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Patent Abstract
In an internal combustion engine with variable actuation valves,
each variable actuation valve is actuated by an actuator assembly
including an actuating piston slidably mounted in a guide bushing.
Between the actuating piston and the stem of the respective valve
is interposed an auxiliary hydraulic tappet positioned outside the
guide bushing of the actuating piston, so that said bushing can
be dimensioned with a relatively small diameter, regardless of the
outer diameter of the auxiliary hydraulic tappet. The intake valves
of a same cylinder are actuated by a single cam, by means of a single
pumping piston and by means of a single pressure chamber controlled
by a single solenoid valve.
Patent Claims
1. A multi-cylinder internal combustion engine, comprising: at least
one intake valve and at least one exhaust valve for each cylinder,
each provided with respective return spring means which bias the
valve towards a closed position, to control respective intake and
exhaust conduits, at least one camshaft, to actuate the intake and
exhaust valves of the engine cylinders by means of respective tappets,
in which at least each intake valve has variable actuation, being
actuated by the respective tappet, against the action of the aforesaid
return spring means, by the interposition of hydraulic means including
a pressurised fluid chamber, into which projects a pumping piston
connected to the tappet of the intake valve, said pressurised fluid
chamber being able to be connected by means of a solenoid valve
with an exhaust channel, in order to uncouple the variable actuation
valve from the respective tappet and cause the rapid closure of
the valve by effect of the-respective return spring means, electronic
control means for controlling each solenoid valve in such a way
as to vary the time and travel of opening of the variable actuation
valve as a function of one or more operative parameters of the engine,
in which the aforesaid hydraulic means further comprise an actuation
assembly for each variable actuation valve, including an actuating
piston slidably mounted in a guide bushing, said actuating piston
facing a variable volume chamber communicating with the pressurised
fluid chamber both through first communication means controlled
by a check valve which allows only the passage of the fluid from
the pressurised fluid chamber to the variable volume chamber, and
through second communication means which allow the passage between
the two chambers in both directions, in which said hydraulic means
further comprise hydraulic braking means able to cause a narrowing
of said second communication means in the final phase of closure
of the engine valve, in which between the actuating piston of each
variable actuation valve and the stem of the valve is interposed
an auxiliary hydraulic tappet, in which said auxiliary hydraulic
tappet comprises: a first bushing having an end wall in contact
with one end of the stem of the variable actuation valve, a second
bushing slidably mounted within said first bushing and having an
end in contact with a corresponding end of said actuating piston,
a first chamber defined between said second bushing and said actuating
piston, which is in communication with a passage for feeding the
pressurised fluid to said first chamber, a second chamber defined
between said first bushing and said second bushing, and a check
valve which controls a passage in a wall of said second bushing
to allow the passage of fluid only from said first chamber to said
second chamber of said auxiliary hydraulic tappet, wherein said
first bushing of the auxiliary hydraulic tappet is mounted outside
the guide bushing of the actuator piston, and wherein for each cylinder
of the engine are provided at least two variable actuation valves,
which are controlled by a single cam by means of a single pumping
piston and by means of a single pressure chamber, controlled by
a single solenoid valve and communicating hydraulically with the
variable volume chambers of the actuator units of said at least
two valves.
2. Engine as claimed in claim 1, wherein it comprises a single
camshaft having cams which mechanically actuate the exhaust valves
of the engine and cams which actuate the engine intake valves by
means of said pumping pistons.
3. Engine as claimed in claim 1, wherein the inner diameter of
the guide bushing is considerably smaller than the outer diameter
of said first bushing of the auxiliary hydraulic tappet.
4. Engine as claimed in claim 1, wherein the second bushing of
the auxiliary hydraulic tappet is positioned outside the guide bushing.
5. Engine as claimed in claim 1, wherein the second bushing of
the auxiliary hydraulic tappet is positioned inside the guide bushing
of the actuating piston.
6. Engine as claimed in claim 5, wherein the actuating piston has
one end with reduced diameter positioned inside the aforesaid second
bushing of the auxiliary hydraulic tappet.
