[0001] The present invention relates to an internal combustion engine according to the preamble
of independent claim 1 and to a method for controlling the valve actuation of an internal
combustion engine according to the preamble of independent claim 13.
[0002] There have been dynamic valve apparatus for engines capable of performing variable
control to shut down some of the plurality of valves on each cylinder, to variably
control the valve opening and closing timing, and to variably control the valve lift.
[0003] An example of a variable lift control type of dynamic valve apparatus is the swing
arm type that was described in the prior art, for example in Japan Patent Application
Disclosure Sho 60-243310 (1985). This conventional apparatus pivotally supports the
swing arms at their base end and brings the valve shaft into contact with their front
end, wherein each of said swing arms would be pushed and driven by a cam nose, a second
pivot also is present between the first pivot and the cam nose on said swing arm,
and said second pivot can be moved up or down by a hydraulic cylinder.
[0004] With the apparatus of the prior art as described in the above application, when the
engine is operating in the low speed operating range, the swing arm pivots on the
first pivot, and when operating in the high speed operating range, the swing arm pivots
on the second pivot. This design causes greater valve lift in the high speed operating
range than in the low speed operating range.
[0005] However, in order to further improve the performance of engines, not only is it necessary
to vary the valve lift between the low speed and high speed operating ranges, but
it is further desirable to vary the valve timing as well. Since the foregoing conventional
apparatus relies on the same cam noses, it is not possible to vary the valve timing
in that design. Furthermore, it is impossible to obtain a zero valve lift, in other
words, to shut down the valves.
[0006] In GB-A-2 139 283 a multi-cylinder internal combustion engine operable with at least
one ineffective cylinder is described, wherein the cylinders of the engine comprise
respective an inlet and an exhaust valve. The inlet and exhaust valve are openable
and closeable by a rocker arm driven by a first cam nose mounted on a camshaft. Otherwise
in a light condition of the engine at least one cylinder is switched off due to the
holding of the inlet and exhaust valve in a close position by the rocker arm driven
by a second cam nose mounted next to the first cam nose on the camshaft wherein the
rocker arm is in sliding contact with the first and second noses.
[0007] Further, US-A-4,515,121 relates to a valve driving control apparatus in an internal
combustion engine, wherein said engine comprises a plurality of power cylinders each
having a plurality of intake and exhaust reciprocating valves which are made operative
or inoperative depending upon the load conditions of said engine. Said operative or
inoperative condition of said valves is controlled by a valve driving apparatus, wherein
a controlling fluid flow is applied in said valve driving apparatus by a de-energizer
or energizer electromagnetic solenoid to make said valves inoperative or operative.
[0008] Furthermore, EP-A-0 037 443 relates to a means for overriding a control means which
controls intake and exhaust valves during operation of an engine to maintain said
intake and exhaust valves closed, wherein said means uses fluid pressure and controlling
members to engage said valves in a closed position.
[0009] Accordingly, it is an objective of the present invention to provide an improved internal
combustion engine as indicated above which facilitates with a simple and space saving
construction the variable control of the valve opening and closing timing as well
as of the valve lift and in addition to control the valve shut down.
[0010] It is a further objective of the present invention to provide an improved method
for controlling the valve actuation of an internal combustion engine as indicated
above which facilitates to reliably control and with a minimal time delay the variable
control of the valve opening and closing timing as well as of the valve lift and in
addition to control the valve shut down.
[0011] According to the present invention, this objective is solved by an internal combustion
engine comprising the features of claim 1.
[0012] Further, according to the present invention, this objective is solved through a method
for controlling the valve actuation of an internal combustion engine having the features
of claim 13.
[0013] In order to further enhance the controllability of the internal combustion engine,
it is advantageous when said moving mechanism comprises sliders slidingly mounted
on the exhaust and intake rocker shafts and being movable by a transmission pin guidable
by respective drive slots formed in said exhaust end intake rocker shafts for pushing
said rocker arms form a first position to a second position, a spring for urging said
rocker arms back to the first position when said sliders are released from said rocker
arms, and an actuator rotating said exhaust and intake rocker shafts to actuate said
sliders.
[0014] When said internal combustion engine comprises three intake air valves and two exhaust
valves symmetrically arranged to both sides of a plane containing a central axis of
said cylinder, it is advantageous when at least said air intake valves arranged at
both sides of said plane and at least one of said exhaust valves are operable by said
moving mechanism.
[0015] According to an advantageous embodiment. all exhaust and all intake valves are operable
by said moving mechanism.
[0016] According to an advantageous embodiment of the method for controlling the valve actuation,
it is advantageous when at least two of said air intake valves and at least one of
said exhaust valves are moved by said moving mechanism.
[0017] It is possible to further enhance the controllability when an engine control unit
controls said moving mechanism.
[0018] According to one preferred embodiment when the rocker arm is positioned in the operational
position, the rotational movement of the cam nose is transmitted to the valve by the
rocker arm; when the rocker arm is in the non-operational position, the rotational
movement of the cam nose is transmitted directly to the valve, and it is possible
to vary the amount of valve lift depending on the axial position of the rocker arm.
[0019] According to another preferred embodiment, the cam nose is composed of a high speed
nose and a low speed nose, so that, when the rocker arm is positioned in the operational
position, the rotational movement of the high speed nose is transmitted by the rocker
arm to the valve, and when the rocker arm is in the non-operational position, the
rotational movement of the cam nose is transmitted directly to the valve. As a result,
depending on the shapes of the low speed nose and high speed nose and the amount of
lift in the designs, it is possible to variably control the valve lift and the opening
and closing timing. In this case, by setting the low speed nose to have approximately
zero lift, it is possible to shut down the valve when the rocker arm is placed in
the non-operational position.
[0020] According to a further preferred embodiment, the above described shifting system
is installed for one of the exhaust valves and for the left and right side intake
valves, and the foregoing low speed nose is shaped to virtually shut down the opening
and closing operations of the valve. Accordingly, during low speed operations, one
of the foregoing exhaust valves, and the left and right side air intake valves are
virtually shut down, while only the remaining exhaust valve and the center air intake
valves are operated. During mid-speed operations, either the foregoing left or right
side air intake valve is shut down while both exhaust valves and two air intake valves
are operated. Further, in high speed operating ranges, all the valves are operated,
thereby making it possible to shut down valve operations in three stages according
to the operating state of the engine.
[0021] Further, since only the center air intake valve, from among the three air intake
valves, is left operational in the low speed operating range, it is possible to direct
the air intake flow in the axial direction of the cylinder, thereby generating a tumbling
action which facilitates stable combustion at lean air/fuel ratios.
[0022] According to still another preferred embodiment since the transfer speed of the rocker
arm from the non-operational position to the operational position is higher than the
transfer speed in the reverse direction, during rapid acceleration, for example, the
number of valves operating can be immediately increased, thereby improving acceleration
response.
[0023] Further, according to a still further the rotation of the inner rocker shaft to preferred
embodiment the non-operational position causes the rocker arms to be shifted to the
non-operational position by the drive surface of the inner rocker arm which drives
it in the non-operational direction when rotated, and the retaining members on the
outer rocker shaft retain the rocker arms in said non-operational position. On the
other hand, when the inner rocker shaft is rotated into the operational position,
the rocker arms are released from the foregoing retainer position by the return drive
surface on the inner rocker shaft, and the foregoing holding force immediately returns
the rocker arms to the operational position. This feature allows the movement of the
rocker arms from the non-operational position to the operational position to be quicker
than their movement in the opposite direction.
[0024] Other preferred embodiments of the present invention are laid down in further dependent
claims.
