The present invention relates to a valve train assembly.
Compression engine brakes are typically used as auxiliary brakes, in addition to wheel brakes, on relatively large vehicles, for example trucks, powered by heavy or medium duty diesel engines. A compression engine braking system is arranged, when activated, to provide an additional opening of an engine cylinder's exhaust valve when the piston in that cylinder is close to the top-dead-center position of its compression stroke so that compressed air is released through the exhaust valve. This causes the engine to function as a power consuming air compressor which slows the vehicle.
In a typical valve train assembly used with a compression engine brake, the exhaust valve is actuated by a rocker arm which engages the exhaust valve by means of a valve bridge. The rocker arm rocks in response to a cam on a rotating cam shaft and presses down on the valve bridge which itself presses down on the exhaust valve to open it. A hydraulic lash adjuster may also be provided in the valve train assembly to remove any lash (i.e. gap) that develops between components in the valve train assembly.
There is a need for an improved valve bridge and in particular, but not exclusively, one that can be used in combination with a compression engine braking system.
In an embodiment, the present invention provides a valve train assembly, the valve train assembly comprising: a valve bridge assembly, the valve bridge assembly comprising: a valve bridge; a first cavity formed towards a first end portion of the valve bridge; and a hydraulic lash adjuster (HLA) disposed within the first cavity, the HLA being configured to engage a first valve stem. The valve train assembly further comprises: a pivotally mounted first rocker arm configured to engage the valve bridge and to pivot in response to a rotating first cam to cause a first valve lift event in an engine cycle. The first rocker arm comprises: a rocker arm cavity formed within an end portion thereof; and a control capsule disposed within the rocker arm cavity, wherein the control capsule is configurable in an ON configuration and an OFF configuration, wherein, in the ON configuration the pivoting of the first rocker arm is configured to cause the first valve lift event and, in the OFF configuration, the control capsule is configured to prevent the pivoting of the first rocker arm from causing the first valve lift event.
The present invention will be described in even greater detail below based on the exemplary figures. The invention is not limited to the exemplary embodiments. Other features and advantages of various embodiments of the present invention will become apparent by reading the following detailed description with reference to the attached drawings which illustrate the following:
As shown in
Similarly, the intake rocker arm 3 is provided at its other end with a spigot located in a complimentary shaped socket of an intake rocker arm E-foot. The intake rocker arm E-foot engages an intake rocker arm valve bridge 37 which operates a pair of intake valves 39 and 41 of the engine cylinder 33.
During normal powered engine operation (i.e. when the engine is generating power strokes) a lobe of the intake cam causes the intake rocker arm 3 to pivot about the rocker shaft 9 to push the intake valve bridge 37 and hence the intake valves 39 and 41 downwards to open them for the intake part of the engine cycle. Likewise, later in the engine cycle, a lobe of the exhaust cam causes the exhaust rocker arm 5 to pivot about the rocker shaft 9 to push the exhaust valve bridge 27 and hence the exhaust valves 29 and 31 downwards to open the them for the exhaust part of the engine cycle. As is conventional, all of the valves 29, 31, 39, 41 are provided with valve return springs biased to cause the valves 29, 31, 39, 41 to return to their closed positions as the relevant cam lobe passes out of engagement with its associated roller 11 or 13.
As shown in
The hydraulic lash adjuster 47 comprises an outer body 49 having a closed end 51 and an open end 53 and defines a longitudinal bore 55 between the closed 51 and open 53 ends. The closed end 51 is for engaging a valve stem 29a of the valve 29. A plunger assembly 57 is mounted for sliding movement back and forth within the bore 55 and its upper end extends above the bore 55.
The plunger assembly 57 and the outer body 49 define between them a first oil pressure chamber 60 towards the bottom of the bore 55 (i.e. towards the bottom of the HLA 47). An aperture 62 at the bottom of the plunger assembly 57 allows oil to flow from a second oil pressure chamber 64, or oil reservoir, within the plunger assembly 57 into the first oil chamber 60. Oil is kept supplied to the second oil pressure chamber 64 from the engine's oil supply via a connected series of oil supply conduits 50 formed through the rocker shaft 9, exhaust rocker arm 5, E-Foot 25 and exhaust valve bridge 27.
