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 an improved locking pin assembly having a fast-acting release.
Camshaft phasers for varying the phase relationship between the crankshaft and a camshaft of an internal combustion engine are well known. In a typical 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 the sprocket, and hence to the stator, under certain conditions of operation of the phaser and engine. A known locking pin mechanism includes a return spring to urge an end of the pin into a hardened seat disposed in the pulley or sprocket (pulley/sprocket) of the phaser, thus locking the rotor with respect to the stator. The rotor may be formed of aluminum, and a steel bushing is pressed and staked into the bore at a predetermined axial location to guide the pin. In at least one prior art embodiment, the pin is shouldered, which shoulder engages the rotor bushing as a limit stop to pin travel. In operation, the pin is forced from the bushing and well in the pulley/sprocket to unlock the rotor from the stator by pressurized oil supplied from a control valve in response to a programmed engine control module (ECM).
A prior art phaser has at least two shortcomings that are overcome by an improved phaser in accordance with the invention.
First, the pin and the seat typically include mating annular bevels to center the pin in the seat and thereby minimize angular lash between the rotor and the sprocket while locked. If the pin is permitted to engage the seat fully, however, the pin may become jammed into the seat and not respond reliably to opening oil pressure. Therefore, a shoulder is provided on the pin to limit travel thereof. It is known that, with repeated use, the pin shoulder can displace the rotor bushing axially, resulting in erratic operation of the locking pin mechanism.
Second, when it is desired to engage the pin to lock the rotor to the sprocket, oil pressure is withheld from the pin end axial face in the well, allowing the spring force to eventually (in milliseconds) overcome the force exerted on the pin end face by the diminishing oil pressure. The force required is proportional to the surface area of the end of the pin. A rapid locking response is benefited by a relatively strong spring (high spring rate); however, in the reverse situation, that of unlocking the pin, a high rate spring results in a relatively slow unlocking response. Hydraulic unlocking force on the pin end is constant but spring resistance increases as the spring is progressively compressed. Thus, the pin initially assumes a relatively high linear velocity which then may slow significantly before the pin is fully withdrawn from the sprocket, resulting in a relatively slow response overall.
What is needed is a means for increasing the withdrawal rate of the locking pin during unlocking of the rotor from the stator/sprocket.
It is a principal object of the present invention to increase the speed of response of a vane-type camshaft phaser in unlocking a rotor from a stator/sprocket.
It is a further object of the invention to increase the locking stability of a rotor-locking mechanism in a vane-type camshaft phaser.
Briefly described, in a rotor-locking mechanism for a vane-type camshaft phaser in accordance with the invention, the locking pin is a straight-sided pin disposed in a bushing in the rotor. The prior art pin shoulder is omitted, permitting the pin to travel without restraint into a well in the sprocket. The pin is urged conventionally into the well by a return spring. A pad partially covering the bottom of the sprocket well is a travel stop for the pin. When the pin is fully seated against the pad, the pad covers a predetermined first portion of the surface area of the end of the pin. A second and uncovered portion of the pin end is exposed to oil pressure for unlocking the pin when it is fully seated. Thus, the pressure area available for unseating the pin is decreased over the prior art pin, permitting use of a lighter locking spring having a lower spring rate.
A principal benefit of the improved configuration is that, as soon as the pin begins to retract in response to oil pressure on the uncovered portion of the pin, the remainder of the pin becomes uncovered, immediately increasing the total hydraulic force on the pin. Because of the lighter locking spring, the pin accelerates more rapidly and unlocks significantly faster than in a comparable prior art phaser.
A secondary benefit is that the reduced surface area of the pin at locking makes it less sensitive to low-pressure variations in oil pressure and accidental unlocking.
The present invention will now be described, by way of example, with reference to the accompanying drawings, in which:
Referring to
A locking bolt mechanism 40 comprises a hollow locking pin 42 and annular shoulder 43, return spring 44, and bushing 46. Spring 44 is disposed inside pin 42, and bushing, pin, and spring are received in a blind, longitudinal bore 48 (shown in phantom view) formed in an oversize vane 22′ of rotor 21, an end portion 45 of pin 42 being extendable by spring 44 from the underside of the vane. A pin guide 47 is disposed in a well 49 formed in pulley/sprocket 12 for receiving end portion 45 of pin 42 when extended from bore 48 to rotationally lock rotor 21 to pulley/sprocket 12 and, hence, stator 16. The axial stroke of pin 42 is limited by interference of shoulder 43 with bushing 46. A shallow channel 51 formed in pulley/sprocket 12 extends from below guide 47 and intersects upper surface 14 in a region of that surface which forms a wall of a selected advance or retard chamber in the assembled phaser. Thus, when oil is supplied to advance the rotor with respect to the stator, oil also flows through channel 51 to bring pressure to bear on the axial face 53 of pin end portion 45, causing the pin to be forced from guide 47 and thereby unlocking the rotor from the stator.
Referring to
In operation, when axial face 53 of pin 42′ is fully seated against pad 62, the pad covers a predetermined covered portion 63 of the surface area of the end portion of the pin. Uncovered portion 65 of the pin end is exposed to oil pressure controllably supplied for unlocking the pin. Thus, the pin end area available initially for unseating the pin is decreased over the prior art pin, permitting use of a lighter locking spring 44′ having a lower spring rate. As noted above, a principal benefit of the improved configuration is that, as soon as the pin begins to retract in response to oil pressure on uncovered portion 65 of the pin, covered portion 63 of the pin becomes uncovered, immediately increasing the total hydraulic force on the pin. Because of the lighter locking spring, the pin accelerates more rapidly and unlocks significantly faster than in prior art phaser 10. The surface area of the pad and the spring constant may be mutually optimized without undue experimentation to provide a desired locking and release performance of the locking pin.
Referring to
Preferably, a pin guide 47′ (omitted for clarity from FIG. 5), similar to pin guide 47 in
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.
Number | Name | Date | Kind |
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5535705 | Eguchi et al. | Jul 1996 | A |
5797361 | Mikame et al. | Aug 1998 | A |
6276322 | Sekiya et al. | Aug 2001 | B1 |
6311655 | Simpson et al. | Nov 2001 | B1 |
6378477 | Fukuhara et al. | Apr 2002 | B1 |
6386164 | Mikame et al. | May 2002 | B1 |
6637390 | Dauer et al. | Oct 2003 | B1 |
Number | Date | Country | |
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20040226527 A1 | Nov 2004 | US |