1. Field of the Invention
The invention pertains to the field of variable cam timing systems. More particularly, the invention pertains to a variable cam timing system including a phaser with concentric cams.
2. Description of Related Art
US Published Application No. US 2005/0279302 discloses a vane-type phaser driven by a crankshaft that drives the inner shaft and the outer tube of a first single cam phaser camshaft, which is coupled for rotation with the inner shaft and the outer tube of a second single cam phaser camshaft by drive links. The drive links are meshing gearwheels. The phaser may alter both the inner shafts and outer tubes of both camshafts or individual single vane-type phasers may each transmit torque to the first and second camshafts.
The first and second camshafts each have cams formed directly on the two inner shafts and other cams formed on the two outer tubes. Cams that rotate with the outer tubes have collars coupled to the outer tube by heat shrinking and cams that rotate with the inner shaft are loose fit on the outer tube and are connected to the inner shaft by pins that pass through the circumferentially elongated slots in the outer tube.
U.S. Pat. No. 7,036,473 discloses an adjustable camshaft with an elongated shaft which includes multiple shaft sections carrying intake and/or exhaust cam lobes. The first shaft section includes a shaft extending therefrom, and the second shaft section includes a hollow sleeve extending therefrom to accept the shaft therein to rotatably associate the first shaft section with the second shaft section. With the first and second shaft sections rotatably associated with each other, the sections may be selectively rotated relative to each other in order to adjust a displacement angle between the cam lobes to alter the intake and exhaust timing. The elongated shaft is attached to a drive/timing gear assembly which includes a gear and hub. An inner shaft may extend through the elongated shaft for attachment to the engine block. The cams may be locked to the shaft and relative to one another by a locking nut or a pin.
An assembly for an engine comprising at least one phaser and a camshaft assembly.
The phaser has a housing, a rotor and a control valve. The housing has an outer circumference for accepting drive force. The rotor is coaxially located within the housing. Both the housing and the rotor define at least one vane that separates a chamber in the housing into advance and retard chambers. The vane is capable of rotation to shift the relative angular position of the housing and the rotor. The control valve is received within a bore in the rotor for directing fluid to the chambers.
The camshaft assembly has an outer camshaft piece and an inner camshaft piece. The outer camshaft piece includes an outside cam integrally attached to the housing of the phaser through a middle portion. The outer camshaft piece also defines a hollow extending a length. The inner camshaft piece includes an inner cam adjacent to the outer cam. A tube portion extends from a first side of the inner cam and is received by the hollow of the outer camshaft piece, connecting the inner cam to the rotor of the phaser. A shaft portion extends to an end portion from the other side of the outer cam. A passage, connected to an inlet line is present within the inner camshaft piece, directing fluid to the control valve of the phaser.
When the rotor of the phaser moves, the inner cam is phased relative to the outer cam, allowing duration of a valve event to be increased or decreased.
In another embodiment, two phasers are used with the camshaft assembly.
The phasers may be cam torque actuated, oil pressure actuated, torsion assist, or hybrid.
Internal combustion engines have employed various mechanisms to vary the angle between the camshaft and the crankshaft for improved engine performance or reduced emissions. The majority of these variable camshaft timing (VCT) mechanism use one or more “vane phasers” on the engine camshaft 26 (or camshafts, in a multiple-camshaft engine). In most cases, the phasers 25 have a rotor 10 with one or more vanes, mounted to the end of the camshaft 26, surrounded by a housing 8 with the vane chambers 9 into which the vanes 11a 11b, 11c fit, dividing the vane chambers 9 into advance and retard chambers 15, 17. It is possible to have the vanes 11 mounted to the housing 8, and the chambers 9 in the rotor 10, as well. The a portion of the housing's 8 outer circumference 4c forms the sprocket, pulley or gear accepting drive force through a chain, belt, or gears, usually from the crankshaft, or possible from another camshaft in a multiple-cam engine.
