The present disclosure relates generally to a rocker arm assembly for use in a valve train assembly and more particularly to a rocker arm assembly having a mechanical latch pin for a deactivating rocker arm assembly capable of full lift, partial lift, or no lift.
Many internal combustion engines utilize rocker arms to transfer rotational motion of cams to linear motion appropriate for opening and closing engine valves. Deactivating rocker arms incorporate mechanisms that allow for selective activation and deactivation of the rocker arm. In a deactivated state, the rocker arm may exhibit lost motion movement. In order to return to an activated state from a deactivated state, the mechanism may require that the rocker arm be in a particular position or within a range of positions that may not be readily achieved while undergoing certain unconstrained movement while in the deactivated state, such as during excessive lash adjuster pump-up.
The background description provided herein is for the purpose of generally presenting the context of the disclosure. Work of the presently named inventors, to the extent it is described in this background section, as well as aspects of the description that may not otherwise qualify as prior art at the time of filing, are neither expressly nor impliedly admitted as prior art against the present disclosure.
The methods disclosed herein overcome the above disadvantages and improves the art by way of a rocker arm assembly comprising a valve side rocker arm portion, a cam side rocker arm portion configured to selectively rotate relative to the valve side rocker arm portion, and a latch pin assembly disposed in the valve side rocker arm portion and in the cam side rocker arm portion. Portions of the latch pin assembly are configured to move so that when the cam side rocker arm portion selectively rotates, the valve side rocker arm portion switches among a full lift mode, a partial lift mode, and a lost motion lift mode.
The latch pin assembly comprises a primary latch pin assembly disposed in the valve side rocker arm portion opposite a secondary latch pin assembly disposed in the cam side rocker arm portion. The valve side rocker arm portion comprises a primary oil control cavity in a valve side body, and the primary latch pin assembly is configured to telescope in and out of the primary oil control cavity. The primary latch pin assembly comprises a first primary pin nested in a channel of the primary oil control cavity and a second primary pin nested in a channel of the first primary pin. The valve side body comprises an oil channel configured to supply oil pressure to the primary oil control cavity. A first biasing member is configured to bias the second primary pin out of the first primary pin.
The cam side rocker arm portion comprises a secondary oil control cavity in a cam side body, and the secondary latch pin assembly is configured to telescope in and out of the secondary oil control cavity. The secondary latch pin assembly comprises a first secondary pin nested in a channel of the secondary oil control cavity and a second secondary pin nested in a channel of the first secondary pin. The cam side body comprises an oil channel configured to supply oil pressure to the secondary oil control cavity. The oil channel in the valve side body is configured to supply oil pressure to the oil channel in the cam side body. A second biasing member is configured to bias the first secondary pin out of the cam side rocker arm portion. The valve side rocker arm portion comprises a rim around the primary latch pin assembly, and the secondary latch pin assembly is configured to telescope out of the cam side rocker arm portion and into the rim. A portion of the secondary latch pin assembly is configured to telescope out of the cam side rocker arm portion and into a portion of the primary latch pin assembly.
The rocker arm assembly can be configured wherein the cam side rocker arm portion comprises a secondary oil control cavity in a cam side body, wherein the secondary latch pin assembly comprises a first secondary pin nested in a channel of the secondary oil control cavity and a second secondary pin nested in a channel of the first secondary pin, and wherein the second secondary pin is configured to telescope out of the channel of the first secondary pin and into the channel of the first primary pin.
The cam side rocker arm portion can be configured to pivot past the valve side rocker arm portion when the primary latch pin assembly opposes the secondary latch pin assembly in the lost motion lift mode.
Additional objects and advantages will be set forth in part in the description which follows, and in part will be obvious from the description, or may be learned by practice of the disclosure. The objects and advantages will also be realized and attained by means of the elements and combinations particularly pointed out in the appended claims.
It is to be understood that both the foregoing general description and the following detailed description are exemplary and explanatory only and are not restrictive of the claimed invention.
Reference will now be made in detail to the examples which are illustrated in the accompanying drawings. Directional references such as “left” and “right” are for ease of reference to the figures.
With reference to
The rocker arm assembly 10 is shown as a type III, center pivot. It can comprise a roller bearing 9 on a bearing axis 8 for interfacing with a cam rail. A cam lobe on the cam rail can impart a valve lift profile to the rocker arm assembly 10. A tappet interface can substitute for the roller bearing 9 and bearing axis 8.
The cam side rocker arm portion 14 and the valve side rocker arm portion 12 can pivot with respect to one another around a pivot axle 7. Or, the pivot location for the cam side rocker arm portion 14 and the valve side rocker arm portion 12 can be shared about the rocker shaft bore 3, as by extending the material of the cam side rocker arm portion 14 around the rocker shaft bore and eliminating the pivot axle 7.