[0025] In the following, the present invention is explained in greater detail with respect
to several embodiments thereof in conjunction with the accompanying drawings, wherein:
Figure 1 is a top view of the dynamic valve apparatus for an engine according to a first embodiment
incorporating the inventions of Claims 1 - 3;
Figure 2 is a sectional view along line II-II of Figure 1;
Figure 3 is a sectional view along line III-III of Figure 1;
Figure 4 is a side view of the cylinder head of the foregoing embodiment;
Figure 5 is a diagram showing the shape of the cam nose in the foregoing embodiment;
Figure 6 is a diagram showing the drive mechanism for the rocker arms in the foregoing embodiment;
Figure 7 is a diagrammatic sectional view showing the drive slots on the rocker shafts in
the foregoing embodiment;
Figure 8 explains the operation of the foregoing embodiment;
Figure 9 explains the operation of the foregoing embodiment;
Figure 10 explains the operation of the foregoing embodiment;
Figure 11 is a top view of a modification around the center air intake valve of the foregoing
first embodiment;
Figure 12 is a sectional side view of a modification around the center air intake valve of
the foregoing first embodiment;
Figure 13 is a top view of the dynamic valve apparatus of a second embodiment that incorporates
the inventions of Claims 4 and 5;
Figure 14 is a diagram showing the drive slots of the foregoing second embodiment;
Figure 15 is a diagram used to explain the operation of the foregoing second embodiment;
Figure 16 is a diagram used to explain the operation of the foregoing second embodiment;
Figure 17 is a diagram used to explain the operation of the foregoing second embodiment; and
Figure 18 is a diagram of the drive slots of the foregoing second embodiment.
[0026] Examples of the present invention will be described below with reference to the attached
Figures.
[0027] Figures 1 - 10 will be used to explain a first embodiment of dynamic valve apparatus
for engines according to the present invention. Figure 1 is a top view showing the
cylinder head with the cover removed; Figures 2 and 3 are sectional views taken along
lines II-II and III-III of Figure 1, respectively; Figure 4 is a side view of the
cylinder head; Figure 5 is a diagram showing the shape of the cam nose; Figure 6 is
a diagram showing the drive slot of the rocker shaft; Figure 7 is a sectional diagram
of the rocker shaft drive mechanism, Figures 8 through 10 are Figures that will be
used to explain the operation. In the present embodiment, the exhaust side will be
the front side and the air intake side will be the rear side, and left, right and
center will refer to the directions when looking toward the front side from the rear
side.
[0028] In the Figures, 1 represents an engine cylinder head for a water-cooled, four-stroke
cycle, in-line, twin cylinder, five-valve engine equipped with an embodiment of this
invention, and it is secured to the top of the top mating surface of a cylinder body
2 that is affixed to the top of a crank case (not shown) by means of head bolts 3.
[0029] Two concave combustion zones 1b are formed in the cylinder body mating surface 1a
of the foregoing cylinder head 1, which, together with the cylinder bores 2a in the
foregoing cylinder body 2, form the combustion chambers. Formed in said combustion
areas 1 b are left and right side air intake valve openings 4a, 4b, a center air intake
valve opening 4c, as well as left and right side exhaust valve openings 5a, 5. Further
there are threaded holes for spark plugs 6 positioned to approximately coincide with
the axial center of the cylinder bores 2a. These hold the spark plugs 6 in a manner
such that their electrodes are exposed to the inside of the foregoing concave combustion
areas 1b.
[0030] The foregoing air intake valve openings 4a - 4c converge into a single air intake
port 4 which connecting them to the rear wall of the cylinder head 1. In addition,
the foregoing exhaust valve openings 5a, 5b converge into a single exhaust port 5
connecting them to the front wall of said cylinder head 1.
[0031] The valve heads 7d of the air intake valves 7a, 7b and 7c are positioned, respectively,
where they can open and close the foregoing air intake valve openings 4a - 4c. Valve
springs 9, which hold the foregoing air intake valves 7a - 7c in the normally closed
position, are located between a retainer 8 on the top surface of the valve shafts
7e and spring seats 1c formed in the cylinder head. Attached to the top ends of the
foregoing air intake valves 7a - 7c are air intake lifters 10a. Said lifters 10a can
freely slide in lifter guide holes 1d formed in the cylinder head 1.
[0032] The valve heads 11c of the left and right side exhaust valves 11a, 11b are positioned,
respectively, where they can open and close the foregoing exhaust valve openings 5a,
5b. Valve springs 9, which hold the foregoing exhaust valves 11a, 11b in the normally
closed position, are located between a retainer 8 on the top surface of the valve
shafts 11d and spring seats 1c that were formed in the cylinder head 1. Attached to
the top ends of the foregoing exhaust valves 11a, 11b are exhaust lifters 10b. Said
lifters 10b can freely slide in lifter guide holes 1d formed in the cylinder head
1.
[0033] An air intake camshaft 12 and exhaust camshaft 13 are installed in parallel above
the foregoing air intake lifters 10a and exhaust lifters 10b. Said air intake and
exhaust camshafts 12, 13 are axially supported by air intake and exhaust center bearings
14, 15 which are located in the areas of the shafts opposite the cylinder bore axes.
[0034] The foregoing center exhaust bearings 15 are composed of receiver members 15a formed
in the cylinder head 1 and of removable cam caps (not shown) attached thereto. Said
cam caps are retained in place over the foregoing head receiver members 15a by cap
bolts secured in two threaded bolt holes 15b.
[0035] The foregoing center air intake bearings 14 are composed of receiver members 14a
formed in the cylinder head 1 and of removable cam caps (not shown) attached thereto.
The foregoing head side receiver member 14a splits left and right, on either side
of the air intake lifter 10a, to accommodate the center air intake valve 7c. Further,
said cam caps are forked and are retained in place over the foregoing head receiver
members 14a by cap bolts secured in three threaded bolt holes 14b.
[0036] The foregoing air intake and exhaust camshafts 12, 13 are supported on their right
ends by the end bearings 16. Said end bearings 16 are composed of a head-side bearing
16a that is formed in the partitioning wall 1f between the cam chamber and the chain
chamber 1e and the cover bearing (not shown) formed on one side of the head cover.
Located inside the foregoing chain chamber are cam sprockets 17, 18 formed on the
right ends of the foregoing camshafts 12, 13, respectively, and said sprockets 17,
18 are linked to the cam sprocket on the crankshaft by means of a timing chain 19.
[0037] A variable exhaust timing mechanism 20 on the foregoing left side exhaust valve 11a
and a fixed exhaust timing mechanism 21 on the right side exhaust valve 11b drive
the valves open and closed, respectively. Further, a variable air intake timing mechanism
22 on the foregoing left and right side air intake valves 7a, 7b, and a fixed air
intake timing mechanism 23 on the center air intakes valves drive them open and closed,
respectively. The left and right side exhaust valves 11a, 11b are the same length.
[0038] The foregoing fixed air intake timing mechanism 23 has a conventional structure.
A center cam nose 12a formed on the air intake camshaft 12 directly drives the air
intake lifter 10a to open and close the air intake valve 7. On the other hand, the
fixed exhaust timing mechanism 20 has a right exhaust rocker arm 24 between the right
side cam nose 13a formed on the exhaust camshaft and exhaust lifter 10b for the right
side exhaust valve. This right side rocker arm 24 runs parallel to the exhaust camshaft
at the front side of the exhaust lifter 10b and moreover it is slidably supported
by the exhaust rocker shaft 25 which rotatably passes through it.
[0039] Further, the variable exhaust timing mechanism 20 of the foregoing right side exhaust
valve 11a and the variable air intake timing mechanism 22 for the left and right side
air intake valves 7a, 7b are of the same basic structure except for the symmetrical
positioning of their respective drive slots which will be described below. Accordingly,
the following explanation will concern the variable air intake timing mechanism 22
for the left side air intake valve 7a.
[0040] The foregoing variable air intake timing mechanism 22 is structured so that the side
cam nose 26 on the air intake camshaft 12 corresponding to the left side air intake
valve 7a is shaped in a manner such that the side air intake lifter can be directly
driven or be driven by means of the rocker arm 28.
[0041] As is primarily shown in Figure 5, the foregoing side cam nose 26 is composed of
a guide circle 26a which is of slightly greater diameter than the casting skin area
26d of the camshaft, of a high speed nose 26b which is of the same diameter of the
base circle but has a lift amount
a appropriate for the opening timing (operating angle) during high speed operations,
and a of low speed nose 26c which has lift
c and which has a base circle diameter that is slightly greater by the dimension
b (1 mm or less) than that of said high speed nose 26b. The approximate center of the
foregoing air intake lifter 10a is between the foregoing guide circle 26a and the
low speed nose 26c.
[0042] The air intake rocker shaft 27 rotatably passes through the rear side of the foregoing
air intake lifter 10a and it runs parallel to the camshaft 12. In the areas on this
air intake rocker shaft 27 corresponding to the left and right air intake lifters
10a, 10a, as will be described further below, are left and right drive slots 31, 31',
and there are a left drive slot 31 and a left side right drive slot 31' for the left
side air intake valve which is shaped differently than that for the right drive slot
31'.