Patent Description
BACKGROUND OF THE INVENTION
[0001] The present invention relates to internal combustion engines
with multiple cylinders, of the type comprising: [0002] at least
one intake valve and at least one exhaust valve for each cylinder,
each provided with respective return spring means which bias the
valve towards a closed position, to control respective intake and
exhaust conduits, [0003] at least one camshaft, to actuate the intake
and exhaust valves of the engine cylinders by means of respective
tappets, [0004] in which each intake valve has variable actuation,
being actuated by the respective tappet, against the action of the
aforesaid return spring means, by the interposition of hydraulic
means including a pressurised fluid chamber, into which projects
a pumping piston connected to the tappet of the intake valve, [0005]
said pressurised fluid chamber being able to be connected by means
of a solenoid valve with an exhaust channel, in order to uncouple
the variable actuation valve from the respective tappet and cause
the rapid closure of the valve by effect of the respective return
spring means, [0006] electronic control means for controlling each
solenoid valve in such a way as to vary the time and travel of opening
of the variable actuation valves as a function of one or more operative
parameters of the engine, [0007] in which the aforesaid hydraulic
means further comprise an actuator unit for each variable actuation
valve, including an actuating piston slidably mounted in guide bushing,
[0008] said actuating piston facing a variable volume chamber communicating
with the pressurised fluid chamber both through first communication
means controlled by a check valve which allows only the passage
of the fluid from the pressurised fluid chamber to the variable
volume chamber, and through second communication means which allow
the passage between the two chambers in both directions, [0009]
in which said hydraulic means further comprise hydraulic braking
means able to cause a narrowing of said second communication means
in the final phase of closure of the engine valve, [0010] in which
between the actuating piston of each variable actuation valve and
the stem of the valve is interposed an auxiliary hydraulic tappet,
[0011] in which said auxiliary hydraulic tappet comprises: [0012]
a first bushing having an end wall in contact with one end of the
stem of the variable actuation valve, [0013] a second bushing slidably
mounted within said first bushing and having one end in contact
with a corresponding end of said actuating piston, [0014] a first
chamber defined between said bushing and said actuating piston,
which is in communication with a passage for feeding the pressurised
fluid to said first chamber, [0015] a second chamber defined between
said first bushing and said second bushing, and [0016] a non return
valve which controls a passage in a wall of said second bushing
to allow the passage of fluid only from said first chamber to said
second chamber of said auxiliary hydraulic tappet.
SUMMARY OF THE INVENTION
[0017] An engine of the type specified above is described for example
in the European patent application EP 1 344 900 A2 by the same Applicant.
[0018] In engines of this kind, it is important that the closing
motion of each valve, determined by the spring means associated
with the valve at the time in which the pressurised chamber of the
actuating system is discharged, be as fast as possible, to be braked
in the final phase of the travel of the valve by the aforesaid hydraulic
braking means. This requirement is particularly important when the
engine is started at low temperature. However, there are limits
to the possibility of making the closing phase of the valve substantially
instantaneous, which derive in particular from the mass of the moving
members, from the load of the spring means which return the valve
to the closed position and from the viscosity of the fluid (the
engine lubricating oil) used in the hydraulic system. To increase
the closing speed of the valve, it would in particular be advantageous
to minimise the diameter of the aforesaid variable volume chamber
which is defined by the actuating piston of the valve within the
related guide bushing, since said chamber must be emptied of oil
during the return movement of the actuating piston caused by the
closing of the valve. However, in known solutions, here too there
is a limit to the possibility of reducing said diameter, since the
inner diameter of the guide bushing of the actuating piston must
be sufficient to house the aforesaid auxiliary hydraulic tappet
which is interposed between the actuating piston and the stem of
the valve. If a tappet of any conventional type available on the
market is to be used, the diameter of said tappet cannot be reduced
beyond a certain limit.
[0019] To eliminate or at least reduce said drawbacks, the Applicant
has already proposed in its European patent application EP 04 425
683.2 (still secret as of the filing date of the present application)
an engine of the type indicated at the start of the present description,
characterised in that said first bushing of the auxiliary hydraulic
tappet is mounted outside the guide bushing of the actuating piston.