Below the aperture 62, a ball valve is provided which comprises a check ball 68 captured by a cage 70 and biased by a spring 72 to a position closing the aperture 62. The plunger assembly 57 is biased outwardly of the outer body 49 by means of a spring 74 held within the first oil pressure chamber 60.
In use, the spring 74 expands the overall length of the hydraulic lash adjuster 47 by pushing the plunger assembly 57 outwardly of the outer body 49 so as to take up any slack that has developed in the valve train assembly 1. During the course of this motion, oil flows from the second oil chamber 64 into the first oil chamber 60 through the aperture 62. When pressure is applied to the upper end of the HLA 47 inward movement of the plunger assembly 57 is inhibited by the high pressure of oil in the first oil chamber 60. The oil in the first oil chamber 60 cannot flow back into the second oil chamber 64 because of the ball 68. As is standard, oil can escape the first oil chamber 60 by leaking between the surface of the bore 55 and the outer surface of the plunger assembly 57, but this can occur only very slowly (particularly if the oil is cold) because the bore 55 and the plunger assembly 57 are made to tight tolerances to restrict oil flow.
The HLA 47 compensates valve lash by expanding to compensate for all lashes on both valve tips. To this end, the HLA 47 will expand until the upper surface of the exhaust valve bridge 27 is in contact and flush with the lower surface of the E-foot 25, whilst the lower surface of the HLA 47 sits without any lash on the tip of the valve 29 and a further contact surface of a support member 80 sits without any lash on the tip of the valve 30.
The exhaust valve bridge 27, after having moved to compensate for all lashes, will not necessarily be horizontal, and for this reason, in this example, the lower surface 47a of the HLA 47 is formed as a part section of a spherical surface or relatively large radius of curvature and, in addition, the exhaust valve bridge 27 is mounted for pivotal movement about the support member 80 which is received within an aperture at one end of the exhaust valve bridge 27. The radius of curvature of the lower surface 47a helps ensure that good contact is maintained between the lower surface 47a and the tip of the valve 29, particularly when the valve bridge 27 is not horizontal, and that that contact is away from the edge of the tip of the valve 29.
As illustrated in
In this example, pivoting of the exhaust valve bridge 27 about the support member 80 helps ensure that good contact is maintained between the support member 80 and the tip of the valve 30, when the valve bridge 27 is not horizontal. In an alternative embodiment (not illustrated), the valve bridge 27 does not comprise the support member 180, but instead, in order to maintain good contact with the tip of the valve 30, it is provided with a fixed valve tip contact surface (i.e. one about which the valve bridge 27 cannot pivot) which similarly to the lower surface 47a of the HLA 47, is formed as a part section of a spherical surface or relatively large radius of curvature.
The exhaust valve bridge 27 is further provided with a clip 90, which is shown in detail in
Referring now to
The engine brake control capsule 112 comprises a first hollow member 122, a second hollow member 124, a push member 126 and a spring 128. The actuator 120 rotates the second hollow member 124 to configure the engine brake control capsule 112 in the engine brake ‘ON’ configuration, or the engine brake ‘OFF’ configuration. The first hollow member 122 is provided with a retaining pin 123 that prevents rotation of the first hollow member 122. An open end of the first member 122 faces an open end of the second member 124 so that the first member 122 and second member 124 define a chamber 130 in which the spring 128 is located. The push member 126 is disposed along the longitudinal axis of the brake capsule 112 through the chamber 130 and comprises an upper end which protrudes through a hole formed in the closed end of the first hollow member 122 and a lower end which extends through a hole formed in the closed end of the second member 124. The open ends of the first and second members are crenulated around their circumferences, each comprising a sequence of alternating raised parts and recesses.