[0043] Also, in the area of the foregoing left and right drive slots 31, 31' on the foregoing
rocker shaft 27 are fitted, annular left and right sliders 29 that can slide in the
axial direction. Each of the sliders 29 has a transmission pin 30 that projects radially.
The inside ends of said pins 30 are held in the foregoing drive slots 31, 31', and
the outside ends are held in guide holes 1h formed parallel to the rocker shaft in
the cylinder head 1. With this structure, when the rocker shaft 27 is rotated, the
foregoing sliders 29 move in the axial direction.
[0044] The foregoing left drive slots 31, 31' are composed of a slot area 31a that slants
to the axial line of the rocker shaft, and a retention area 31b which is at right
angles to the axial line of the rocker shaft, as is shown in Figure 6. Accordingly,
when the rocker shaft 27 is rotated in the direction of arrow
a shown in Figure 6, during the first half of the rotation, the foregoing transmission
pin 30 moves in the left drive slots toward the cylindrical axis, but it does not
move further during the second half. On the other hand, on the drive slot 31 side,
there is no movement during the first half, but during the second half of the rotation
there is movement toward the cylinder axis.
[0045] The structure for the rocker shaft 25 drive slot on the exhaust side is similar to
that of the foregoing left side drive slot 31, the first half of the rotation of the
rocker arm causes the slider to move but will be held stationary through the second
half of the rotation.
[0046] Attached to the foregoing rocker shaft 27 is the above-mentioned rocker arm 28, which
is in contact with the end surface of the foregoing slider 29, and said rocker arm
28 is free to slide and to move in the axial direction. There is a spring 32 held
by a spring receiver 32a in contact with the anti-slider end surface of said rocker
arm 28, and the other end of the spring is in held by a spring receiver 32a in the
support boss 1g formed in the cylinder head 1. In this manner, the rocker arm 28 is
normally held on the side of the high speed nose 26b.
[0047] Thus, the rocker arm 28 with the foregoing structure follows the movement of the
foregoing slider 29; when said rocker arm 28 is positioned farther away from the cylindrical
axis by the slider 29, then it lies between the foregoing guide circle 26a and the
lifter 10a (in the non-operational position), and when it is positioned closer to
the cylindrical bore (the inside end) it lies between the foregoing high speed cam
nose 26b and the lifter 10 (the operational position).
[0048] There is a pinion unit 25b, 27b formed on the left ends of the foregoing exhaust
and air intake rocker shafts 25, 27, and these pinion units engage a rack unit formed
on the output shaft of a hydraulic actuator that is located in the left end of the
cam chamber. A control signal is fed into a switching oil pressure valve in an oil
pressure circuit for the foregoing hydraulic actuator 33 by an ECU (not shown). The
control will be described in detail for the valve shutdown control, variable valve
opening and closing timing, and variable valve lift control. To wit, the foregoing
ECU functions as a positioning means for the rocker arms in this invention.
[0049] Next, the operational effects of the embodiment's apparatus will be explained.
[0050] When the engine is operating at low speeds, the air intake and exhaust rocker shafts
25, 27 are held in the low speed position, and the transmission pins 30 on the sliders
29 lie in the low speed position (the outside end) in the various drive slots 31,
31', to position the sliders toward the outside. Accordingly, the rocker arm 28 lies
in the non-operational position between the guide circle 26a and the lifter 10a. As
a result, the rocker arm 28 does not swing, and the low speed cam nose 26c directly
drives the lifter 10a. Accordingly, the left side exhaust valve 11a and the left and
right side air intake valves 7a, 7b are lifted only slightly by the low speed cam
nose 26c to a lift height c which keeps the valves virtually in a shutdown condition.
[0051] The center air intake valve is always opened and closed at a fixed timing and lifts
according to the nose shape and nose height of the center cam nose 12a which opens
and closes the center air intake valve opening no matter what the engine RPM range,
while the exhaust rocker arm 24, based upon its rocker ratio, opens and closes the
right side exhaust valve opening 5b at a fixed timing and lift.
[0052] When a change is made from low speed to mid-speed engine operations, the rocker shaft
27 is rotated to the mid-speed position and the transmission pins 30 move to the mid
speed position in the drive slots 31, 31'. In this case, transmission pin 30 for the
drive slot 31' for the right side air intake valve is not displaced in the axial direction,
so that the right side valve 7b remains virtually shut down just as it was during
the above described low speed operations.
[0053] On the other hand, the transmission pins 30 are moved axially in the drive slot 31
for the foregoing left side exhaust valve 11a and the left side air intake valve 7a
to advance their rocker arms 28 to between the high speed nose 26b and the lifter
10a or 10b, thereby driving the left side exhaust valve 11a and the left side air
intake valve 7a opened and closed by means of the high speed cam nose 26b and the
rocker arms 28. As a result, the two exhaust valves, and two of the air intake valves
are operating, while one air intake valve is shut down.
[0054] The above described switching operation is performed as follows. When, in response
to a switching signal, the foregoing hydraulic actuator rotates the rocker shafts
25, 27 as shown in Figure 6 from the low speed position to the mid-speed position,
the slider 29 moves toward the inside and the cylindrical axis due to the transmission
pin 30 moving in the drive area 31a of the drive slot 31. At this time, when the camshaft
rotates from the position (shown in Figure 2) where the side surface of the high speed
cam nose 26b is sliding against the side surface of the rocker arm 28 (the side facing
the cam nose) to the position corresponding to where the foregoing opposite surfaces
are at the base circle position, the spring force against the foregoing rocker arm
28 will cause it to slide toward the slider 29, advancing it to the position between
the high speed cam nose 26b and the lifter 10a.
[0055] After that, the rotational action by the high speed cam nose is transmitted to the
lifter 10a, or lifter 10b by means of the rocker arm 28 with the result that the foregoing
left side exhaust valve 11a and the left side air intake valve 7a are opened and closed,
respectively, according to the nose shape and height of the high speed cam nose 26b
and the rocker ratio of the rocker arm 28.
[0056] When a transition is made from mid-speed to high speed operations, the rocker shaft
27 is rotated to its high speed position and the rocker pins 30 move to the high speed
positions in the drive slots 31, 31'. In this case, the transmission pins 30 for the
left side exhaust valve and the left side air intake valve do not move. On the other
hand, the transmission pin for the right side air intake valve moves toward the inside
in the drive area 31a of the drive slot 31', thereby causing the right side air intake
valve 7b to begin operating. As a result, all the valves are operational.
[0057] Also, when making the transition from high speed to mid-speed and then to low speed
operations, the transition is made from all the valves being operational to shutting
down one of the air intake valves, followed by a condition where two of the air intake
valves and one of the exhaust valves are shut down. Making the transition from operational
to shutdown occurs by rotating the rocker shafts 25, 27 in the reverse direction as
described above. In this case, the sliders 29 directly slide the rocker arm 28 from
the position shown in Figure 10 to the position shown in Figure 9 or Figure 8 without
respect to the angular position of the camshaft.
[0058] Thus in the current embodiment, since there is a high speed cam nose 26b and a low
speed cam nose 26c with a larger diameter base circle, the rocker arm 28 can be advanced
into an operational position between the high speed cam nose 26c and the lifter 10a
or withdrawn into the non-operational position, thereby making it possible to shut
down two air intake valves and one exhaust valve during low speed operations, and
to shut down one exhaust valve during mid-speed operations, thereby shutting down
valves on the basis of the operating state of the engine.
[0059] Here, since the low speed cam nose 26c has but a slight nose height
c, even when the foregoing valves are in a shutdown period, the foregoing valves 11a,
7a, and 7b are opening and closing slightly, eliminating the possibility of fuel remaining
in the vicinity of the valve opening and preventing the buildup of carbon and other
deposits in the area of the exhaust valve opening.
[0060] Further, with regard to the switching structure that switches from low speed to mid-speed
to high speed operations, because the rocker shaft 27 forcibly slides the slider 29,
and the spring 32 pressing against the rocker arm 38 causes it to follow the movement
of the-slider, so-called synchronized movement has been made possible; and the movement
of a plurality of rocker arms 28 can be performed unobstructed in multi-cylinder engines.
[0061] Incidentally, in the case where the structure is such that the rocker arms are directly
moved by the rocker shaft without using any springs, the rocker arm must move at the
point when the rocker's side surface is positioned at the base circle of the cam nose.
