FIELD
[0001] The present disclosure relates to hydraulic devices.
BACKGROUND
[0002] Hydraulic pumps and motors are used predominantly in industry when mechanical actuation
is desired to convert hydraulic pressure and flow into torque and angular (rotation).
Examples of hydraulic application can be in braking systems, propulsion systems (e.g.
automotive, drilling) as well as in electrical energy generation systems (e.g. windmills).
Other common uses of hydraulic devices as a direct drive system can be in drilling
rigs, winches and crane drives, wheel motors for vehicles, cranes, and excavators,
conveyor and feeder drives, mixer and agitator drives, roll mills, drum drives for
digesters, kilns, trench cutters, high-powered lawn trimmers, and plastic injection
machines. Further, hydraulic pumps, motors, can be combined into hydraulic drive systems,
for example one or more hydraulic pumps coupled to one or more hydraulic motors constituting
a hydraulic transmission.
[0003] Due to currently available configurations, there exists disadvantages with hydraulic
devices when operated in systems exhibiting dynamic variation fluid flow requirements.
For example, the torque requirements of a load in a hydraulic system can dynamically
change, such that the hydraulic device must instantaneously react to the changing
flow conditions dictated by the dynamic change in the torque.
[0004] In terms of current axial piston pump configurations, there exists mechanical complications
in the design and use of variable angle rotating drive plates (i.e. wobble plate),
in order to dynamically change the fluid flow in response to the changing torque conditions.
As such, current axial piston pump designs tend to have higher than desired maintenance
costs and issues, are considered operationally inefficient as compared to other reciprocating
piston pump designs, and more importantly, current axial piston pumps and motors produce
vibration/noise (e.g. Fluidborne noise and Structuralborne Noise). These disadvantages
with current axial piston pump design are considered by the industry as the two primary,
potentially unsolvable and unwanted problems.
SUMMARY
[0005] It is an object of the present invention to provide a hydraulic device to obviate
or mitigate at least some of the above presented disadvantages.
[0006] A first aspect provided is a variable displacement hydraulic device comprising: a
housing having an inlet for receiving hydraulic fluid and an outlet for outputting
the hydraulic fluid, the housing having a reciprocation axis; a first cylinder positioned
in the housing along the reciprocation axis, the first cylinder having a first input
for receiving the hydraulic fluid on a first intake stroke and a first output for
ejecting the hydraulic fluid on a first exhaust stroke; a first piston positioned
for a first reciprocal motion within the first cylinder, the first piston having a
first main end exposed to the hydraulic fluid and a second main end coupled to an
actuator, the actuator for driving the second main end when coupled to the actuator
for causing the first reciprocal motion to induce a first portion of said outputting
of the hydraulic fluid; a second cylinder positioned in the first piston along the
reciprocation axis, the second cylinder having a second input for receiving the hydraulic
fluid on a second intake stroke and a second output for ejecting the hydraulic fluid
on a second exhaust stroke; a second piston positioned for a second reciprocal motion
within the second cylinder, the second piston having a first secondary end exposed
to the hydraulic fluid and a second secondary end coupled to the actuator, the actuator
for driving the second secondary end when coupled to the actuator for causing the
second reciprocal motion to induce a second portion of said outputting of the hydraulic
fluid; and a locking mechanism for inhibiting the first reciprocal motion of the first
piston; wherein when engaged the locking mechanism inhibits the first portion of said
outputting of the hydraulic fluid by decoupling the first piston from the actuator
while continued operation of the actuator provides the second portion of said outputting
of the hydraulic fluid by the second piston.
[0007] The hydraulic device has the second piston is concentrically positioned within the
first piston on the reciprocation axis.
[0008] The hydraulic device has the first output and the second output fluidly coupled at
the outlet.
[0009] The hydraulic device has the first input and the second input fluidly coupled at
the inlet.
[0010] The hydraulic device has the first main end and the second main end offset from one another
when the first main end is at a first Top Dead Center of the first reciprocal motion
and the first secondary end is at a second Top Dead Center of the second reciprocal
motion.