The actuator 120 comprises a cylinder 140 provided on a side of the rocker arm 7 and containing a piston 142 mounted for reciprocating movement within the cylinder between an engine brake off position, in which the piston is fully retracted, and an engine brake on position, in which the piston is fully extended. The actuator 120 further comprises a return spring 144 disposed within the cylinder 140 and arranged to bias the piston 142 towards the engine brake ON position. The piston 142 comprises an end which extends outside of the cylinder 140 and which is fixed, for example, by a rivet, to a planar ring member 146. As best seen in
In the default engine brake ‘ON’ configuration, shown in
During engine operation when the engine brake is ON, once per cam shaft rotation, a lobe of the engine brake cam causes the exhaust brake rocker arm 7 to pivot about the rocker shaft 9 so that the first hollow member pushes 122 down on the second hollow member 124 which in turn causes the push member 126 to push down on the HLA 47 (i.e. the capsule behaves as a solid body). Hence, the HLA 47 pushes down on the exhaust valve 29 which opens to provide an engine brake event timed to coincide with a compression stroke of the piston. A valve return spring causes the exhaust valve 29 to return to its closed position as the exhaust cam lobe passes out of engagement with its associated roller.
As is illustrated in
In order to deactivate the engine brake, an engine control system supplies hydraulic fluid (for example, oil), via fluid supply path 141 (best seen in
During engine operation when the engine brake is OFF, as the lobe of the engine brake cam causes the exhaust brake rocker arm 7 to pivot about the rocker shaft 9, the first member 122 and the ring member 146 move relative to the second member 124, which remains stationary. The first 122 and second 124 members remain out of contact throughout this movement, even at the bottom of the exhaust rockers arm's stroke, and therefore no force is exerted on the push member 126 and consequently the exhaust valve 29 does not open. As the exhaust brake rocker arm 7 returns to its starting position, the first member 122 and the ring member 146 return to their starting positions, the first member 122 under the action of the return spring 130. It should be appreciated that
The actuator 102 is provided with a safety check valve 143, which is biased to a closed position, but which opens under increased fluid pressure in the cylinder 140 caused when the piston 142 is sometimes hit backwards into the cylinder 140. The safety check valve reliefs the increased fluid pressure in such circumstances, thereby avoiding hydraulic lock.
During engine operation when the engine brake is OFF, when the single cam profile 200 engages the roller causing the exhaust rocker arm 5 to pivot about the rocker shaft 9 during the part of the cycle that would produce the engine brake event in the engine brake ‘ON’ configuration, as with the embodiment described above, the first member 122 and the ring member 146 are free to move relative to the second member 124, which remains stationary throughout the movement of the rocker arm 5, and so no force transferred to the exhaust valves 29 and 30 which remain closed. Then, later in that cam shaft rotation, when the single cam profile again causes the exhaust brake rocker arm 5 to pivot about the rocker shaft 9, the first member 122 moves further and is brought into meshing contact with the second member 124. Consequently, the first member 122 and second member 124 then act as a solid body and as the rocker arm 5 continues its downward stroke a force is transferred to the exhaust valves 29 and 30 which open to provide a main exhaust valve event.
Further embodiments of the invention include a valve bridge for a valve train assembly, the valve bridge comprising a first cavity formed towards a first end portion of the valve bridge; and a hydraulic lash adjuster (HLA) disposed within the first cavity for engaging a first valve stem. The valve bridge may further comprise a second cavity, formed towards a second end portion of the valve bridge, containing a support member; wherein the valve bridge is supported for pivotal movement about the support member. The support member may be for engaging a second valve stem. The valve bridge may further comprise a clip member which supports the valve bridge and is clipped to the support member. The valve bridge may further comprise a contact surface at a second end portion of the valve bridge for engaging a second valve stem, wherein the contact surface is curved. The curved contact surface may be substantially part spherical. The HLA may comprise a contact surface for engaging the first valve stem, wherein the contact surface is curved. The curved contact surface may be substantially part spherical. The valve train assembly may further comprise a pivotally mounted first rocker arm for engaging the valve bridge and pivoting in response to a rotating first cam to cause a first valve lift event in an engine cycle. The first rocker arm may comprise a third cavity formed within an end portion thereof and a control capsule disposed within the third cavity, wherein the control capsule is configurable in an ON configuration and OFF configuration, wherein, in the ON configuration pivoting of the first rocker arm causes the first valve lift event and, in the OFF configuration, the control capsule prevents the pivoting of the first rocker arm from causing the first valve lift event. The first rocker arm may be for engaging the valve bridge and pivoting in response to the rotating first cam to also cause a second valve lift event in the engine cycle, wherein the second valve lift event occurs irrespective of whether the control capsule is in the ON configuration or the OFF configuration. The first rocker arm may be for engaging the HLA in the valve bridge and the assembly further comprises a second pivotally mounted rocker arm for engaging the valve bridge and pivoting in response to a rotating second cam to cause a second valve lift event in the engine cycle. The first valve event may be an engine brake valve event. The second valve lift event may be a main exhaust lift event.