However, in the case of a four-cylinder engine, it is normally the case that the valve
opening timing for each of the cylinders is different, and it would usually be impossible
to set the timing for the rocker arms of all four cylinders to move to the base circle
of the cam nose at the same time. Accordingly, in the case of four-cylinder engines,
it is difficult to adopt a direct moving structure for the rocker arms, although it
would be possible for a single-cylinder engine, and even possible for two-cylinder
engines if the movement could be set between the combustion intervals.
[0062] Further, in the rocker arm 28's non-operational position (shutdown position), since
the present embodiment uses a guide circle 26a which is formed to the same diameter
as the base circle of the high speed cam nose 26b, there can be a smooth transition
from the shutdown position of the rocker arm 28 to the operational position. Even
if the guide circle 26a is designed to be of somewhat larger diameter (10µm for example)
than the base circle of the high speed nose 26b, there is almost no impediment to
the foregoing transition.
[0063] Further, since the present embodiment continues the normal operation of the center
air intake valve 7c while two of the three air intake valves are shut down, and because
the left and right side exhaust valves 7a, 7b are shut down and put on variable timing,
not only is it easy to secure the space required for said shifting mechanism, but
in addition, since the center air intake valve 7c is the only valve imparting direction
to the air intake during low speed operations, which directs it in the axial direction
of the cylinder, the resulting tumbling action stabilizes lean combustion.
[0064] While the foregoing first embodiment allows one air intake valve to operate during
low speed operations, two to operate during mid-speed operations and three to operate
during high-speed operations, it is possible to select the number of operating valves
by the shape of the foregoing drive slots 31, 31'.
[0065] Further, while the present embodiment uses a nose of 1 mm or less for the low speed
nose 26c that virtually shuts down the valve, it is of course possible to employ any
nose shape and height appropriate to low speed operations for said low speed nose
26c, thereby allowing different opening and closing timing and lift between low speed
operations and mid-/high speed operations.
[0066] Further, in the present embodiment, the rocker arms are shifted between an operational
position between the high speed nose and the lifter, and a non-operational position
outside that position, and the freedom in design of the shape of the nose can be further
broadened by using a structure that makes the rocker arm slidable between a high speed
nose and a lifter and between a low speed nose and a lifter.
[0067] The foregoing embodiment describes the case where the center cam nose 12a presses
against the lifter 10a to directly drive the center air intake valve 7c open and closed,
but this drive could equally well be performed through a rocker arm.
[0068] Figures 11 and 12 show an example where the center air intake valve 7c is driven
by a rocker arm 28'. In this example the center bearing 14', composed of the bearing
15a formed in the head and the cam cap, has been divided into two parts which sandwich,
on the left and right sides, the air intake lifter 10a, and a center rocker arm 28'
is positioned between the left and right sections. The foregoing head cap is removably
held in place by four bolts that thread into the head side bearings 14a.
[0069] Figures 13 through 18 will be used to explain a second embodiment.
[0070] In the Figures, parts that are the same as those in Figures 1 through 12 bear the
same reference numbers. This second embodiment is an example wherein the transition
time for the rocker arm to move from the non-operational position to the operational
position is much greater than the transition time for the movement in the opposite
direction.
[0071] The engine used in this second embodiment is the same engine used in the foregoing
first embodiment, and the basic structure of the dynamic valve apparatus is the same
as that of the first embodiment, except that the rocker shafts have a double walled
pipe structure composed of an inner rocker shaft and outer rocker shaft. To wit, the
inner rocker shaft 41 on the air intake side is rotatably and axially supported by
the support boss 1g and the center bearings 14, but it is incapable of movement in
the axial direction. It can be rotated by means of the actuator 33.
[0072] An outer rocker shaft 42 is installed coaxially around the outside circumference
of the foregoing inner rocker shaft 41 and is rotatable with respect to it. The ends
of said outer rocker shaft 42 are in contact with the foregoing support boss 1g and
with the end surface of the center bearing 14 and it cannot move in the axial direction.
[0073] Left and right drive slots 43, 44 are formed in the areas of the foregoing inner
rocker shaft 41 and outer rocker shaft 42 that correspond to the left and right side
air intake valves, as shown in Figure 14. Said left drive slot 43 is composed of inner
and outer left drive slots 45,46 formed in the inner and outer rocker shafts 41, 42,
respectively. The right drive slot 44 is composed of the inner and outer right drive
slots 47 and 48 formed in the inner and outer rocker shafts 41, 42, respectively.
[0074] The foregoing inner left drive slot 45 is composed of: a holding slot 45a, which
extends at right angles (in the circumferential direction) with respect to the axial
line a of the rocker shaft to form the operational position holding slot which holds
the foregoing transmission pin 30 and the slider in the operational position; a non-operational
direction angular drive surface 45b that continues from said operational position
retention slot 45a and runs at an angle with respect to the rocker shaft axis
a, and which, in conjunction with the rotation of said inner rocker shaft 41, causes
the slider to move to the non-operational position; and a return drive surface 45c,
which is formed parallel to the rocker shaft axis
a, continuing from the foregoing operational position slot 45a, so that the slider
can return from the above described non-operational position to the operational position
without rotating the inner rocker shaft 41. Furthermore, the above mentioned outer
left drive slot 46 has a non-operational position retention slot 46a which holds the
foregoing slider in the non-operational position, and a guide slot 46 b, which extends
in parallel to the rocker shaft axis
a and which guides the movement of the foregoing slider 29 between the operational
and non-operational positions.
[0075] The foregoing inner right drive slot 47 is composed of: a non operational direction
angular drive surface 47a, which is formed at an angle with respect to the rocker
shaft axis
a, and which with the rotation of the inner rocker shaft 41 causes the foregoing slider
to move to the non-operational position; and a return drive surface 47b which is formed
parallel to the rocker shaft axis and which, without the rotation of the inner rocker
shaft 41, allows the slider 29 to return from the foregoing non-operational position
to the operational position. Furthermore, the foregoing outer right drive slot 48
has a non-operational position retaining slot 48a that extends perpendicularly with
respect to the rocker shaft axis
a and which holds the foregoing slider in the non-operational position, and a guide
slot 48b which extends in parallel to the rocker shaft axis.
[0076] The exhaust rocker shaft is composed of an inner rocker shaft 52 which can be rotated
by the foregoing actuator 33, and an outer rocker shaft 52, which can rotate with
respect to the inner rocker shaft 51 but which cannot move axially. As is shown in
Figure 18, an inner drive slot and outer drive slot are formed in both of said rocker
shafts 51, 52. Said inner drive slot 53 is formed at an angle with respect to the
rocker shaft axis and it has a non-operational direction slanted drive surface 53a
that drives the foregoing slider 29 to the non-operational position and a return drive
surface 53b that is formed parallel to the rocker axis. Further, the foregoing outer
drive slot 54 has a non-operational position retention slot which retains the foregoing
slider in the non-operational position, and a guide slot which runs parallel to the
rocker shaft and which guides the movement of the foregoing slider between the operational
and non-operation positions, parallel to the rocker shaft.
[0077] Next, the operation of the present embodiment will be explained.
[0078] First, the operation on the air intake side will be explained. In Figures 15 and
16, the drive slots 45 for the left and right side air intake valves have been flipped
upside-down from the position shown in Figure 14 for the purpose of seeing the action
of the transmission pins for the left and right side air intake valves.
[0079] When the engine is operating in the high speed range as shown in Figure 15 (a), the
inner rocker shaft is at the right side position (the high speed operating position),
and the transmission pins 30, in other words, the sliders 29, are positioned in the
inner left and right drive slots 45, 47 in the left edge of the Figure, as well as
in the left and right outer drive slots in the lower part of the Figure. This positions
the left and right side air intake rocker arms 28 in the operating position, and as
a result, the three intake valves, including the left and right side air intake valves
7a, 7b, and the center air intake valve 7c, are all being driven by the high speed
nose through the rocker arms.
[0080] When the engine is operating in the mid-speed range as shown in Figure 15 (b) - (e),
the inner rocker shaft 41 is rotated to the middle position (the mid-speed operations
position), which is to the left with respect to the Figure, whereupon the slider 29
for the right side air intake valve is moved by the non-operational direction slanted
drive surface 47a in the axial direction and upward to the non-operational position
side, while the rocker arm 28 for the right side is pushed into the non-operational
position against the force of the spring 32 (see the position in Figure 13). This
design causes the right side air intake valve 7b to be driven open and closed by the
low speed nose 26c, thereby setting it into a virtually shutdown condition.