[0011] The hydraulic device has the first main end and the second main end offset from one
another by 180 degrees.
[0012] The hydraulic device has the first output fluidly coupled to the outlet and the second
output fluidly coupled to a second outlet of the housing, such that the first portion
is ejected from the outlet and the second portion is ejected separately from the second
outlet, the first output fluidly coupled to the outlet and the second output fluidly
coupled to the second outlet.
[0013] The hydraulic device has a first check valve positioned in the first input, a second
check valve positioned in the first output, a third check valve positioned in the
second input and a fourth check valve positioned in the second output.
[0014] The hydraulic device is a pump.
[0015] The hydraulic device is a motor.
[0016] The hydraulic device has rotation of a driveshaft coupled to the actuator in a clockwise
direction or a counter clockwise direction.
BRIEF DESCRIPTION OF THE DRAWINGS
[0017] The foregoing and other aspects will now be described by way of example only with
reference to the attached drawings, in which:
Figure 1 refers to a first embodiment of a hydraulic device;
Figure 2 is an view of the hydraulic device of Figure 1 in the full or maximum displacement
state;
Figure 3 is a view of the hydraulic device of Figure 1 in a first locked state for
variable displacement operation;
Figure 4 is a view of the hydraulic device of Figure 1 in a second locked state for
variable displacement operation;
Figure 5 is a view of the hydraulic device of Figure 1 in a third locked state for
variable displacement operation;
Figure 6A,B,C,D is an example operation of the hydraulic device of Figure 4 for variable
displacement operation;
Figure 7A,B,C,D is an example operation of the hydraulic device of Figure 3 for variable
displacement operation;
Figure 8A,B,C,D is an example operation of the hydraulic device of Figure 5 for variable
displacement operation, also referred to as pump unload operation;
Figure 9A,B,C,D,E,F provide further embodiments of the locking mechanism Figure 1;
Figure 10A,B are a side view of a further embodiment of the hydraulic device of Figure
1;
Figures 11A, B are a further embodiment and operation of the hydraulic device of Figures1-10A;
Figures 12A,B,C are further operations of the hydraulic device of Figures 11A,B;
Figures 13A,B, 14A,B and 15A,B are further examples of the cam of Figure 1;
Figures 16, 17 are examples of the hydraulic device of Figures 1-15A, B having multiple
piston-cylinder pairs/triplets, some of which being of different diameter bores; and
Figure 18 is a further alternative embodiment of the hydraulic device of Figure 1.
DETAILED DESCRIPTION
[0018] Referring to Figure 1, shown is a cutaway side view of a variable displacement hydraulic
device 20 (e.g. a pump or a motor) having a primary piston 105 and a secondary piston
115. The device 20 has a housing 25 having a common inlet 135 for receiving hydraulic
fluid and a common outlet 125 for outputting the hydraulic fluid, the housing 25 having
a reciprocation axis 11 for axial reciprocation 12, 13 of the primary piston 105 and
/ or the secondary piston 115 respectively. The housing has a main cylinder bore 110
positioned in the housing 25 along the reciprocation axis 11, the main cylinder bore
110 having a first input 112 (e.g. bore, passage, etc.) for receiving the hydraulic
fluid on a first intake stroke of the primary piston 105 and a first output 127 for
ejecting the hydraulic fluid on a first exhaust stroke of the primary piston 105.
It is recognized that the main / primary piston 105 is positioned for a first reciprocal
motion 12 within the main cylinder bore 110, the main piston 105 having a first main
end 105a exposed to the hydraulic fluid and a second main end 105b coupled to an actuator
85, the actuator 85 for driving the second main end 105b when coupled to the actuator
85 for causing the first reciprocal motion 12 to induce a first portion of the outputting
of the hydraulic fluid via the output 127, which can provide for a shared input and/or
output configuration, or a split flow configuration (see Figure 10). It is recognized
that coupling with the actuator 85 can be defined as when a surface 86 is adjacent
and in contact with the end(s) 105b, 115b. Alternatively, decoupled can be defined
as when the surface 86 is spaced apart from and thus out of contact with the end(s)
105b, 115b.