[0020] Thanks to said characteristic, in the engine according to
the prior proposal the dimensioning of the inner diameter of the
guide bushing of the actuating piston of the valve becomes completely
independent of the outer dimension of the aforesaid auxiliary hydraulic
tappet. It is thus possible, in particular, to adopt a guide bushing
of the actuating piston with a smaller inner diameter than the outer
diameter of said auxiliary hydraulic tappet. Therefore, it is possible
considerably to reduce the diameter of said variable volume chamber
with respect to known solutions, with consequent possibility of
greatly accelerating the valve closing motion.
[0021] The object of the present invention is further to improve
the prior proposal.
[0022] To achieve said object, the present invention relates to
an engine of the type indicated at the start of the present description,
characterised in that said first bushing of each auxiliary hydraulic
tappet is mounted outside the guide bushing of the actuating piston,
and
[0023] in that for each cylinder of the engine are provided at
least two variable actuation valves, preferably at least two intake
valves, which are controlled by a single cam by means of a single
pumping piston and by means of a single pressure chamber, controlled
by a single solenoid valve and communicating hydraulically with
all variable volume chambers of the actuator units of said at least
two valves.
[0024] The Applicant has discovered that the disposition of the
auxiliary hydraulic tappets outside the guide bushings of the respective
actuating pistons results in the further advantage of making it
concretely possible to provide a single pumping piston and a single
solenoid valve to actuate multiple valves for each cylinder. This
last characteristic is advantageous in itself from the viewpoint
of the simplicity and of the low fabrication cost, in addition to
the reduction of the dimensions, relative to the solution that comprises
one pumping piston and one solenoid valve for each valve of the
engine. However, an efficient and reliable operation of a system
having a single pressure chamber communicating hydraulically with
multiple valve actuator units is possible only if the volumes of
the hydraulic chambers are kept extremely small, which in fact,
as has been seen, can be achieved effectively thanks to the adoption
of the characteristic in accordance with the prior proposal. The
provision of the auxiliary hydraulic tappets outside the guide bushings
of the respective actuator pistons allows to reduce the inner diameter
of said bushings by the necessary extent, with the consequent reduction
of the hydraulic chambers defined within them. The disposition of
the auxiliary hydraulic tappets outside the guide bushings of the
respective actuating pistons enables to reduce by the necessary
extent the inner diameter of said bushings, with the consequent
reduction of the hydraulic chambers defined within them.
[0025] An additional important advantage of the invention resides
in the fact that, thanks to the ability to reduce the diameter of
the actuator pistons of the valves, the volume of oil present in
the chamber of each actuator unit is minimised, which allows to
achieve the goal of making nearly instantaneous, and anyway very
fast, the closure of the engine valves when the pressure chamber
is discharged by means of the respective solenoid valve, which constitutes
an essential element for the efficiency of the system.
BRIEF DESCRIPTION OF THE DRAWINGS
[0026] The invention shall now be described with reference to the
accompanying drawings, provided purely by way of non limiting example,
in which:
[0027] FIG. 1 is a section view of a prior art engine, of the type
described for example in European Patent EP 0 803 642 B1 by the
same Applicant, which is shown herein to illustrate the fundamental
principles of a variable actuation system of the valves,
[0028] FIG. 2 is a section view in enlarged scale of an auxiliary
hydraulic tappet associated with an intake valve of an engine of
a type similar to that of FIG. 1, as previously proposed in the
European Patent application EP 1 344 900 by the Applicant,
[0029] FIG. 3 is a schematic section view of an auxiliary hydraulic
tappet in an engine according to the present invention,
[0030] FIG. 4 is a similar view to FIG. 3, showing an embodiment
example,
[0031] FIG. 5 shows a diagram that illustrates the advantages of
the invention,
[0032] FIG. 6 is a schematic view of a system according to the
invention,
[0033] FIGS. 7 and 8 are diagrams which show the advantages of
the invention, and
[0034] FIGS. 9, 10 illustrate two section views of an embodiment
of the system according to the invention.
DETAILED DESCRIPTION OF THE INVENTION
[0035] With reference to FIG. 1, the internal combustion engine
described in the prior European patent application EP-A-0 803 642
by the same Applicant is a multi-cylinder engine, for instance an
engine with four cylinders in line, comprising a cylinder head 1.