[0081] In this case, since the slider 29 for the left side air intake valve 7a is maintained
in the operating retention slot 45a of the inner left drive slot 45, even when the
inner rocker shaft 41 is rotated, it does not move axially, but rather, the left side
air intake valve 7a continues to operate.
[0082] On the other hand, when the engine is in the low speed operating range, as shown
by Figure 15 (f) - (i), the inner rocker shaft 41 is rotated to its left side position
(the low speed operating position) and the slider 29 for the left side air intake
valve is moved axially and upwardly as shown in the Figure (downward in Figure 13)
by the non-operational position direction slanted drive surface 45b of the inner left
drive slot 45 that moves the slider 29t and the rocker arm 28 for the left side air
intake valve into the non-operational position. This feature causes the left side
air intake valve to be driven by the low speed nose 26c, setting it into a virtual
shutdown state. Also, the transmission pin 30 for the left side air intake valve is
held in the non-operational position retention area 46a of the outer left drive slot
46.
[0083] When the foregoing inner rocker shaft 41 is rotated to the left side in Figure 15,
the transmission pin 30 of the right side air intake valve moves further to the left
due to the inner left drive slot 47, but at this time, since it remains within the
non-operational position retention slot 48a of the outer left drive slot 48, the left
side air intake valve maintains a virtually shutdown state.
[0084] In the above described low speed operating range, only the center air intake valve
remains operational, while the left and right side air intake valves are virtually
shut down, but, as shown in Figure 15 (j) - (l) when the inner rocker shaft 41 is
rotated to the right side shown in the Figure to the low speed operation holding position.
In other words, when the inner rocker shaft 41 is rotated to the right from the foregoing
left side position to just before the foregoing middle position, this feature causes
the transmission pin 30 for the right side air intake valve to come into contact with
the return drive surface 45c of the inner drive slot 45, and it is held in this position.
[0085] Then, when the engine again reaches the mid-speed operating range, as shown in Figure
15 at steps (m), (n), rotating the inner rocker shaft 41 just slightly to the right
achieves the foregoing mid-speed operating position. When this event happens, the
return drive surface 45c of the inner left drive slot causes the transmission pin
30 to be pushed to the right side shown in the Figure, away from the retention slot
46a of outer left drive slot 46. This design causes the transmission pin 30 to be
immediately moved to the operating position by the foregoing spring force, to immediately
render the left side air intake valve operational.
[0086] Also, when returning to low speed operations, as shown in Figure 15 at steps (o)
- (r), the inner rocker shaft 41 is rotated to the left to the low speed operating
position, and the transmission pin 30 for the left side air intake valve is moved
in the axial direction to once again put the left side air intake valve into a virtually
shutdown condition, and further rotation brings it into the low speed operation holding
position (Figure, steps 16 (a) - (c)).
[0087] Further still, when moving toward the mid-speed operational state, the left side
air intake valve becomes operational immediately ( Figure 15, (d), (e)). In this mid-speed
operating range, the center air intake valve 7c and the left side air intake valve
7a are operating, while the right side air intake valve 7b remains virtually shut
down. However, when the inner rocker shaft 41 is rotated to the mid-speed operation
holding position as shown in Figure 16 in steps (f) - (i), the latter valve remains
holding in that position. To wit, when the inner rocker arm 41 is rotated from the
foregoing middle position to just before the foregoing right side position, the transmission
pin 30 for the right side air intake valve is in contact with the return drive surface
47b of the inner right drive slot 47, and it is held in this position.
[0088] Then, for high speed operations, as shown in Figure 16 in steps (j), (k), the slight
rotation of the inner rocker shaft 41 to the right causes the foregoing far-right,
high speed operations position to be assumed. This feature causes the transmission
pin 30 to be pushed to the right by the return drive surface 47b of the inner right
drive slot 47 from the retaining slot 48a of the outer right drive slot 48, whereupon
the foregoing spring force causes the transmission pin 30 to be immediately returned
to the operating position, thereby bringing the right side air intake valve into immediate
operation.
[0089] With regard to the exhaust side, during high and mid-speed operating ranges, as shown
in Figure 17a, the inner rocker shaft 51 is positioned in the high and mid-speed operating
position on the right side shown in the Figure, and the transmission pin 30 is in
its operating position so that both the left and right side exhaust valves 11a, 11b
are operating.
[0090] When the engine is changed to a low speed operating state, the inner rocker shaft
51 is rotated to the left as shown in the Figure to the low speed operating position,
and the non-operational direction slanted drive surface 53a of the inner drive slot
53 causes the transmission pin 30 to move to the non-operational position, and said
transmission pin 30 is retained in the retention slot 54a of the outer drive slot
54 ( Figure 17 (b) - (f)), thereby putting the left exhaust valve in a shutdown condition.
[0091] Then, during the foregoing low speed operations, when the inner rocker shaft 51 is
rotated to just before the foregoing right side high and mid-speed operating position,
the transmission pin 30 comes into contact with the return drive surface 53b of the
inner drive slot 53 which is a holding position ( Figure 17, steps (g) - (j)), so
that if a transition is made once again to high speed operations, the inner rocker
shaft 51 can be rotated to the right slightly, causing the transmission pin 30 to
be pushed from the foregoing retention slot 54a and immediately returned to the operating
position by the above described spring force. As a result, the shut down left exhaust
valve 11a is immediately returned to operation.
[0092] Thus, in this second embodiment, when the air intake valve(s) and exhaust valve are
shut down (to a non-operational state) from an operating state, the inner rocker shafts
41, 51 must be rotated through the entire angular length of the slanted drive surfaces
45b, 47a, and 53a, but on the other hand, when making a transition from a shutdown
state to an operational state, the inner rocker shafts 41, 51 need only to be slightly
rotated, thereby making the switch from a shutdown state to an operational state instantaneous.
[0093] For example, as is shown in Figure 14b, the change from an operational state to a
non-operational state (reducing the number of operational valves) takes 0.7 second,
while the switch from a non-operational state to an operational state (increasing
the number of operating valves) takes only 0.1 second. Although there might be some
concerns over diminished acceleration response when valves are shut down, the present
embodiment avoids this potential problem by immediately restoring shut down valves
to operation, thereby avoiding the foregoing diminished acceleration response.
[0094] In the present embodiment, the time when the rocker arms can be moved axially into
the operating position is restricted to the time interval when the base circle of
the high speed cam 26b is positioned on the rocker arm side, and the higher the RPM,
the shorter this interval. However since the present embodiment requires but a short
interval for switching to the operational position, it is advantageous from this perspective
as well.
[0095] The present embodiment further sets the engine RPM at which switching is made to
the non-operational state to be lower than that at which switching is made to the
operational state. In other words, there is hysteresis involved in the number of switchings,
and avoiding frequent switching between operational and non-operational states avoids
the problem of so-called hunting.
[0096] In the foregoing embodiments, the left and right side air intake valves were shut
down during low-speed operations, and one was returned to the operational state during
mid-speed operations, and the remainder was rendered operational in the high speed
operating range, thereby achieving valve shut down in stages, but the invention may
also be applied of course to the shutting down and restorations of a single valve,
or, a plurality of valves may be shut down at one time.
[0097] According to the dynamic valve apparatus in one embodiment of the invention, when
the rocker arms are in the operating position, the rotational movement of the cam
nose is transmitted to the valves by the rocker arms, and when they are in the non-operational
position, the valves are operated directly by the rotational movement of the cam nose,
thereby allowing variable control of valve lift based upon the axial position of the
rocker arms.
[0098] According to another embodiment of the invention, by constituting the cam nose of
a high speed nose and a low speed nose, by putting the rocker arm into the operational
position so that the rotational movement of the high speed cam nose is transmitted
to the valve by the rocker arm, and by directly transmitting the rotational movement
of the low speed cam nose to the valves when the rocker arm is in the non-operational
position, it is possible to vary the amount of lift and the opening and closing timing
according to the nose shapes of the low speed nose and the high speed nose and according
to the lift height. Further, by setting the lift of the low speed nose to approximately
zero, it is possible to place valves into a shutdown state using a very simple structure.
