Variable valve lift system
11047267 ยท 2021-06-29
Assignee
Inventors
Cpc classification
F01L1/182
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01L1/181
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01L2001/186
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01L13/0047
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01L1/267
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01L1/22
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01L2001/467
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01L2001/0473
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01L1/053
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01L2301/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01L2303/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01L1/26
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F01L1/18
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A summation rocker system is disclosed for acting on the end of a stem of a poppet valve (16) in dependence upon the combined lifts of a first and a second cam profile defined by different cam lobes (14, 22) of a concentric camshaft (46). The system comprises a first rocker (12) mounted on a pivot shaft (18) and having a first follower (44) to contact the first cam profile and an end acting on the valve (16) to displace the valve (16) by an amount dependent upon the lift of the first cam profile, a rocker shaft (24) to be fixedly mounted on the engine, and a second rocker (20) pivotable about the rocker shaft (24), the second rocker (20) having a second follower (48) to contact the second cam profile and acting to displace the pivot shaft (18) of the first rocker (12) in dependence of the lift of second cam profile. The rocker shaft (24) intersects a plane containing the axis of the pivot shaft (18) and the end of the first rocker (12) acting on the valve stem, and the first rocker (12) includes a cut-out (26) for receiving the rocker shaft (24), which cut-out (26) is configured and dimensioned to prevent the rocker shaft (24) from interfering with movement of the first rocker (12).
Claims
1. A summation rocker system for acting on a valve stem end of a poppet valve (16) based on combined lifts of a first and a second cam profile respectively defined by different cam lobes (14, 22) of a concentric camshaft (46), the summation rocker system comprising: a first rocker (12) mounted on a pivot shaft (18), the first rocker including: a first end configured to contact the first cam profile via a first follower (44); and a second end configured to displace the valve (16) by a lift amount determined by the first cam profile; a rocker shaft (24) fixedly mounted on an engine; and a second rocker (20) pivotably mounted on the rocker shaft (24), the second rocker (20) configured to contact the second cam profile via a second follower (48) so as to displace the pivot shat (18) by a lift amount determined by the second cam profile, wherein the rocker shaft (24) extends parallel to the pivot shaft (18), and wherein the first rocker (12) further includes a cut-out (26) configured to receive the rocker shaft (24), the cut-out (26) configured to prevent the rocker shaft (24) from interfering with a movement of the first rocker (12).
2. The summation rocker system as claimed in claim 1, wherein the cut-out (26) is a hole configured to permit the rocker shaft (24) to pass through the hole with swept clearance.
3. The summation rocker system as claimed in claim 1, wherein the rocker shaft (124) has a reduced cross sectional area in regions (121,123) where the rocker shaft is received within the cut-out (126).
4. The summation rocker system as claimed in claim 1, wherein the first rocker (212) further includes two surfaces (213,215) axially straddling the second rocker (20) such that the two surfaces (213,215) define a pocket (217) configured to receive the second rocker (20) with clearance.
5. The summation rocker system as claimed in claim 1, wherein the first rocker (212) comprises at least two parts (712a; 712b) secured to one another.
6. The summation rocker system as claimed in claim 1, wherein the first rocker (212) is formed from sheet metal.
7. The summation rocker system as claimed in claim 1, further comprising a control spring (28) configured to act between a stationary point in the engine and the first rocker (12) so as to urge the first follower (44) towards the first cam profile (14).
8. The summation rocker system as claimed in claim 1, further comprising a control spring (528) connected to the second rocker (520), the control ring configured to pass with clearance through a hole in the first rocker (512) which extends in a direction perpendicular to the pivot shaft.
9. A valvetrain comprising the summation rocker system of claim 1, wherein the engine includes an intake valve and an exhaust valve, wherein the valve (16) is one of the intake valve or the exhaust valve such that said summation rocker system is configured to open and close the one of the intake valve or the exhaust valve, and wherein the valvetrain further comprises a third rocker (332) configured to operate a remaining one of the intake valve or the exhaust valve based on a single profile of a third cam (334) of the camshaft.