[0019] It is recognized that each of the pistons 105,115 operate on a fixed stroke length
when coupled to the actuator 85 (e.g. reciprocating between TDC and BDC). In view
of the fixed stroke length during operation of the hydraulic device 20 (for those
pistons 105,115 in an unlocked state - further described below), variability of hydraulic
device 20 throughput of hydraulic fluid (e.g. in pump mode or in motor mode) is done
by locking selected pistons 105, 115 rather than varying the length of the stroke
of piston(s) as is done in prior art pumps.
[0020] Referring again to Figure 1, the hydraulic device 20 has a second cylinder bore 120
positioned in the main piston 105 and in the housing 25 along the reciprocation axis
11 (e.g. concentric with the reciprocation axis 11 or non-concentric with the reciprocation
axis 11, as desired), the second cylinder bore 120 having a second input 113 for receiving
the hydraulic fluid on a second intake stroke and a second output 126 for ejecting
the hydraulic fluid on a second exhaust stroke. It is recognized that the second cylinder
bore 120 is comprised of two portions, a first portion 120a positioned in the housing
25 and a second portion 120b positioned in the min piston 105. In this manner, the
second cylinder bore 120 is made of two parts, namely 120a, 120b, which are aligned
to facilitate the second reciprocal motion 13 (e.g. axial) of the second piston 115.
Accordingly, the secondary piston 115 is positioned for the second reciprocal motion
13 within the second cylinder 120, the secondary piston 115 having a first secondary
end 115a exposed to the hydraulic fluid (located in the first portion 120a) and a
second secondary end 115b coupled to the actuator 85 (e.g. the same actuator 85 for
both the primary piston 105 and the secondary piston 115), the actuator 85 for driving
the second secondary end 115b when coupled to the actuator 85 for causing the second
reciprocal motion 13 in order to induce a second portion of the outputting of the
hydraulic fluid from the hydraulic device 20. Both the pistons 105, 115 are shown
in Figure 1 in a Top Dead Center (TDC) position in their respective bores 110, 120.
It is recognized that the main piston 105 can also be referred to as a secondary piston
105 and the second piston 115 can also be referred to as a secondary piston 115. Further,
the main piston 105 can be referred to as a first piston 105 and the secondary piston
115 can be referred to as a second piston 115. It is recognized that housing 25 can
contain multiple sets the first piston 105 and the second piston 115 as multiple sets
of pistons 105,115 (e.g. the housing 25 can contain two or more sets of pistons 105,115
- see Figures 16, 17, 18 as examples of multiple sets of pistons 105,115 for the hydraulic
device 20).
[0021] As shown in Figure 1 by example, the secondary piston 115 can be concentrically positioned
within the main piston 105 on the reciprocation axis 11, however other non-concentric
configurations can be provided, as desired. Further, by example, the first output
portion and the second output portion are fluidly coupled at the common outlet 125.
Further, by example, the first input portion and the second input portion are fluidly
coupled at the common inlet 135 (e.g. when the reciprocation 12 is occurring the hydraulic
fluid is drawn through the input 112 and when the reciprocation 13 is occurring the
hydraulic fluid is drawn through the input 113). It is recognized that the single
port inlet 135 (e.g. a single port fitting for the housing 25) can be coupled to a
common gallery 130, such that multiple sets of the pistons 105, 115 (of a multi piston
pair hydraulic device 20 - see Figure 16) can be provided hydraulic fluid at the same
time. It is also recognized that each set of pistons 105, 115 (e.g. a piston pair)
would have their own flow control valves SV1, SV2, such that variable displacement
mode vs full displacement mode can be controlled via each respective set of control
valves SV1, SV2, or another version of the locking mechanism 14, as desired. Further,
in the case of the hydraulic device 25 being a motor, inputs 112a, 113a adjacent to
the flow control valves SV!, SV2 can be utilized as common galleries.