[0099] According to a further embodiment of the invention , by installing the foregoing
variation apparatus on one of the exhaust valves and upon the left and right side
air intake valves, and by setting the foregoing low speed nose shape to virtually
shut down the opening and closing operation, it is possible during low speed engine
operations, to virtually shut down one of the foregoing exhaust valves, and the left
and right side air intake valves and leave the other exhaust valve and the center
valve operational, and, during mid-speed engine operations, it is possible to shut
down the right or the left side air intake valve and leave the other two, as well
as the two exhaust valves operational, and further, during high speed engine operations,-to
have all the valves operational, thereby achieving a three-stage valve shutdown control
that corresponds to the operating state of the engine.
[0100] Further, during low speed operations, since only the center air intake valve from
among the three intake valves is left operational, the air entering the cylinders
is directed in the axial direction of the cylinders to generate a tumbling action,
which is effective in stabilizing the combustion at lean air/fuel ratios.
[0101] According to still another embodiment of the invention, because the displacement
speed of the rocker arms from the non-operational to the operational position is higher
than in the reverse direction, it is possible to immediately increase the number of
operational valves during rapid acceleration, which is effective in improving acceleration
response.
[0102] According to a still further embodiment of the invention , since on the one hand
the amount of rotation of the inner rocker shaft causes a proportional movement of
the rocker arm from the operational position to the non-operational position, while
on the other, the rocker arms may be moved from the non-operational to the operational
position without the rotation of the inner rocker shaft, it is possible to make a
speedier transition in moving the rocker arm from the non-operational to the operational
position than is in the reverse direction.
1. Internal combustion engine comprising a cylinder body (2) having at least one cylinder
(2a), a cylinder head (1) provided with each a plurality of air intake and exhaust
valves (7a-7c;11a,11b) actuatable via air intake and exhaust camshafts (12,13) in
cooperation with respective rocker arms (28) mounted at respective exhaust and intake
rocker shafts (25,27) and associated with said cylinder (25, and a dynamic valve apparatus
(20,22) being capable to variably control the valve opening and closing timing, the
valve lift, and the shut down of at least some of said air intake and exhaust valves
(7a,11a), characterized in that the dynamic valve apparatus (20,22) comprising a moving mechanism (29-33) for moving
respective rocker arms (28) between an operational position in which a cam nose (26)
of each of said camshafts (12,13) is in sliding contact with said rocker arms (28)
and a non-operational position in which said rocker arm (28) is offset of said cam
nose (26) in axial direction of said exhaust and intake rocker shafts (25,27) in accordance
with detected engine operational conditions, said moving mechanism (29-33) being adapted
to operate at least one of said air intake valves (7a,7b) being disposed at both sides
of a plane containing a central axis of the cylinder (2a) and a center intake valve
(7c) which is always operative, and at least one of the exhaust valves (11a, 11b).
2. Internal combustion engine according to claim 1, characterized in that said cam (26) comprises a guide circle (26a) engagable by said rocker arm (28) and
constituting said non-operational position and a high speed nose (26b) engagable by
said rocker arm (28) and constituting said operational position.
3. Internal combustion engine according to claim 1 or 2, characterized in that said cam (26) further comprises a low speed nose (26c) contacting said respective
air intake valve (7a) or exhaust valve (11a), respectively, when said rocker arm (28)
is in said non-operational position.
4. Internal combustion engine according to claim 3, characterized in that said low speed nose (26c) has a larger rotational diameter than said high speed nose
(26b).
5. Internal combustion engine according to at least one of claims 1 to 4, characterized in that said moving mechanism comprises sliders (29) slidingly mounted on said exhaust and
intake rocker shafts (25,27) and being movable by a transmission pin (30) guidable
by respective drive slots (31,31') formed in said exhaust and intake rocker shafts
(25,27) for pushing said rocker arms (28) from a first position to a second position,
a spring (32) for urging said rocker arms (28) back to said first position when said
sliders (29) are released from said rocker arms (28), and an actuator (33) rotating
said exhaust and intake rocker shafts (25,27) to actuate said sliders (29).
6. Internal combustion engine according to at least one of claims 1 to 5, characterized in that three air intake valves (7a-7c) and two exhaust valves (11a,11b) are symmetrically
arranged to both sides of said plane containing said central axis of said cylinder
(2a).
7. Internal combustion engine according to claim 6, characterized in that said moving mechanism (29-33) is capable of moving said respective rocker arms (28)
of said two air intake valves (7a-7c) and said one exhaust valve (11a,11b) into said
non-operational position in a low speed condition of said engine.
8. Internal combustion engine according to claim 7, characterized in that during a mid-speed condition of said engine only one air intake valve (7a-7c) is
movable into said non-operational position.
9. Internal combustion engine according to at least one of claims 1 to 8, characterized in that said moving mechanism (29-33) is capable to move said respective rocker arms (28)
from said non-operational position to said operational position with a higher speed
than from said operational position to said non-operational position.
10. Internal combustion engine according to at least one of claims 1 to 9, characterized in that said moving mechanism (29-33) is controllable by an engine control unit (ECU).
11. Internal combustion engine according to at least one of claims 5 to 10, characterized in that said moving mechanism (29,30,32,33) further comprises inner rocker shafts (41,51)
provided with respective inner drive slots (45,47,53), outer rocker shafts (42,52)
coaxially aligned with said inner rocker shafts (41,51) and provided with respective
outer drive slots (46,48,54) in such a manner that they are rotatable with respect
to each other.
12. Internal combustion engine according to at least one of claims 6 to 11, characterized in that all exhaust and air intake valves (11a,11b,7a-7c) are operable by said moving mechanism
(29-33).
13. Method for controlling the valve actuation of an internal combustion engine comprising
a cylinder body (2) having at least one cylinder (2a), a cylinder head (1) provided
with a plurality of air intake and exhaust valves (7a, 11a) actuatable via air intake
and exhaust camshafts (12,13) in cooperation with respective rocker arms (28) mounted
at respective exhaust and intake rocker shafts (25,27) and associated with said cylinder
(2a), and a dynamic valve apparatus (20,22) being capable to variably control the
valve opening and closing timing, the valve lift, and the shut down of at least some
of said air intake and exhaust valves (7a,11a), characterized by the steps of moving said rocker arms (28) by means of said dynamic valve apparatus
(20,22) having a moving mechanism (29-33) between an operational position in which
a cam nose (26) of each of said camshafts (12,13) is in sliding contact with said
rocker arm (28) and a non-operational position in which said rocker arm (218) is offset
of said cam nose (26) in axial direction of said exhaust and intake rocker shafts
(25,27) in accordance with detected engine operational conditions, wherein at least
one of said air intake valves (7a, 7b) being disposed at both sides of a plane containing
a central axis of the cylinder (2a) and a center intake valve (7c) which is always
operative, and at least one of the exhaust valves (11a, 11b) being operated by said
moving mechanism (29-33).
14. Method according to claim 13, characterized in that during a low speed condition of said engine, said two air intake valves (7a-7c) and
said one exhaust valve (11a,11b) are moved to said non-operational position.
15. Method according to claim 13 or 14, characterized in that in a mid-speed condition of said engine only one air intake valve (7a-7c) is moved
into said non-operational position.
16. Method according to at least one of claims 13 to 15, characterized in that an engine control unit (ECU) controls said moving mechanism (29-33).
1. Brennkraftmaschine mit einem Zylinderkörper (2), der zumindest einen Zylinder (2a)
hat, einem Zylinderkopf (1), versehen mit jeweils einer Mehrzahl von Lufteinlaß- und
Auslassventilen (7a - 7c; 11a; 11b), betätigbar über Lufteinlaß- und Luft-auslaßnockenwellen
(12, 13) im Zusammenwirken mit jeweiligen Unterbrecherhebeln (28), montiert an jeweiligen
Auslaß- und Einlassunterbrecherwellen (25, 27) und verbunden mit dem Zylinder (2a),
und einer dynamischen Ventilvorrichtung (20, 22), die in der Lage ist, den Ventilöffnungs-
und - schließzeitpunkt, den Ventilhub, und das Abschalten von zumindest einigen der
Lufteinlaß- oder Auslassventile (7a, 11a) veränderbar zu steuern, dadurch gekennzeichnet, daß die dynamische Ventilvorrichtung (20, 22) mit einer Bewegungsvorrichtung (29 - 33)
zum Bewegen der jeweiligen Unterbrecherhebel (28), zwischen einer Betriebsposition,
in der eine Nockennase (26) jeder der Nockenwellen (12, 13) in Gleitkontakt mit den
Unterbrecherhebeln (28) ist und einer Nichtbetriebsposition, in der der Unterbrecherhebel
(28) der Nockennase (26) in axialer Richtung der Auslaß- und Einlassunterbrecherwellen
(25, 27) versetzt ist, in Übereinstimmung mit den erfassten Motorbetriebsbedingungen,
wobei die Bewegungsvorrichtung (29 - 33) vorgesehen ist, zumindest eines der Lufteinlassventile(7a,
7b), vorgesehen zu beiden Seiten einer Ebene, die eine Mittelachse des Zylinders (2a)
und ein Mittel- Einlassventil (7c), das ständig betreibbar ist, enthält, und zumindest
eines der Auslassventile (11a, 11b), zu betätigen.