The head 1 comprises, for each cylinder, a cavity 2 formed in the
base surface 3 of the head 1, defining the combustion chamber, into
which end two intake conduits 4, 5 and two exhaust conduits 6. The
communication of the two intake conduits 4, 5 with the combustion
chamber 2 is controlled by two intake valves 7, of the traditional
mushroom type, each comprising a stem 8 slidably mounted in the
body of the head 1. Each valve 7 is returned towards the closed
position by springs 9 interposed between an inner surface of the
head 1 and an end cup 10 of the valve. The opening of the intake
valves 7 is controlled, in the manner described below, by a camshaft
11 rotatably mounted around an axis 12 within supports of the head
1, and comprising a plurality of cams 14 for actuating the valves.
[0036] Each cam 14 which controls an intake valve 7 co-operates
with the washer 15 of a tappet 16 slidably mounted along an axis
17 which, in case of the example illustrated in the aforementioned
prior document, was directed substantially at 90.degree. relative
to the axis of the valve 7. The tappet 16 is slidably mounted within
a bushing 18 borne by a body 19 of a pre-assembled set 20 incorporating
all the electrical and hydraulic devices associated to the actuation
of the intake valves, as described in detailed below. The tappet
16 is able to transmit a bias to the stem 8 of the valve 7, in such
a way as to cause the opening thereof against the action of the
spring means 9, by means of pressurised fluid (typically oil from
the engine lubrication loop) present in a pressure chamber C, and
a piston 21 mounted slidably in a cylindrical body constituted by
a bushing 22 which is also borne by the body 19 of the subgroup
20. In the known solution shown in FIG. 1, the pressurised fluid
chamber C associated to each intake valve 7 can be placed in communication
with the exhaust channel 23 by means of a solenoid valve 24. The
solenoid valve 24, which can be of any known type, suited to the
function illustrated herein, is controlled by electronic control
means, schematically designated by the number 25, according to signals
S indicative of engine operating parameters, such as the position
of the accelerator pedal and the number of engine revolutions per
minute. When the solenoid valve 24 is opened, the chamber C comes
in communication with the channel 23, so the pressurised fluid present
in the chamber C flows into said channel and an uncoupling is obtained
of the cam 14 and of the respective tappet 16 from the intake valve
7, which then rapidly returns to its closed position under the action
of the return spring 9. By controlling communication between the
chamber C and the outlet channel 23, it is therefore possible to
vary at will the time and opening stroke of each intake valve 7.
[0037] The outlet channels 23 of the various solenoid valves 24
all end in a same longitudinal channel 26 communicating with pressure
accumulators 27, only one whereof is visible in FIG. 1. All the
tappets 16 with the associated bushings 18, the pistons 21 with
the associated bushings 22, the solenoid valves 24 and the related
channels 23, 26 are borne and formed in the aforesaid body 19 of
the pre-assembled set 20, to the advantage of the rapidity and ease
of assembly of the engine.
[0038] The exhaust valves 70 associated to each cylinder are controlled,
in the embodiment illustrated in FIG. 1, in traditional fashion,
by a respective camshaft 28, by means of respective tappets 29,
although in principle, both in the case of the prior document mentioned
above, and in the case of the present invention, an application
of the variable actuation system to command the exhaust valves is
not excluded.
[0039] Also with reference to FIG. 1, the variable volume chamber
defined inside the bushing 22 by the piston 21 (which in FIG. 1
is shown in its minimum volume condition, the piston 21 being in
its upper top stroke end position) communicates with the pressurised
fluid chamber C through an opening 30 obtained in an end wall of
the bushing 22. Said opening 30 is engaged by an end nose 31 of
the piston 21 in such a way as to obtain a hydraulic braking of
the motion of the valve 7 in the closing phase, when the valve is
near the closed position, since the oil present in the variable
volume chamber is forced to flow into the pressurised fluid chamber
C passing through the play existing between the end nose 31 and
the wall of the opening 30 engaged thereby. In addition to the communication
constituted by the opening 30, the pressurised fluid chamber C and
the variable volume chamber of the piston 21 communicate with each
other by means of internal passages formed in the body of the piston
21 and controlled by a check valve 32 which allows the passage of
fluid only from the pressurised chamber C to the variable volume
chamber of the piston.