A spring 6 can be biased between the cam side rocker arm portion 14 and the valve side rocker arm portion 12. The spring can enable lost motion valve lift profiles, including zero lift profiles, as described more below, when the latch pin assembly 20 is configured for lost motion.
The valve side rocker arm portion 12 can comprise a variety of additional aspects such as a lash adjuster, deactivating capsule, engine brake capsule, among others as by an insert 5. An engine valve stem can connect directly or indirectly at an elephant foot (e-foot) 4 or the like, and valve bridges and other valve connections can be used.
The rocker shaft bore 3 can couple to a rocker shaft and the rocker shaft can be configured to supply pressurized control fluid to the rocker arm assembly 10. Then, internal oil channels 200-204 can supply control fluid. For example, oil channel 202 can supply control fluid to enable hydraulic lash adjustment in the insert 5, or to enable engine braking or cylinder deactivation functionality, as per the insert 5. Oil channel 200 in valve side latch body 240 of valve side rocker arm portion 12 can supply control fluid to the latch pin assembly 20. Oil channel 201 in cam side latch body 242 can supply a separate control fluid. Oil channels 200-202 connect to receive fluid from the rocker shaft bore 3, and oil channels 203, 204 can be formed for additional functionality, such as an EEVO (early exhaust valve opening) control fluid. The oil channels 200-204 can be drilled or cast or otherwise formed into the rocker arm assembly 10, and in some alternatives plugs 1 can be used to fluidly seal an end of the oil channel, as shown for oil channel 200 in
A slot 30 is defined in the cam side rocker arm portion 14. The latch pin assembly 20 engages the slot 30 in a way that is normally latched and allows for lost motion when disengaged, and also engages in a way as referred to herein as partially engaged. Slot 30 comprises on one side, shown in body portion 240 of valve side rocker arm portion 12, a primary oil control cavity 70. On the other side of slot 30, shown in body portion 242 of cam side rocker arm portion 14, a secondary oil control cavity 72 is formed. Latch pin assembly 20 is nested in slot 30 and comprises telescoping aspects to interface with channels 440, 540, 4400, 5400, 701, 722, 1701, 1722 and rims 401, 402, 4010, 4020 to provide at least two valve lift profiles to one or more valves coupled to the rocker arm, and to provide at least three valve lift profiles.
Referring now to
A first end 441 of first primary pin 44 can abut a back wall 1700 of oil control cavity 70 in
Outward surface 462 of first secondary pin 46 can be biased towards secondary latch pin assembly 42 by first biasing member 60 in a cavity 461. Outward surface 562 of second secondary pin 56 can be biased towards primary latch pin assembly 40 by the second biasing member 62 and by oil pressure to gland communicating with secondary oil control cavity 72. The blind bore 68 can be oil fed by oil channel 201. Lock ring 66 can seat second secondary pin 56. And, secondary pin 56 can be opposed and positioned in secondary channel 540 by oil pressure to second primary pin 46.
With reference to
Comparing
With reference now to
Outward surface 1462 of first secondary pin 146 can be biased towards secondary latch pin assembly 142 by first biasing member 160. Outward surface 1562 of second secondary pin 156 can be biased towards primary latch pin assembly 140 by the second biasing member 162 and by oil pressure to gland communicating with secondary oil control cavity 172. The blind bore 168 can be oil fed by oil channel 201. Lock ring 166 can seat second secondary pin 156. And, secondary pin 156 can be opposed and positioned in secondary channel 1540 by oil pressure to second primary pin 146.
A first end 1441 of first primary pin 144 can abut a back wall 1700 of oil control cavity 170 in
Turning to
In reference to
In reference to
Another kind of “lost motion” is shown in
Other implementations will be apparent to those skilled in the art from consideration of the specification and practice of the examples disclosed herein. The foregoing description has been provided for purposes of illustration. It is not intended to be exhaustive. Individual elements or features of a particular example are not exclusive to that particular example, but, where applicable, are interchangeable and can be used in other examples disclosed.
This is a § 371 National Stage Entry of Patent Cooperation Treaty Application No. PCT/EP2019/025261, filed Aug. 7, 2019 which claims the benefit of U.S. provisional application No. 62/716,712, filed Aug. 9, 2018, all of which are incorporated herein by reference.
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PCT/EP2019/025261 | 8/7/2019 | WO | 00 |
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WO2020/030298 | 2/13/2020 | WO | A |
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Number | Date | Country | |
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20210324768 A1 | Oct 2021 | US |
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62716712 | Aug 2018 | US |