[0022] A variable displacement mode for a piston pair 105, 115 can be when one or both of
the flow control valves SV1, SV2 is/are closed, e.g. the locking mechanism 14 is employed,
thus resulting in one or both of the pistons 105, 115 ceasing their reciprocal motion
12, 13 and thus becoming held at their respective TDC (i.e. decoupled from the actuator
85) as further described below.
[0023] Referring to Figure 2, shown is one embodiment of a locking mechanism 14 for inhibiting
the first reciprocal motion 12 of the main piston 105 and/or the second reciprocal
motion 13 of the secondary piston 115. In the present example, the locking mechanism
14 is the pair of flow valves (SV1, SV2, e.g. solenoid) for blocking the inflow of
hydraulic fluid to either or both of the first input 112 and the second input 113,
however in Figure 2 the locking mechanism 14 is unactivated. Both the pistons 105,
115 are shown in Figure 2 in a Bottom Dead Center (BDC) position in their respective
bores 110, 120, as the actuator 85 continues to provide for both reciprocations 12,
13 together / at the same time. In this manner, operation of the hydraulic device
20 between the TDC and BDC positions of Figures 1 and 2 provide for a full / constant
displacement of the hydraulic device 20 (i.e. the first and second output portions
of the hydraulic fluid are both ejected from the common output 135 of the respective
piston 105, 115 pair). It is recognized that each piston pair 105, 115 can be controlled
(for example on demand, by the operator, etc.) to switch between variable displacement
mode and full displacement mode using their respective flow control valve(s) SV1,
SV2 (e.g. an example locking mechanism 14) during operation of the hydraulic device
20.
[0024] In view of the above, one embodiment of the locking mechanism 14 is a hydraulic locking
mechanism, such that the hydraulic locking mechanism inhibits at least one of: the
first input 112 from receiving the hydraulic fluid on the first intake stroke; and
the first output 127 from ejecting (not shown) the hydraulic fluid on the first exhaust
stroke; and/or the second input 113 from receiving the hydraulic fluid on the second
intake stroke; and the second output 126 from ejecting (not shown) the hydraulic fluid
on the second exhaust stroke. For example, the hydraulic locking mechanism 14 includes
at least one of: a first flow valve SV1,SV2 positioned as shown by example on the
input(s)112,113 for inhibiting receipt of the hydraulic fluid on the first/second
intake stroke; a second valve (not shown) positioned on the output(s)126,127 (not
shown) for inhibiting ejection of the hydraulic fluid on the first/second exhaust
stroke.
[0025] Referring to Figure 9A,B,C,D,E,F, shown are alternative examples of the locking,
mechanism 14. For example, the locking mechanism 14 is a mechanical locking mechanism,
such that the mechanical locking mechanism 14 inhibits the first reciprocal motion
12. The mechanical locking mechanism 14 includes a mechanical element positioned adjacent
to a sidewall of the main piston 105, such that contact of the mechanical element
with the sidewall is used to inhibit the first reciprocal motion 12.
[0026] For example, Figures 9A,B,C,D,E,F show a mechanical lock 14 consisting of a pin P2
positioned adjacent to a ramp W2 located in a sidewall of the piston 105, as well
as a pin P1 positioned adjacent to a ramp W1 located in a sidewall of the piston 115,
in various operational modes. In the case of a piston 105, 115 which can turn in the
bore 110 during the reciprocation 12, the ramp W1, W2 can be formed about the periphery
of the sidewall of the piston 105,115. In Figure 9A, the piston 115 is locked (pin
P1 is engaged with ramp W1) at TDC while piston 105 is starting the exhaust stroke.