[0040] During the normal operation of the prior art engine illustrated
in FIG. 1, when the solenoid valve 24 excludes the communication
of the pressurised fluid chamber C with the exhaust channel 23,
the oil present in this chamber transmits the motion of the tappet
16 imparted by the cam 14 to the piston 21 that commands the opening
of the valve 7. In the initial phase of the opening movement of
the valve, the fluid coming from the chamber C reaches the variable
volume chamber of the piston 21 passing through an axial hole 30
drilled in the nose, the check valve 32 and additional passages
which place in communication the inner cavity of the piston 21,
which has tubular shape, with the variable volume chamber. After
a first displacement of the piston 21, the nose 31 comes out of
the opening 30, so the fluid coming from the chamber C can pass
directly into the variable volume chamber through the opening 30,
which is now free. In the inverse movement of closure of the valve,
as stated, during the final phase the nose 31 enters into the opening
30 causing the hydraulic braking of the valve, to prevent any impacts
of the body of the valve against its seat.
[0041] FIG. 2 shows the device described above in the modified
form which was proposed in the previous European Patent application
EP 0 1 344 900 by the same Applicant.
[0042] In FIG. 2, the parts in common with FIG. 1 are designated
by the same reference number.
[0043] A first evident difference of the device of FIG. 2 with
respect to that of FIG. 1 is that in the case of FIG. 2, the tappet
16, the piston 21 and the stem 8 of the valve are mutually aligned
along an axis 40. This difference does not fall within the scope
of the invention, as it is already contemplated in the prior art.
Similarly, the invention would also apply to the case in which the
axes of the tappet 16 and of the stem 8 were to form an angle between
them.
[0044] Similarly to the solution of FIG. 1, the tappet 16, with
the related washer 15 which co-operates with the cam of the camshaft
11 is slidably mounted in a bushing 18. In the case of FIG. 2, the
bushing 18 is screwed into a threaded cylindrical seat 18a obtained
in the metal body 19 of the pre-assembled set 20. A sealing gasket
18b is interposed between the bottom wall of the bushing 18 and
the bottom wall of the seat 18a. A spring 18c returns the washer
15 in contact with the cam of the camshaft 11.
[0045] In the case of FIG. 2 also, as in FIG. 1, the piston 21
is slidably in a bushing 22 which is received in a cylindrical cavity
32 obtained in the metallic body 19, with the interposition of sealing
gaskets. The bushing 22 is held in the mounted condition by a threaded
ring nut 33 which is screwed in a threaded end portion of the cavity
32 and which presses the body of the bushing 22 against an abutment
surface 35 of the cavity 32. Between the locking ring nut 33 and
the flange 34 is interposed a Belleville washer 36 to assure a controlled
axial load to compensate for the differential thermal expansions
between the different materials constituting the body 19 and the
bushing 22.
[0046] The main difference of the prior art solution shown in FIG.
2 and the one, also known, of FIG. 1 is that in this case the check
valve 32 which allows the passage of pressurised fluid from the
chamber C to the chamber of the piston 21 is not borne by the piston
21 but rather by a separate element 37 which is fixed relative to
the body 19 and it superiorly closes the cavity of the bushing 22
within which is slidably mounted the piston 21. Moreover, the piston
21 does not have the complicated conformation of FIG. 1, with the
end nose 31, but it is shaped as a simple cup-like cylindrical element,
with a bottom wall facing the variable volume chamber which receives
pressurised fluid from the chamber C through the check valve 32.