2. Brennkraftmaschine nach Anspruch 1, dadurch gekennzeichnet, dass der Nokken (26) einen Führungskreis (26a) aufweist, eingreifbar durch den Unterbrecherhebel
(28) und der die Nichtbetriebsposition bildet und eine Hochdrehzahlnase (26b), ergreifbar
durch den Unterbrecherhebel (28) und der die Betriebsposition bildet.
3. Brennkraftmaschine nach Anspruch 1 oder 2, dadurch gekennzeichnet, dass der Nocken (26) außerdem eine Niedrigdrehzahlnase (26c) aufweist, die das jeweilige
Lufteinlassventil (7a) oder Auslaßventil (11a) jeweils berührt, wenn der Unterbrecherhebel
(28) in der Nichtbetriebsposition ist.
4. Brennkraftmaschine nach Anspruch 3, dadurch gekennzeichnet, dass die Niedrigdrehzahlnase (26c) einen größeren Drehdurchmesser als die Hochdrehzahlnase
(26b) hat.
5. Brennkraftmaschine nach zumindest einem der Ansprüche 1 bis 4, dadurch gekennzeichnet, dass die Bewegungsvorrichtung Gleiter (29) aufweist, die gleitend auf den Auslaß- und
Einlassunterbrecherwellen (25, 27) montiert sind und die durch einen Übertragungsbolzen
(30) beweglich sind, führbar durch jeweilige Antriebsschlitze (31, 31'), die in den
Auslaß- und Einlassunterbrecherwellen (25, 27) gebildet sind, um die Unterbrecherhebel
(28) von einer ersten Position zu einer zweiten Position zu drücken, eine Feder (32)
zum Zurückdrücken der Unterbrecherhebel (28) in die erste Position, wenn die Gleiter
(29) von den Unterbrecherhebeln (28) freigegeben sind, und einen Betätiger (33), der
die Auslaß- und Einlassunterbrecherwellen (25, 27) dreht, um die Gleiter (29) zu betätigen.
6. Brennkraftmaschine nach zumindest einem der Ansprüche 1 bis 5, dadurch gekennzeichnet, dass drei Lufteinlassventile (7a - 7c) und zwei Auslassventile (11a, 11b) symmetrisch
zu beiden Seiten der Ebene, die die Mittelachse des Zylinders (2a) enthält, angeordnet
sind.
7. Brennkraftmaschine nach Anspruch 6, dadurch gekennzeichnet, dass die Bewegungsvorrichtung (29 - 33) in der Lage ist, die jeweiligen Unterbrecherhebel
(28) der zwei Lufteinlassventile (7a - 7c) und des einen Auslassventiles (11a, 11b)
in die Nichtbetriebsposition in einem Niedrigdrehzahlzustand des Motors zu bewegen.
8. Brennkraftmaschine nach Anspruch 7, dadurch gekennzeichnet, dass während eines mittleren Drehzahlzustandes des Motors nur ein Lufteinlaßventil (7a
- 7c) in die Nichtbetriebsposition bewegbar ist.
9. Brennkraftmaschine nach zumindest einem der Ansprüche 1 bis 8, dadurch gekennzeichnet, dass die Bewegungsvorrichtung (29 - 33) in der Lage ist, die jeweiligen Unterbrecherhebel
(28) von der Nichtbetriebsposition mit einer höheren Drehzahl als von der Betriebsposition
in die Nichtbetriebsposition zu bewegen.
10. Brennkraftmaschine nach zumindest einem der Ansprüche 1 bis 9, dadurch gekennzeichnet, dass die Bewegungsvorrichtung (29 - 33) durch eine Motorsteuereinheit (ECU) steuerbar
ist.
11. Brennkraftmaschine nach zumindest einem der Ansprüche 5 bis 10, dadurch gekennzeichnet, dass die Bewegungsvorrichtung (29, 30, 32, 33) außerdem aufweist innere Unterbrecherwellen
(41, 51), versehen mit jeweiligen inneren Antriebsschlitzen (45, 47,53), äußere Unterbrecherwellen
(42, 52), koaxial ausgerichtet mit den inneren Unterbrecherwellen (41, 51) und versehen
mit jeweiligen äußeren Antriebsschlitzen (46, 48, 54) in solch einer Weise, dass sie
in Bezug zueinander drehbar sind.
12. Brennkraftmaschine nach zumindest einem der Ansprüche 6 bis 11, dadurch gekennzeichnet, dass alle Auslaß- und Einlassventile (11a, 11b, 7a - 7c) durch die Bewegungsvorrichtungen
(29 - 33) betätigbar sind.
13. Verfahren zum Steuern der Ventilbetätigung einer Brennkraftmaschine mit einem Zylinderkörper
(2), der zumindest eine Zylinder (2a) hat, einem Zylinderkopf (1), versehen mit einer
Mehrzahl von Einlaß- und Auslassventilen (7a, 11a), betätigbar über Lufteinlaß- und
Luftauslassnockenwellen (12, 13) im Zusammenwirken mit jeweiligen Unterbrecherhebeln
(28), montiert an jeweiligen Auslaß- und Einlassunterbrecherwellen (25, 27) und verbunden
mit dem Zylinder (2a), und einer dynamischen Ventilvorrichtung (20, 22), die in der
Lage ist, den Ventilöffnungs- oder -schließzeitpunkt, den Ventilhub, und das Abschalten
von zumindest einigen der Lufteinlaß- oder Auslassventile (7a, 11a) veränderbar zu
steuern, gekennzeichnet durch die Schritte des Bewegens der Unterbrecherhebel (28) mittels der dynamischen Ventilvorrichtung
(20, 22), die eine Bewegungsvorrichtung (29 - 33) hat, zwischen einer Betriebsposition,
in der eine Nockennase (26) jeder der Nockenwellen (12, 13) in Gleitkontakt mit dem
Unterbrecherhebel (28) ist und einer Nichtbetriebsposition, in der der Unterbrecherhebel
(218) der Nockennase (26) in axialer Richtung der Auslaß- und Einlassunterbrecherwellen
(25, 27) versetzt ist, in Übereinstimmung mit den erfassten Motorbetriebsbedingungen,
wobei zumindest eines der Luftelnlassventile(7a, 7b), vorgesehen zu beiden Seiten
einer Ebene, die eine Mittelachse des Zylinders (2a) und ein Mittel- Einlassventil
(7c), das ständig betreibbar ist, enthält, und zumindest eines der Auslassventile
(11a, 11b) durch die Bewegungsvorrichtung (29 - 33) betätigt werden.
14. Verfahren nach Anspruch 13, dadurch gekennzeichnet, dass während eines Niedrigdrehzahlzustandes des Motors die zwei Luft- Einlassventile (7a
- 7c) und das eine Auslaßventil (11a, 11b) in den Nichtbetriebszustand bewegt werden.
15. Verfahren nach dem Anspruch 13 oder 14, dadurch gekennzeichnet, dass in einem mittleren Drehzahlzustand des Motors nur ein Lufteinlassventil (7a - 7c)
in den Nichtbetriebszustand bewegt wird.
16. Verfahren nach zumindest einem der Ansprüche 13 bis 15, dadurch gekennzeichnet, dass eine Motorsteuereinheit (ECU) die Bewegungsvorrichtung (29 - 33) steuert.