In Figure 9B, the mechanical lock 14 of pin P2 engages ramp W2 and piston 105 is locked
at TDC while piston 115 is unlocked (pin P1 is disengaged with ramp W1) and thus starting
the exhaust stroke. In Figure 9C, the piston 105 is locked at TDC and the piston 115
is starting the intake stroke. In Figure 9D, the piston 105 is locked at TDC and the
piston 115 is starting the exhaust stroke. In Figure 9E, the piston 115 is locked
at TDC and the piston 105 is starting the intake stroke. In Figure 9F, the piston
115 is locked at TDC and the piston 105 is starting the exhaust stroke.
[0027] In a further embodiment of the locking mechanism 14, the locking mechanism 14 can
be a magnetic locking mechanism 14, such that the magnetic locking mechanism 14 inhibits
the first reciprocal motion 12 and/ or the second reciprocal motion 13. For example,
the magnetic locking mechanism 14 can include a solenoid element positioned adjacent
to a sidewall of the main piston 105 and/or the secondary piston 115, such that operation
of the solenoid element(s) is used to inhibit the first reciprocal motion 12 and/or
the second reciprocal motion 13.
[0028] It is also recognized that the locking mechanism 14 can be a combination of the hydraulic
locking mechanism 14 (e.g. flow control valves SV1, SV2) and the mechanical locking
mechanism 14 (e.g. mechanical elements or solenoid elements). It is recognized that
when using the hydraulic locking mechanism 14, the locking operation can be provided
by hydraulic vacuum which is systematically created when injection into and/or ejection
from a selected cylinder-piston is truncated.
[0029] In view of the above, the locking mechanism 14 for each of the piston 105, 115 pairs
can be used to provide a variable displacement of the hydraulic device, such that
one or both of the pistons 105,115 is disconnected from the actuator 85 for one or
more selected pairs of the multi pair hydraulic device 20. As discussed above, to
disconnect a piston 105, 115, we can activate the respective locking mechanism 14
(e.g. using hydraulic lock we truncate the injection flow into the related bore 110,
120 by simply closing off the related solenoid flow control valve SV1, SV2). During
the locking operation and thus the resulting decoupling of the locked piston 105,
115 from the actuator 85, the actuator 85 drives all pistons 105, 115to TDC at which
point, the piston without a new injection (e.g. locked) will be held at TDC. Once
disconnected from the actuator 85, the piston(s) 105, 115 can be held at TDC by way
of mechanical and/ or vacuum lock (depending upon the desired locking mechanism(s)
14 employed by the hydraulic device 20). Any piston 105, 115 held at TDC will no longer
contribute to the outlet flow volume for the outlet 125.
[0030] For example, in Figure 4, a first flow valve SV1 (when activated - e.g. closed) can
block the inflow of hydraulic fluid through the first input 112 and into the main
cylinder 110. For example, a second flow valve SV2 (when activated - e.g. closed)
can block the inflow of hydraulic fluid through the second input 113 and into the
secondary cylinder 120. Therefore, when engaging the locking mechanism 14 by way of
closing the first flow valve SV1 inhibits the first portion of the outputting of the
hydraulic fluid by decoupling the main piston 105 from the actuator 85, due to a hydraulic
lock provided by a vacuum formed adjacent to the end 105a while continued operation
of the actuator 85 provides for the second portion of the outputting of the hydraulic
fluid via the continued reciprocation 13 of the secondary piston 115. This occurs
because the second flow valve SV2 is open and thus provides for the flow of hydraulic
fluid from the second input 113 to the second output 126. In this manner, the main
piston 105 becomes stopped (i.e. the reciprocal motion 12 is halted) and the secondary
piston 115 continues to reciprocate 13. As shown, when the reciprocal motion 12 is
halted the main piston 105 becomes decoupled from the actuator 85, i.e. the second
end 105b losses contact with the actuator 85. As shown, when the reciprocal motion
13 is continued, the secondary piston 115 remains coupled to the actuator 85, i.e.
the second end 115b remains in contact with the actuator 85. Both the pistons 105,
115 are shown in Figure 4, the main piston 105 locked and in a Top Dead Center (TDC)
position in the respective bore 110, and the secondary piston 115 unlocked at a Bottom
Dead Center (BDC) position in the respective bore 120. In this manner, operation of
the hydraulic device 20 between the TDC and BDC positions of Figures 1 and 4 provide
for a variable displacement mode of the hydraulic device 20 (i.e. only the second
output portion of the hydraulic fluid is ejected from the common output 125 while
the first output portion of the hydraulic fluid is withheld from the common output
125).