[0047] The element 37 is constituted by an annular plate which
is locked in position between the abutment surface 35 and the end
surface of the bushing 22, as a result of the tightening of the
locking ring nut 33. The annular plate has a central cylindrical
projection which serves as a container for the check valve 32 and
which has an upper central hole for the passage of the fluid. In
the case of FIG. 2 as well, the chamber C and the variable volume
chamber delimited by the piston 21 communicate with each other,
as well as through the check valve 32, through an additional passage,
constituted by a lateral cavity 38 obtained in the body 19, a peripheral
cavity 39 defined by a flattening of the outer surface of the bushing
22, and by an opening (not showing in FIG. 2) of greater size and
a hole 42 of smaller size obtained radially in the wall of the bushing
22. These openings are shaped and mutually arranged in such a way
as to achieve operation with hydraulic brake in the final closing
phase of the valve, for when the piston 21 has obstructed the opening
of greater size, the hole 42 remains free, which intercepts a peripheral
end throat 43 defined by a circumferential end groove of the piston
21. To assure that the aforesaid two openings correctly intercept
the fixed passage 38, the bushing 34 must be mounted in a precise
angular position, which is assured by an axial pin 44. This solution
is preferred with respect to the arrangement of a circumferential
throat on the outer surface of the bushing 22, for this would entail
an increase in the oil volumes in play, with consequent drawbacks
in operation. A calibrated hole 320 is also provided in the element
37, which directly places the annular chamber defined by the throat
43 in communication with the chamber C. Said hole 320 assures correct
operation at low temperature, when the fluid (engine lubrication
oil) is very viscous.
[0048] In operation, when the valve needs to be opened, pressurised
oil, bias by the tappet 16, flows from the chamber C to the chamber
of the piston 21 through the check valve 32. As soon as the piston
21 has moved away from its upper end stop position, the oil can
then flow directly into the variable volume chamber through the
passage 38 and the two aforesaid openings (the larger one and the
smaller one 42), bypassing the check valve 32. In the return movement,
when the valve is near its closed position, the piston 21 intercepts
first the large opening and then the opening 42 determining the
hydraulic braking. A calibrated hole can also be provided in the
wall of the element 37 to reduce the braking effect at low temperatures,
when the viscosity of the oil would cause excessive slowing in the
movement of the valve.
[0049] As is readily apparent, the main different with respect
to the solution shown in FIG. 1 is that the operations for fabricating
the piston 21 are much simpler, since said piston has a far less
complicated conformation than the one contemplated in the prior
art. The solution according to the invention also allows to reduce
the oil volume in the chamber associated with the piston 21, which
allows to obtain a regular closing movement of the valve, without
hydraulic bounces, a reduction in the time required for closing,
a regular operation of the hydraulic tappet, without pumping, a
reduction in impulsive force in the springs of the engine valves
and reduction in hydraulic noise.
[0050] An additional characteristic of the prior art solution shown
in FIG. 2 is the provision of a hydraulic tappet 400 between the
piston 21 and the stem 8 of the valve. The tappet 400 comprises
two concentric slidable bushings 401, 402. The inner bushing 402
defines with the inner cavity of the piston 21 a chamber 403 which
is fed a pressurised fluid through passages 405, 406 in the body
19, a hole 407 in the bushing 22 and passages 408, 409 in the bushing
402 and in the piston 21.
[0051] A check valve 410 controls a central hole in a frontal wall
borne by the bushing 402.
[0052] In regard to the present invention, FIG. 3 shows a schematic
section view of the end wall of the actuating piston 21 of a variable
actuation valve and the related guide bushing 22, as well as the
auxiliary hydraulic tappet 400 associated with the actuator assembly
constituted by the piston 21 and by the bushing 22. As FIG. 3 clearly
shows, the main difference with respect to the prior art solution
illustrated in FIG. 2 is that in this case the auxiliary hydraulic
tappet 400 is completely positioned outside the actuator assembly
of the variable actuation valve. More specifically, the first bushing
401 of the auxiliary hydraulic tappet 400 is not positioned inside
the guide bushing 22. Thanks to this characteristic, the dimensioning
of the guide bushing 22 is completely independent of the dimensions
of the auxiliary hydraulic tappet 400. This is an advantage, since,
if a hydraulic tappet of any conventional type available on the
market is to be used, the outer diameter of said tappet cannot be
reduced beyond a certain limit. On the other hand, there is an advantage,
as discussed at the start of the present description, in reducing
the diameter of the guide bushing 22, since said reduction in diameter
entails a reduction in the quantity of oil which must flow out of
the variable volume chamber defined inside the guide bushing 22
from the upper end of the piston 21 when the engine valve has to
close. It is thereby possible to obtain a substantial reduction
in the closing time of the valve, with consequent advantages in
terms of the efficient operation of the engine, with respect to
the prior art solution illustrated in FIG. 2.