Referring to
Adjacent to the outside cam 4a is an inner cam 6a. By having the inside and outside cams 4a, 6a inline next to each other, the roller 28 of the lifter 29 is able to ride on both lobes of the cams 4a, 6a at the same time. The inner cam 6a is integral with a tube 6b on one end that is received within the hollow 5 of the first camshaft piece 40 and is connected to the rotor 10 of the phaser 25 coaxially located within the housing 8. The rotor 10 has a plurality of vanes 11a, 11b, 11c that separate chambers 9 formed between the housing 8 and the rotor 10 into advance chambers and retard chambers 15, 17. Opposite the inner tube portion 6b, on the other side of the inner cam 6a is a shaft portion 6c with an end piece 6d larger than the diameter of the first camshaft piece 40 and the inner tube portion 6b and shaft portion 6c. The end piece 6d on the shaft portion 6c prevents the second camshaft piece or inner camshaft piece 60 comprised of the inner cam, 6a, the inner tube portion 6b, shaft portion 6c, and the end piece 6d, from dislodging from the assembly. The shaft portion 6c, not including the end piece 6d is surrounded by a second bearing 18. A passage 20b is present along the length of the second camshaft piece or inner camshaft piece 60 to supply fluid from the inlet line 20a to the phaser. Line 22 supplies oil to feed the cam bearing. The passage 20b provides fluid to the advance and retard chambers 15, 17 through a control valve 14 with in a bore 3 in the rotor 10. The control valve 14 controls the flow of fluid to the advance and retard chambers 15, 17 and the position of the rotor 10 relative to the housing 8. The position of the control valve 14 is influenced by an actuator 12. The actuator shown in
As the rotor 10 moves, the inner cam 6a is phased relative to the fixed outer cam 4a, allowing duration of the valve event to be increased or decreased. By varying the duration of the valve event, the valve opening or closing ramps are varied. Since the cam bearings 16, 18 in the head are used to support the inner camshaft piece 40 and the outer camshaft piece 60, no bearings are required in the outer camshaft piece 60 to support the inner camshaft piece 40. By not having any bearings internal to the outer cam 4a, the base circle runout is dictated by the cam bearing clearance in the head.
As the rotor 10 moves, the inner cam 6a is phased relative to the outer camshaft piece 40, allowing duration of the valve event to be increased or decreased. By varying the duration of the valve event, the valve opening or closing ramps are varied. Since the cam bearings 16, 18 in the head are used to support the inner camshaft piece 40 and the outer camshaft piece 60, no bearings are required in the outer camshaft piece 60 to support the inner camshaft piece 40. By not having any bearings internal to the outer cam 4a, the base circle runout is dictated by the cam bearing clearance in the head.
Both the inner and outer cams 6a, 4a have a phaser 125, 25 attached to them allowing both cams 6a, 4a to be phased relative to each other. The outside cam 4a is integrally attached to a middle tubular portion 4b that extends from the outside cam 4a through the second phaser 125 and through the end plate 24 of the first phaser 25, fixedly attaching to the end plate 24 of the first phaser 25. Extending through the outside cam 4a and middle tubular portion 4b is a central hollow 5. A portion of the middle tubular portion 4b is surrounded by a first bearing 16. Through the first bearing 16 multiple passages 23a, 23b, 22 are present leading from supply, providing fluid to the control valve 114 received within a bore 103 in the rotor 110 of the second phaser 125. Line 22 provides fluid to the bearing.
