeve 28 to ensure that sleeve retard passages 106 are in continuous fluid communication with bolt retard passages 82 regardless of the radial orientation of valve sleeve 28 within bolt valve bore 64. Alternatively, sleeve retard passages 106 may be a plurality of drilled holes. It should be noted that sleeve retard passages 106 are located axially between second O-ring 94 and third O-ring 98.
Valve spool 30 is moved axially within sleeve bore 60 of valve sleeve 28 by an actuator 105 and a valve spring 107 to achieve desired operational states of camshaft phaser 12 by opening and closing sleeve advance passages 104 and sleeve retard passages 106. Opening and closing of sleeve advance passages 104 and sleeve retard passages 106 is accomplished by aligning features of valve spool 30, which will be described in the paragraphs that follow, with sleeve advance passages 104 and sleeve retard passages 106.
Valve spool 30 includes a cylindrical outer surface which is interrupted by spool inlet slots 108, spool advance vent slots 110, spool supply slots 112, and spool retard vent slots 114 which are axially separated from each other by lands in the form of continuous annular sections of the cylindrical outer surface of valve spool 30. A spool inlet end land 116 is located at the end of valve spool 30 that is proximal to the closed end of sleeve bore 60. Spool inlet end land 116 is sized to interface with sleeve bore 60 in a close sliding fit such that spool inlet end land 116 is able to slide freely axially within sleeve bore 60 while preventing oil from passing between the interface of spool inlet end land 116 and sleeve bore 60. The diametric clearance between sleeve bore 60 and spool inlet end land 116 is no more than 0.030 mm. Valve spool 30 is retained within sleeve bore 60 by valve retention member 100. More specifically, as illustrated, valve retention member 100 that is embodied as a snap ring includes tabs that extend radially inward to prevent valve spool 30 from coming out of sleeve bore 60.
A spool inlet-advance vent land 118 is spaced axially apart from spool inlet end land 116 such that spool inlet slots 108 are terminated axially by spool inlet end land 116 and spool inlet-advance vent land 118. Spool inlet-advance vent land 118 is sized to interface with sleeve bore 60 in a close sliding fit such that spool inlet-advance vent land 118 is able to slide freely axially within sleeve bore 60 while preventing oil from passing between the interface of spool inlet-advance vent land 118 and sleeve bore 60. The diametric clearance between sleeve bore 60 and spool inlet-advance vent land 118 is no more than 0.030 mm. As shown, there are preferably two spool inlet slots 108 which are diametrically opposed to each other.
A spool supply-advance vent land 120 is spaced axially apart from spool inlet-advance vent land 118 such that spool advance vent slots 110 are terminated axially by spool inlet-advance vent land 118 and spool supply-advance vent land 120. Spool supply-advance vent land 120 is sized to interface with sleeve bore 60 in a close sliding fit such that spool supply-advance vent land 120 is able to slide freely axially within sleeve bore 60 while preventing oil from passing between the interface of spool supply-advance vent land 120 and sleeve bore 60. The diametric clearance between sleeve bore 60 and spool supply-advance vent land 120 is no more than 0.030 mm. As shown, there are preferably two spool advance vent slots 110 which are diametrically opposed to each other. Also as shown, spool advance vent slots 110 are preferably located circumferentially at a position rotated 90° relative to the circumferential location of spool inlet slots 108.
A spool supply-retard vent land 122 is spaced axially apart from spool supply-advance vent land 120 such that spool supply slots 112 are terminated axially by spool supply-advance vent land 120 and spool supply-retard vent land 122. Spool supply-retard vent land 122 is sized to interface with sleeve bore 60 in a close sliding fit such that spool supply-retard vent land 122 is able to slide freely axially within sleeve bore 60 while preventing oil from passing between the interface of spool supply-retard vent land 122 and sleeve bore 60. The diametric clearance between sleeve bore 60 and spool supply-retard vent land 122 is no more than 0.030 mm. As shown, there are preferably two spool supply slots 112 which are diametrically opposed to each other. Also as shown, spool supply slots 112 are preferably located circumferentially at a position rotated 90° relative to the circumferential location of spool advance vent slots 110 which locates spool supply slots 112 at the same circumferential location as spool inlet slots 108.
A spool retard vent-end land 124 is spaced axially apart from spool supply-retard vent land 122 such that spool retard vent slots 114 are terminated axially by spool supply-retard vent land 122 and spool retard vent-end land 124. Spool retard vent-end land 124 is sized to interface with sleeve bore 60 in a close sliding fit such that spool retard vent-end land 124 is able to slide freely axially with sleeve bore 60 while preventing oil from passing between the interface of spool retard vent-end land 124 and sleeve bore 60. The diametric clearance between sleeve bore 60 and spool retard vent-end land 124 is no more than 0.030 mm. As shown, there are preferably two spool retard vent slots 114 which are diametrically opposed to each other. Also as shown, spool retard vent slots 114 are preferably located circumferentially at a position rotated 90° relative to the circumferential location of spool inlet slots 108 which locates spool supply slots 112 at the same circumferential location as spool advance vent slots 110.