The above embodiments are to be understood as an illustrative example of the invention only. Further embodiments of the invention are envisaged. For example, although the embodiments have been described in the context of a valve bridge used in a valve train that provides an engine brake function this need not be the case. A valve bridge embodying the present invention might be used to enable valve lift events other than those described above. Furthermore, equivalents and modifications not described above may also be employed without departing from the scope of the invention, which is defined in the accompanying claims.
While the invention has been illustrated and described in detail in the drawings and foregoing description, such illustration and description are to be considered illustrative or exemplary and not restrictive. It will be understood that changes and modifications may be made by those of ordinary skill within the scope of the following claims. In particular, the present invention covers further embodiments with any combination of features from different embodiments described above and below. Additionally, statements made herein characterizing the invention refer to an embodiment of the invention and not necessarily all embodiments.
The terms used in the claims should be construed to have the broadest reasonable interpretation consistent with the foregoing description. For example, the use of the article “a” or “the” in introducing an element should not be interpreted as being exclusive of a plurality of elements. Likewise, the recitation of “or” should be interpreted as being inclusive, such that the recitation of “A or B” is not exclusive of “A and B,” unless it is clear from the context or the foregoing description that only one of A and B is intended. Further, the recitation of “at least one of A, B and C” should be interpreted as one or more of a group of elements consisting of A, B and C, and should not be interpreted as requiring at least one of each of the listed elements A, B and C, regardless of whether A, B and C are related as categories or otherwise. Moreover, the recitation of “A, B and/or C” or “at least one of A, B or C” should be interpreted as including any singular entity from the listed elements, e.g., A, any subset from the listed elements, e.g., A and B, or the entire list of elements A, B and C.
Number | Date | Country | Kind |
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1211534.1 | Jun 2012 | GB | national |
This application is a continuation of a U.S. patent application Ser. No. 14/411,524, filed on Dec. 29, 2014, which is a U.S. National Stage application under 35 U.S.C. § 371 of International Application No. PCT/EP2013/063787, filed on Jul. 1, 2013, which claims benefit to British Patent Application No. 1211534.1, filed on Jun. 29, 2012. The International Application was published in English on Jan. 3, 2014, as WO 2014/001560 A1 under PCT Article 21(2). The entire disclosures of the foregoing applications are hereby incorporated by reference herein.
Number | Name | Date | Kind |
---|---|---|---|
2380051 | Kettering | Jul 1945 | A |
3140698 | Voorhies | Jul 1964 | A |
4677723 | Greene, Sr. | Jul 1987 | A |
4924821 | Teerman | May 1990 | A |
5150672 | Fischer et al. | Sep 1992 | A |
5501187 | Speil et al. | Mar 1996 | A |
6334429 | Little, Jr. | Jan 2002 | B1 |
7984705 | Yang | Jul 2011 | B2 |
8210144 | Langewisch | Jul 2012 | B2 |
8413626 | MacVicar | Apr 2013 | B2 |
8578901 | Ruggiero et al. | Nov 2013 | B2 |
8627791 | Janak et al. | Jan 2014 | B2 |
8813719 | Sailer et al. | Aug 2014 | B2 |
8851048 | Meistrick | Oct 2014 | B2 |
9512745 | Cecur | Dec 2016 | B2 |
20090064955 | Rauch et al. | Mar 2009 | A1 |
20090199802 | MacVicar | Aug 2009 | A1 |
Number | Date | Country |
---|---|---|
4338845 | May 1995 | DE |
4410122 | Sep 1995 | DE |
19836906 | Feb 2000 | DE |
0504128 | Sep 1992 | EP |
2034138 | Mar 2009 | EP |
WO 2010078280 | Jul 2010 | WO |
WO 2011015603 | Feb 2011 | WO |
Number | Date | Country | |
---|---|---|---|
20170051638 A1 | Feb 2017 | US |
Number | Date | Country | |
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Parent | 14411524 | US | |
Child | 15346770 | US |