[0053] With reference again to FIG. 3, the inner chamber 403 of
the hydraulic tappet is fed with oil from the engine lubrication
loop in similar fashion to the one illustrated in FIG. 2. The oil
coming from a feeding channel 405 (2) reaches a circumferential
chamber 406 (3) defined by an outer peripheral throat of the guide
bushing 22. From said circumferential chamber 406, the oil flows,
through a radial hole 407 obtained in the wall of the guide bushing
22 into a peripheral chamber 408 defined by a circumferential throat
of the outer surface of the piston 21. Thence the oil passes into
the chamber 403 through a radial hole 409 obtained in the wall of
the piston 21. The communication between the chamber 403 defined
between the piston 21 and the bushing 402, and the chamber 411 defined
between the two bushings 401, 402, is controlled by the check valve
410, subjected to the action of the return spring 412. The operation
of the actuator assembly 21, 211 and of the auxiliary hydraulic
tappet 400 is wholly similar to the one described above with reference
to prior art solutions.
[0054] In the case of the solution illustrated in FIG. 3, both
bushings 401, 402 constituting the auxiliary hydraulic tappet 400
are positioned outside the guide bushing 22 of the actuator piston
21.
[0055] FIG. 4 shows a variant, wholly similar, in principle, to
the solution of FIG. 3, which differs therefrom in that only the
bushing 401 of the auxiliary hydraulic tappet 400 is positioned
outside the guide bushing 22, whilst the bushing 402 is mounted
within it. Otherwise, the solution shown in FIG. 4 differs from
the solution shown only schematically in FIG. 3 solely in some constructive
details. FIG. 4 also partially shows the upper end of the stem 8
of the valve with the respective return valve 9 and the respective
end element 10 for bearing the spring 9.
[0056] FIG. 5 is a diagram that shows the advantages of the invention.
It illustrates the displacement X of the engine valve in the closing
phase, as the angle of the drive shaft changes in three different
situations. Diagrams A and B refer to the case in which, all other
dimensions being equal, the inner diameter of the guide bushing
22 of the piston is respectively 11 mm (diagram A) and 9 mm (diagram
B). The solution A substantially corresponds to the one illustrated
in FIG. 2, while the solution B becomes possible thanks to the present
invention, because of the positioning of the auxiliary hydraulic
tappet 14 outside the valve actuator assembly. As is readily apparent,
the angle of rotation of the drive shaft required to obtain the
complete closing of the valve is substantially reduced in the case
of the present invention.
[0057] Naturally, a determining factor influencing the closing
speed of the valve is the ratio between the narrow passage area
of the solenoid valve (24, FIG. 1) through which the oil present
in the chamber of the actuator assembly returns into the low pressure
area (23, FIG. 1) and the area of the chamber of the actuator assembly,
defined by the upper end of the piston 21 inside the guide bushing
22. The diagram C shows the situation of an ideal actuator, in which
the ratio between said areas is equal to 1. Obviously, this solution
cannot be achieved in practice, but it is interesting to note that,
thanks to the invention, a closing speed of the valve is obtained
(diagram B) that is not much lower than the ideal solution represented
by diagram C.
[0058] FIG. 6 is a schematic view of the system according to the
invention. In this figure, the parts in common with those of the
previous figures are designated with the same reference number.
The figure shows two intake valves 7 associated to a same cylinder
of an internal combustion engine, which are controlled by a single
pumping piston 16, in turn actuated by a single cam of the engine
camshaft (not shown) acting against its washer 15. The figure does
not show the return springs 9 (see FIG. 1) which are associated
to the valves 7 and tend to return them to the respective closed
positions.
[0059] As is readily apparent, in the system according to the invention
a single pumping piston 16 actuates the two valves 7 by means of
a single pressure chamber C, whose communication with the exhaust
is controlled by a single solenoid valve 24. This solution thus
allows obvious advantages in terms of simplicity and economy of
construction and from the viewpoint of bulk reduction.
