The present invention relates to vane-type camshaft phasers for varying the phase relationship between crankshafts and camshafts in internal combustion engines; more particularly, to such phasers wherein a locking pin assembly is utilized to lock the phaser rotor with respect to the stator at certain times in the operating cycle; and most particularly, to a phaser that utilizes applied torque between a sprocket and a rotor to assist a lock pin in locking the rotor at a rotational position intermediate between full phaser advance and full phaser retard positions.
Camshaft phasers for varying the phase relationship between the crankshaft and a camshaft of an internal combustion engine are well known. A prior art vane-type phaser 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 supplied via a multiport oil control valve (OCV), in accordance with an engine control module, to either the advance or retard chambers as required to meet current or anticipated engine operating conditions.
In a typical prior art vane-type cam phaser, a controllably variable locking pin is slidingly disposed in a bore in a rotor vane to permit rotational locking of the rotor to a locking pin seat in the stator (or sprocket wheel or pulley) under certain conditions of operation of the phaser and engine. In older prior art phasers, it is desired that the rotor be locked at an extreme of the rotor authority, typically at the full retard position. To assist in positioning the rotor, it is known to incorporate a mechanical stop for the rotor and a torsional bias spring acting between the rotor and the stator to urge the rotor against the stop at the desired position for locking. Such desired position is typically at full phaser retard.
In newer prior art phasers, it is desirable that the rotor be lockable to the stator at an intermediate position in an increased rotor range of rotational authority. A known problem in such phasers is that there is no mechanical means such as a stop to assist in positioning the rotor for locking in an intermediate position; thus, locking is not reliable, and an unacceptably high rate of locking failures may occur.
What is needed in the art of phasers requiring an intermediate lock pin angle is mechanical means to advance the cam timing angle from full retard to align the lock pin with a mid-range pin seat when oil pressure is low.
It is a principal object of the present invention to cause a rotor lock pin to be properly positioned for engagement with a stator at a mid-point of the rotor's range of authority.
Briefly described, a vane-type camshaft phaser in accordance with the invention for varying the timing of combustion valves in an internal combustion engine includes a rotor having a plurality of vanes disposed in a stator having a plurality of lobes, the interspersion of vanes and lobes defining a plurality of alternating valve timing advance and valve timing retard chambers with respect to the engine crankshaft. The rotational authority of the rotor within the stator with respect to top-dead-center of the crankshaft is preferably between about 40 crank degrees before TDC (valve timing advanced) and about 30 crank degrees after TDC (valve timing retarded). It is generally desirable that an engine be started under an intake phaser position of about 10 crank degrees valve retard. Thus, an improved phaser in accordance with the present invention includes a pin seat formed in the stator at the appropriate position of intermediate rotation and a locking pin slidably disposed in a vane of the rotor for engaging the seat to lock the rotor at the intermediate position. An exemplary prior art locking pin means suitable for use in a camshaft phaser in accordance with the invention is disclosed in U.S. Pat. No. 6,948,467, the relevant disclosure of which is incorporated herein by reference.
A toroidal spring disposed on the phaser cover plate is grounded to the stator and is variably grounded to the rotor. When the rotor is moving in a phase-advance direction, at or near the rotor locking position the bias spring becomes disengaged from the rotor, and the rotor thus moves without spring restraint. When the rotor is moving in a phase-retard direction, at or near the rotor locking position the bias spring becomes engaged, causing the rotor to decelerate and thereby increase the reliability of locking at the intermediate position. The phase angle will tend to oscillate about the interemediate position with each torque reversal typical of each valve event. Therefore, the lock pin will pass over its seat with each such oscillation, allowing it to re-engage when lock pin retracting pressure is removed.
The present invention will now be described, by way of example, with reference to the accompanying drawings, in which:
Referring to
Referring now to
In a novel improvement over prior art phaser 10, spring 136 is captured axially by an annular anchor plate 150 having a central opening 152 and a plurality of holes 154 permitting anchor plate 150 to be slidably mounted onto bolt extensions 156. Anchor plate 150 is further provided with a slot 158 for receiving a second axially-extending spring tang 140. Slot 158 is formed such that tang 140 engages a first end of slot 158 corresponding to a full-retard position of rotor 18. Spring 136 may be formed to any convenient degree of spring force and configuration of windings such that when installed between cover plate 128 and anchor plate 150, spring 136 exerts any desired level of force bias against slot 156. Note that in this position, spring 136 is not engaged with rotor 18 and rather is grounded between two elements (bolt head 34 and anchor plate 150) both attached to stator 14. Note further that slot 158 is sufficiently extensive angularly that tang 140 can never engage the opposite end of slot 158 during operational motion of spring 136.
A spring retainer 160 comprises a first flange portion 162 extending radially over anchor plate 150, and a cylindrical portion 164 and second flange portion 166 extending through spring 136 and captured against rotor 18 by an assembly bolt 168. Preferably, spring retainer 160 is rotationally coupled to rotor 18 via pin 170, thereby correctly indexing slot 172 in spring retainer 160 to second spring tang 140 and slot 158.
In rotating with rotor 18, spring retainer 160 is freely rotatable past anchor plate 150. Note that the bias spring is coupled to the rotor via spring retainer 160 only when the rotor is in a retard position. Therefore, the phaser may be assembled without having the spring coupled to the rotor, thereby overcoming a rotor cocking problem inherent in prior art phasers and assuring reliable mounting of an assembled phaser onto a camshaft during engine assembly.
Referring to
While the invention has been described by reference to various specific embodiments, it should be understood that numerous changes may be made within the spirit and scope of the inventive concepts described. Accordingly, it is intended that the invention not be limited to the described embodiments, but will have full scope defined by the language of the following claims.
The present application is a Continuation-In-Part of a pending U.S. patent application Ser. No. 11/447,437, filed Jun. 6, 2006.
Number | Name | Date | Kind |
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6276321 | Lichti et al. | Aug 2001 | B1 |
Number | Date | Country | |
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20070277758 A1 | Dec 2007 | US |
Number | Date | Country | |
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Parent | 11447437 | Jun 2006 | US |
Child | 11639530 | US |