Adjacent to the outside cam 4a is an inner cam 6a. By having the inside and outside cams 6a, 4a inline next to each other, the roller 28 of the lifter 29 is able to ride on both lobes of the cams at the same time. The inner cam 6a is integral with an inner tube portion 6b on one end that is received within the hollow 5 of the first camshaft piece 60 and passes through the second phaser 125 and is connected to the rotor 8 coaxially located within the housing 8 of the first phaser 25. Opposite the inner tube portion 6b, on the other side of the inner cam 6a is a shaft portion 6c with an end piece 6d larger than the diameter of the first camshaft piece 60, the inner tube portion 6b, and the shaft portion 6c. The end piece 6d on the shaft portion 6c prevents the second camshaft piece or inner camshaft piece 40 comprised of the inner cam 6a, the inner tube portion 6b, the shaft portion 6c, and the end piece 6d from dislodging from the assembly. The shaft portion 6c, not including the end piece 6d is surrounded by the second bearing 18. A passage 20b is present along the length of the second camshaft piece or the inner camshaft piece 40 to supply fluid from an inlet line 20a to the first phaser 25. The passages 20a, 20b provide fluid to the advance and retard chambers 15, 17 through a control valve 14 within a bore 3 in the rotor 10 of the first phaser 25. The control valve 14 controls the flow of fluid to the advance and retard chambers 15, 17 and the position of the rotor 8 relative to the housing 8. The position of the control valve 14 in the first phaser 25 is influenced by an actuator 12. The actuator 12 shown in
By using two phasers 25, 125, one attached to each cam 6a, 4a, both the opening and closing ramps of the valve event can be adjusted simultaneously while increasing or decreasing the duration of the valve event. In this embodiment, the valve event itself may also be phased. Furthermore, by adding a phaser 125 to the outer cam 4a, the entire valve event can be advanced or retarded from its base timing position. Valve events may also be added as necessary. Using two phasers 25, 125 also allows both cam lobes to be phased far enough apart form each other, allowing two valve events for one cylinder within a 360 degree revolution of both camshaft pieces, allowing strategies such as internal EGR and engine braking to be used.
The second phaser of the embodiment shown in
In all of the above embodiments, the first camshaft piece or the outer camshaft piece 40 and the second camshaft piece or the inner camshaft piece 60 together form the camshaft assembly 26.
The phasers in any of the above embodiments may be cam torque actuated phasers as disclosed in U.S. Pat. No. 5,107,804 issued Apr. 28, 1992, entitled “VARIABLE CAMSHAFT TIMING FOR INTERNAL COMBUSTION ENGINE” and is herein incorporated by reference, or hybrid as disclosed in a patent application Ser. No. 11/286,483 entitled, “CTA PHASER WITH PROPORTIONAL OIL PRESSURE FOR ACTUATION AT ENGINE CONDITION WITH LOW CAM TORSIONALS,” filed on Nov. 23, 2005 and hereby incorporated by reference, torsion assist phasers as disclosed in U.S. Pat. No. 6,883,481, issued Apr. 26, 2005, entitled “TORSIONAL ASSISTED MULTI-POSITION CAM INDEXER HAVING CONTROLS LOCATED IN ROTOR” with a single check valve TA, and is herein incorporated by reference and/or U.S. Pat. No. 6,763,791, issued Jul. 20, 2004, entitled “CAM PHASER FOR ENGINES HAVING TWO CHECK VALVES IN ROTOR BETWEEN CHAMBERS AND SPOOL VALVE” which discloses two check valve TA, and is herein incorporated by reference, or oil pressure actuated phasers.
Accordingly, it is to be understood that the embodiments of the invention herein described are merely illustrative of the application of the principles of the invention. Reference herein to details of the illustrated embodiments is not intended to limit the scope of the claims, which themselves recite those features regarded as essential to the invention.
This application claims one or more inventions which were disclosed in Provisional Application No. 60/944,806, filed Jun. 19, 2007, entitled “CONCENTRI CAM WITH PHASER”. The benefit under 35 USC §119(e) of the United States provisional application is hereby claimed, and the aforementioned application is hereby incorporated herein by reference.
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/US2008/066030 | 6/6/2008 | WO | 00 | 12/8/2009 |
Publishing Document | Publishing Date | Country | Kind |
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WO2008/157076 | 12/24/2008 | WO | A |
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Number | Date | Country | |
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20100186698 A1 | Jul 2010 | US |
Number | Date | Country | |
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60944806 | Jun 2007 | US |