[0060] The sole pressure chamber C is hydraulically in communication
with both variable volume chambers C1, C2 which face the pistons
21 that actuate the two valves.
[0061] The system according to the invention is able to operate
efficiently and reliably especially if the volumes of the hydraulic
chambers are relatively small. This possibility is offered by the
adoption of hydraulic tappets 400 outside the bushings 22, because
by so doing the bushings 22 can have an inner diameter that can
be chosen as small as is desired.
[0062] It should also be added that the possible differences in
displacement of the two valves 7, due to slight differences in the
load of the springs 9 associated to them, do not compromise the
proper operation of the system, since, due to the hydraulic connection,
all other conditions being equal, the identical rise of the two
valves in the theoretical case of identical springs is equal to
the mean of the two real rises in the case of springs with different
loads. The comprehension of this aspect has enabled the Applicant
to intuit the practical advantages of the system illustrated herein
and the absence of any drawback from the operative viewpoint.
[0063] FIG. 7 shows a diagram of the real lifts of the two intake
valves associated to each cylinder of the engine according to the
invention. These lifts differ from each other in the differences
of the load of the respective return springs 9, due to manufacturing
tolerances. As is readily apparent, the part of the diagram that
describes the closure of the valves corresponds to an extremely
small variation of the engine angle. This is allowed by the fact
that the diameter of the pistons 21 of the actuator units of the
valve can be considerably reduced relative to the measure that would
be necessary if the guide bushing 22 of each unit were to house
the tappet 400 in its interior. In a concrete case, the adoption
of the tappet 400 outside the bushing 22 has allowed to adopt a
diameter of only 9 mm for the piston 21, instead of 11 mm (measure
which would have been necessary to house a standard tappet). The
diagram of FIG. 8 shows a line A which refers to a conventional
solution of four-cylinder engine with two intake valves per cylinder
and a pumping piston per each valve. The line B refers to the system
according to the invention, with a single pumping piston for the
two intake valves of each cylinder. Both lines show the value of
the closing velocity of the valves, in metres per second, as a function
of the diameter of the piston 21. As is readily apparent, in the
conventional case (line A) a value of 11 mm of the diameter of the
piston 21 corresponds to a closing velocity of the valves in the
order of 4 metres per second. In the system according to the invention,
the adoption of a single pumping piston would produce a reduction
in the aforesaid velocity, but the possibility of adopting a value
of 9 mm for the diameter of the piston 21 associated to each valve
brings the velocity back to a value that is substantially equal
to that of the conventional system. Therefore, the system according
to the invention does not entail penalisations with respect to traditional
systems and at the same time it achieves a great simplification
and great savings in costs and size.
[0064] FIGS. 9 and 10 are a simplified section view and a schematic
perspective view of the components of the system according to the
invention in a practical embodiment. In these figures, too, the
parts in common with those of the previous figures are designated
with the same reference number. The illustrated example refers to
a particularly preferred solution, in which the intake valves 7
and the exhaust valves 70 are actuated by a single camshaft 11,
having cams 28 which mechanical actuate the exhaust valves 70 and
cams 14 which actuate four pumping pistons 16 associated to the
four cylinders of the engine, by means of respective rocker arms
500. Each rocker arm 500 supports at its centre in 501 a rotatable
roller for engagement with the respective cam 14, has one end pivotally
engaged to the structure 19 by means of a support 502 and the opposite
end acting against the washer 15 of the respective pumping piston
16. The upper part of FIG. 9, and FIG. 10, for the sake of clarity,
show only the components of the system, without showing the structure
19 in which they are mounted. The arrangement described and illustrated
above allows the additional advantage of simplifying the structure
of the engine and of containing the size of the system. In the illustrated
example, the tappets 29 and the rocker arms 500 co-operate with
regions that are angularly offset by about 90.degree. on the camshaft
11. Moreover, each of the four cams 14 which actuate the eight intake
valves is axially offset relative to both intake valves of the respective
cylinder of the engine. Naturally, without altering the principle
of the invention, the construction details and the embodiments may
be widely varied relative to what is described and illustrated purely
by way of example herein, without thereby departing from the scope
of the present invention. |