10. The valvetrain as claimed in claim 9, wherein the third rocker (332) is pivotably mounted about an axis of the rocker shaft (324).
11. The valvetrain as claimed in claim 9, wherein the third rocker (432) is mounted to the rocker shaft (424) via an eccentric component (436) so as to pivot about an axis offset from an as is of the second rocker (420).
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) The invention will now be described further, by way of example, with reference to the accompanying drawings, in which:
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DETAILED DESCRIPTION OF EMBODIMENTS
(11) In the description below of embodiments of the invention, in order to avoid unnecessary repetition, like parts of different embodiments have been allocated reference numerals with the same last two digits. Hence numerals XX, 1XX, 2XX, 3XX etc. will be to designate identical components, or possibly modified components fulfilling the same function.
(12)
(13) As can be seen from
(14) To accommodate the rocker shaft 24 in such a position, the first rocker 12 of the embodiments of the invention shown in
(15) While a circular hole of sufficiently large diameter may be used, it is preferred to minimise the amount of material removed from the first rocker by providing a hole that is elongated in the direction of relative movement. The direction of relative movement may be curved or relatively straight, depending on the geometry of the valvetrain.
(16) The first rocker 212, of the embodiment shown in
(17) A control spring 28, shown in
(18) The optimum position of the control spring 28 creates a force vector through the pivot shaft 18 perpendicular to a line created between the pivot shaft 18 and the fixed rocker shaft 24. However, it is often a greater priority to minimize the height of the valvetrain, in which case the spring 28 may be moved from this optimum position.
(19) In a second embodiment of the invention as shown in
(20) It would equally be possible to form the reduced regions of the rocker shaft 124 with one or more slots rather than a reduced diameter in order to reduce the size of the cut-out 126 in the first rocker 112.
(21) If formed as a hole, a portion of the cut-out 126 should remain of a diameter to provide a clearance fit for the larger diameter regions of the rocker shaft 124. The diameter of the rocker shaft 124 is usually specified for a journal bearing of the second rocker 120 and so cannot be directly modified in the region that passes through the second rocker 120. The position of this larger diameter portion of the hole may be positioned anywhere along its swept range in order to maximize stiffness.
(22) The first rocker 212 of
(23) Alternatively, as illustrated in
(24) It is common for a summation rocker system to be used on only one of the intake or exhaust valves, the valve being operated using a conventional system with a single cam profile. Such a valvetrain is shown in each of
(25) The embodiments of the invention shown in
(26) An alternative approach for preventing rotation of the bushing 436 is adopted in the embodiment illustrated in
(27) As previously disclosed, the control spring 28 can sometimes be mounted in a less than optimal orientation in order to minimize the overall height of the valvetrain. Moving the control spring 28 from its optimal position requires the spring 28 to produce a higher force. Designing a control spring which exerts sufficient force but still fits into the packaging space of the cylinder head may be difficult or costly.
(28)
(29) It will be appreciated that the embodiments described above may be combined where technically possible. For example, the control spring may act on the second rocker independent of the design of the first rocker. If the first rocker were to be constructed in any other way than illustrated in
(30) Furthermore, it is alternatively possible for the control spring to be arranged to act between the two rockers in order to maintain the desired contact with one of the cam profiles, rather than acting between one of the rockers and a fixed point on the engine.
(31) Although the summation rocker system is, in the above embodiments, related to varying the lift of the valve, the duration that the valves are open and the timing of the valves may be varied depending on the phase of the cam lobes with respect to either each other, the crankshaft of the engine, or both.
(32) The invention may be used with any number of intake or exhaust valves in the engine, or indeed any engine configuration or number of cylinders. Where more than one valve per rocker is acted upon, the valves may be synchronized through a valve bridge connecting them to the rocker.