1. Moteur à combustion interne, comprenant un bloc-cylindres (2) comportant au moins
un cylindre (2a), une culasse (1) dotée, pour chaque cylindre, d'une pluralité de
soupapes d'admission d'air et d'échappement (7a-7c ; 11a, 11b) pouvant être actionnées,
par l'intermédiaire d'arbres à cames d'admission d'air et d'échappement (12, 13),
en coopération avec des culbuteurs respectifs (28) montés sur des axes de culbuteurs
d'échappement et d'admission respectifs (25, 27) et associés audit cylindre (2a),
et un dispositif dynamique pour soupapes (20, 22) apte à commander, de façon variable,
la synchronisation d'ouverture et de fermeture des soupapes, le soulèvement des soupapes
et l'obturation d'au moins certaines desdites soupapes d'admission d'air et d'échappement
(7a, 11a), caractérisé en ce que le dispositif dynamique pour soupapes (20, 22) comprenant un mécanisme de déplacement
(29-33) destiné à déplacer les culbuteurs respectifs (28) entre une position opérante
dans laquelle un bossage de came (26) de chacun desdits arbres à cames (12, 13) se
trouve en contact de coulissement avec lesdits culbuteurs (28) et une position inopérante
dans laquelle ledit culbuteur (28) est déporté par rapport audit bossage de came (26)
suivant une direction axiale desdits axes de culbuteurs d'échappement et d'admission
(25, 27) en fonction des conditions opérantes détectées du moteur, ledit mécanisme
de déplacement (29, 33) étant conçu pour commander au moins l'une desdites soupapes
d'admission d'air (7a, 7b) qui sont disposées des deux côtés d'un plan contenant un
axe central du cylindre (2a) et une soupape d'admission centrale (7c) qui demeure
toujours opératoire, et au moins l'une des soupapes d'échappement (11a, 11b).
2. Moteur à combustion interne selon la revendication 1, caractérisé en ce que ladite came (26) comprend un cercle de guidage (26a) pouvant être mis en prise par
ledit culbuteur (28) et constituant ladite position inopérante, et un bossage de haute
vitesse (26b) pouvant être mis en prise par ledit culbuteur (28) et constituant ladite
position opérante.
3. Moteur à combustion interne selon la revendication 1 ou 2, caractérisé en ce que ladite came (26) comprend, en outre, un bossage de basse vitesse (26c) venant au
contact de ladite soupape d'admission d'air (7a) ou de ladite soupape d'échappement
(11a) respective, respectivement, lorsque ledit culbuteur (28) se trouve dans ladite
position inopérante.
4. Moteur à combustion interne selon la revendication 3, caractérisé en ce que ledit bossage de basse vitesse (26c) possède un diamètre de rotation supérieur à
celui dudit bossage de haute vitesse (26b).
5. Moteur à combustion interne selon au moins l'une des revendications 1 à 4, caractérisé en ce que ledit mécanisme de déplacement comprend des pièces coulissantes (29) montées, pour
pouvoir coulisser, sur lesdits axes de culbuteurs d'échappement et d'admission (25,
27) et étant déplacées par une goupille de transmission (30) pouvant être guidée par
des rainures d'entraînement respectives (31, 31') pratiquées dans lesdits axes de
culbuteurs d'échappement et d'admission (25, 27) de manière à pousser lesdits culbuteurs
(28) d'une première position à une seconde position, un ressort (32) destiné à pousser
lesdits culbuteurs (28) en les ramenant à ladite première position lorsque lesdites
pièces coulissantes (29) sont libérées desdits culbuteurs (28), et un actionneur (33)
faisant tourner lesdits axes de culbuteurs d'échappement et d'admission (25, 27) afin
d'actionner lesdites pièces coulissantes (29).
6. Moteur à combustion interne selon au moins l'une des revendications 1 à 5, caractérisé en ce que trois soupapes d'admission d'air (7a-7c) et deux soupapes d'échappement (11a, 11b)
sont symétriquement disposées sur les deux côtés dudit plan contenant ledit axe central
dudit cylindre (2a).
7. Moteur à combustion interne selon la revendication 6, caractérisé en ce que ledit mécanisme de déplacement (29-33) est apte à déplacer lesdits culbuteurs respectifs
(28) desdites deux soupapes d'admission d'air (7a-7c) et de ladite une soupape d'échappement
(11a, 11b) dans ladite position inopérante dans une condition de basse vitesse dudit
moteur.
8. Moteur à combustion interne selon la revendication 7, caractérisé en ce que, au cours d'une condition de vitesse intermédiaire dudit moteur, seule une soupape
d'admission d'air (7a-7c) peut être déplacée dans ladite position inopérante.
9. Moteur à combustion interne selon au moins l'une des revendications 1 à 8, caractérisé en ce que ledit mécanisme de déplacement (29-33) est apte à déplacer lesdits culbuteurs respectifs
(28) de ladite position inopérante à ladite position opérante avec une vitesse supérieure
à celle avec laquelle il les déplace de ladite position opérante à ladite position
inopérante.
10. Moteur à combustion interne selon au moins l'une des revendications 1 à 9, caractérisé en ce que ledit mécanisme de déplacement (29-33) peut être commandé par une unité de commande
de moteur (ECU).
11. Moteur à combustion interne selon au moins l'une des revendications 5 à 10, caractérisé en ce que ledit mécanisme de déplacement (29, 30, 32, 33) comprend, en outre, des axes de culbuteurs
intérieurs (41, 51) pourvus de fentes d'entraînement intérieures respectives (45,
47, 53), d'axes de culbuteurs extérieurs (42, 52) alignés coaxialement auxdits axes
de culbuteurs intérieurs (41, 51) et pourvus de fentes d'entraînement extérieures
respectives (46, 48, 54) de telle manière qu'ils peuvent être mis en rotation les
uns par rapport aux autres.
12. Moteur à combustion interne selon au moins l'une des revendications 6 à 11, caractérisé en ce que toutes les soupapes d'échappement et d'admission d'air (11a, 11b, 7a-7c) peuvent
être commandées par ledit mécanisme de déplacement (29-33).
13. Procédé pour commander l'actionnement des soupapes d'un moteur à combustion interne
comprenant un bloc-cylindres (2) comportant au moins un cylindre (2a), une culasse
(1) pourvue d'une pluralité de soupapes d'admission d'air et d'échappement (7a, 11a)
pouvant être actionnées, par l'intermédiaire d'arbres à cames d'admission d'air et
d'échappement (12, 13), en coopération avec des culbuteurs respectifs (28) montés
sur des axes de culbuteurs d'échappement et d'admission respectifs (25, 27) et associés
audit cylindre (2a), et un dispositif dynamique pour soupapes (20, 22) étant apte
à commander, de façon variable, la synchronisation d'ouverture et de fermeture des
soupapes, le soulèvement des soupapes et l'obturation d'au moins certaines desdites
soupapes d'admission d'air et d'échappement (7a, 11a), caractérisé par les étapes consistant à déplacer lesdits culbuteurs (28) au moyen dudit dispositif
dynamique pour soupapes (20, 22) comportant un mécanisme de déplacement (29-33) entre
une position opérante dans laquelle un bossage de came (26) de chacun desdits arbres
à cames (12, 13) est en contact de coulissement avec ledit culbuteur (28) et une position
inopérante dans laquelle ledit culbuteur (218) est déporté par rapport audit bossage
de came (26) suivant une direction axiale desdits axes de culbuteurs d'échappement
et d'admission (25, 27) en fonction des conditions opérantes détectées du moteur,
dans lequel au moins l'une desdites soupapes d'admission d'air (7a, 7b) qui sont disposées
sur les deux côtés d'un plan contenant un axe central du cylindre (2a) et une soupape
d'admission centrale (7c) qui demeure toujours opératoire, et au moins l'une des soupapes
d'échappement (11a, 11b) étant commandée par ledit mécanisme de déplacement (29-33).
14. Procédé selon la revendication 13 caractérisé en ce que, au cours d'une condition de basse vitesse dudit moteur, lesdites deux soupapes d'admission
d'air (7a-7c) et ladite une soupape d'échappement (11a, 11b) sont déplacées vers ladite
position inopérante.
15. Procédé selon la revendication 13 ou 14, caractérisé en ce que, dans une condition de vitesse intermédiaire dudit moteur, seule une soupape d'admission
d'air (7a-7c) est déplacée dans ladite position inopérante.
16. Procédé selon au moins l'une des revendications 13 à 15, caractérisé en ce qu'une unité de commande de moteur (ECU) commande ledit mécanisme de déplacement (29-33).