[0031] Referring to Figure 3, on the contrary, when engaging the locking mechanism 14 by
way of closing the second flow valve SV2inhibits the second portion of the outputting
of the hydraulic fluid by decoupling the secondary piston 115 from the actuator 85,
due to a hydraulic lock provided by a vacuum formed adjacent to the end 115a while
continued operation of the actuator 85 provides for the first portion of the outputting
of the hydraulic fluid via the continued reciprocation 12 of the main piston 105.
This occurs because the first flow valve SV1 is open and thus provides for the flow
of hydraulic fluid from the first input 112 to the first output 127. In this manner,
the secondary piston 115 becomes stopped (i.e. the reciprocal motion 13 is halted)
and the main piston 105 continues to reciprocate 12. As shown, when the reciprocal
motion 13 is halted the secondary piston 115 becomes decoupled from the actuator 85,
i.e. the second end 115b losses contact with the actuator 85. As shown, when the reciprocal
motion 12 is continued, the main piston 105 remains coupled to the actuator 85, i.e.
the second end 105b remains in contact with the actuator 85. Both the pistons 105,
115 are shown in Figure 3, the main piston 105 unlocked and in a Bottom Dead Center
(BDC) position in the respective bore 110, and the secondary piston 115 locked at
a Top Dead Center (TDC) position in the respective bore 120. In this manner, operation
of the hydraulic device 20 between the TDC and BDC positions of Figures 1 and 3 provide
for a variable displacement mode of the hydraulic device 20 (i.e. only the first output
portion of the hydraulic fluid is ejected from the common output 125 while the second
output portion of the hydraulic fluid is withheld from the common output 125).
[0032] In general, the actuator 85 includes an eccentric cam 100 driven off a main shaft
95, the eccentric cam 100 having a cam surface 86 for contacting the second main end
105b and the second secondary end 115b during the first reciprocal motion 12 and the
second reciprocal motion 13. Further, the cam surface 86 can decouple from the second
main end 105b while retaining contact with the second secondary end 115b when the
locking mechanism 14 is locking the main piston 105. Further, the cam surface 86 can
remain engaged with the second main end 105b while decoupling from the second secondary
end 115b when the locking mechanism 14 is locking the secondary piston 115.
[0033] Referring to Figures 11A,B, 12A,B,C, shown is a further embodiment of the coupling
/ decoupling between the actuator 85 and pistons 105, 115, 250 (in the case of a three
piston embodiment). Note that the cylinder bores are For example, the hydraulic device
20 can have one or more inner piston(s) 115, 250 inside the outer piston 105, such
that only the outer (e.g. full time) piston 105 is in contact with the actuator 85
while the inside (e.g. part time) piston(s) 115, 250 are actuated by an actuating
surface 106 (e.g. abutment surface) located on the outer piston 105. Referring to
Figure 11A, shown is the actuator 85 at BDC. Shown in Figure 11B is where all of the
pistons 105, 115, 250 are operating (e.g. are all unlocked) and thus the piston 105
is pushed upwards to TDC by the actuator 85 while the pistons 115, 250 are pushed
upwards to TDC by the actuating surface 106 of the piston 105.
[0034] Figure 12A shows one example operation of the hydraulic device 20 of Figures 11A,B,
whereby piston 105 is locked and thus decoupled from the actuating surface 106 (once
pushed to TDC by the actuating surface 106), while the piston 115 continues to be
actuated by the actuator 85 and the piston 250 continues to be actuated by the surface
106. Figure 12B shows one example operation of the hydraulic device 20 of Figures
11A,B, whereby pistons 105,250 are locked and thus decoupled from the actuating surface
106 (once pushed to TDC by the actuating surface 106), while the piston 115 continues
to be actuated by the actuator 85. Figure 12C shows one example operation of the hydraulic
device 20 of Figures 11A,B, whereby all pistons 105, 115, 250 are locked and thus
decoupled, i.e. pistons 105, 250 from the actuating surface 106 (once pushed to TDC
by the actuating surface 106) and piston 115 is decoupled from the actuator 85 (once
pushed to TDC by the actuator 85).