Valve spool 30 also includes spool supply passages 126 which extend axially within valve spool 30. Each spool supply passage 126 connects a respective one of spool inlet slots 108 with a respective one of spool supply slots 112. As shown, spool supply passages 126 may be formed by drilling into valve spool 30 from the axial end of valve spool 30 that defines spool retard vent-end land 124 to spool inlet slots 108, then plugging (best shown in
Valve spool 30 also includes spool vent passages 128 which extend axially through valve spool 30, thereby fluidly connecting opposing axial ends of valve spool 30 which define spool inlet end land 116 and spool retard vent-end land 124. Each spool vent passages 128 also fluidly connects a respective one of spool advance vent slots 110 and a respective one of spool retard vent slots 114. It is important to note that spool vent passages 128 do not communicate with spool inlet slots 108 and spool supply slots 112. This arrangement of spool vent passages 128 is made possible by spool inlet slots 108 and spool supply slots 112 being located circumferentially at a position rotated 90° relative to the circumferential location of spool advance vent slots 110 and spool retard vent slots 114. As a result, spool vent passages 128 are each parallel to camshaft axis 16 and spool supply passages 126 are diametrically opposed to each other. It is also important to note that since spool vent passages 128 connect opposing axial ends of valve spool 30, oil cannot leak into, and become trapped in the volume which contains valve spring 107.
Valve spool 30 also includes a spool actuation rod 130 which is centered about camshaft axis 16. Spool actuation rod 130 is engaged by actuator 105 to vary the position of valve spool 30 within sleeve bore 60.
Check valve 76 includes a flat disk portion 76a which selectively covers bolt supply passage 66. More specifically, flat disk portion 76a covers bolt supply passages when the oil pressure within annular space 86 exceeds the pressure of oil supplied by oil source 55. A plurality of biasing arms 76b extend from flat disk portion 76a such that biasing arms 76b first extend radially outward from flat disk portion 76a, then wrap around 180° to be axially spaced apart from, and axially aligned with, flat disk portion 76a. Biasing arms 76b are resilient and compliant such that biasing arms 76b engage the axial end of valve sleeve 28, thereby biasing flat disk portion 76a toward closing with bolt supply passage 66. However, when the pressure differential between annular space 86 and oil source 55 permits, biasing arms 76b are resiliently deflected to allow flat disk portion 76a to be separated from bolt supply passage 66. Check valve 76 may be made of spring steel which is formed by conventional metal bending and stamping techniques. While three biasing arms 76b have been illustrated, it should now be understood that other quantities may be provided. Furthermore, other check valve designs may be used, for example, check valves that use a spring bias ball or conical member that interface with a corresponding seat.
Actuator 105 may be a solenoid actuator that is selectively energized with an electric current of varying magnitude in order to position valve spool 30 within sleeve bore 60 at desired axial positions, thereby controlling oil flow to achieve desired operation of camshaft phaser 12.
In an advance position, when no electric current is supplied to actuator 105 as shown in
In a hold position, when an electric current of a first magnitude is supplied to actuator 105 as shown in
In a retard position, when an electric current of a second magnitude is supplied to actuator 105 as shown in
While camshaft phaser 12 has been described as defaulting to full advance, it should now be understood that camshaft phaser 12 may alternatively default to full retard by simply rearranging oil passages. Similarly, while full advance has been described as full counterclockwise rotation of rotor 20 within stator 18 as shown in
Valve sleeve 28 as described herein allows valve spool 30 to be isolated from radially inward expansion of camshaft phaser attachment bolt 26 when camshaft phaser attachment bolt 26 is tightened to camshaft 14. More specifically, the clearance between valve sleeve 28 and bolt valve bore 64 is sufficiently large to accommodate the radially inward expansion of camshaft phaser attachment bolt 26. Furthermore, the clearance between valve sleeve 28 and bolt valve bore 64 is not relied upon to prevent oil leakage therebetween. Instead, first O-ring 90, second O-ring 94, and third O-ring 98 are used seal between valve sleeve 28 and bolt valve bore 64, thereby ensuring an oil-tight interface. First O-ring 90, second O-ring 94, and third O-ring 98 are each compliant in order to take up the radially inward expansion of camshaft phaser attachment bolt 26 without resulting in radially inward expansion of valve sleeve 28. In this way, the clearance between valve spool 30 and sleeve bore 60 can be minimized to prevent oil leakage at the interface of valve spool 30 and sleeve bore 60 since valve sleeve 28 will not incur radially inward expansion due to camshaft phaser attachment bolt 26 expanding radially inward.
While camshaft phaser 12 has been embodied herein as being actuated by pressurized oil from oil source 55, it should now be understood that camshaft phaser 12 could alternatively be modified to be actuated by using torque reversals of camshaft 14 which alternatingly pressurize oil in advance chambers 42 and retard chambers 44. As in known to those of ordinary skill in the art of camshaft phasers, torque reversals of camshaft 14 can be used to rotate rotor 20 within stator 18 in a controlled manner by inclusion of one or more check valves.
While this invention has been described in terms of preferred embodiments thereof, it is not intended to be so limited, but rather only to the extent set forth in the claims that follow.
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20180058272 A1 | Mar 2018 | US |