[0035] Referring to Figures 6A,6B,6C,6D, shown is the main piston 105 is locked at TDC and
thus is decoupled from the actuator 85 (i.e. the main piston 105 remains out of contact
with the surface 86 and the reciprocal motion 12 is halted),while the actuator 85
is driving the secondary piston 115 between the TDC position (see Figure 6D) and the
BDC position (see Figure 6A). Thus, the reciprocal motion 13 in Figures 6A, 6B, 6C,
6D is shown progressing from BDC to TDC under influence of the actuator 85 being coupled
to the secondary piston 115. Shown in Figure 6A to Figure 6D is an exhaust stroke
for the hydraulic fluid, using the secondary piston 115. It is recognized that an
intake stroke for the secondary piston 115 would be the reverse, from Figure 6D to
Figure 6A (i.e. from TDC to BDC).
[0036] Referring to Figures 7A, 7B, 7C, 7D, shown is the secondary piston 115 is locked
at TDC and thus is decoupled from the actuator 85 (i.e. the secondary piston 115 remains
out of contact with the surface 86 and the reciprocal motion 13 is halted), while
the actuator 85 is driving the main piston 105 between the TDC position (see Figure
7D) and the BDC position (see Figure 7A). Thus, the reciprocal motion 12 in Figures
7A, 7B, 7C, 7D is shown progressing from BDC to TDC under influence of the actuator
85 being coupled to the main piston 105. Shown in Figure 7A to Figure 7D is an exhaust
stroke for the hydraulic fluid, using the main piston 105. It is recognized that an
intake stroke for the main piston 105 would be the reverse, from Figure 7D to Figure
7A (i.e. from TDC to BDC).
[0037] Referring to Figures 8A, 8B, 8C, 8D, shown are both pistons 105,115 are locked at
TDC and thus are decoupled from the actuator 85 (i.e. both pistons 105,115 remain
out of contact with the surface 86 and the reciprocal motions 12, 13 are halted),
while the actuator 85 rotates between the TDC position (see Figure 8D) and the BDC
position (see Figure 8A).
[0038] As provided above by example in Figures 6A,6B,6C,6D, 7A,7B,7C,7D, 8A,8B,8C,8D, to
provide variable displacement for one or more of each piston pair 105,115, one (or
both) of the pistons 105, 115 is / are disconnected from the actuator 85. To disconnect
a piston 105,115, we truncate the injection flow into the related bore 110, 120 by
simply closing off the related solenoid (e.g. flow control valve SV1, SV2). Once the
flow control valve(s) SV1, SV2 is closed, the actuator 85 can always drive all pistons
105,115 to TDC, at which point, the piston 105, 115 without a new injection (having
a closed flow control valve SV1, SV2) will be held at TDC by way of mechanical or
vacuum lock. Once held, the piston(s) 105, 115 will become decoupled from the actuator
85 and the held piston(s) 105,115 at TDC will no longer contribute to the outlet flow
volume in their respective outputs 126, 127.
[0039] It is therefore recognized that all pistons 105, 115 placed in a locked mode (e.g.
by closing the respective flow control valve SV1, SV2) travel first to TDC under mechanical
power by the actuator 85 and will therefore, exhaust. Lock-down takes place when pistons
are held at TDC (e.g. such as by using a hydraulic vacuum lock mechanism 14, a mechanical
lock mechanism 14, etc.), we cannot stop a piston 105, 115 from moving to TDC but
we can inhibit piston 105, 115 travel to BDC using the locking mechanism(s) 14.
[0040] In turn, in one embodiment, re-engaging the disconnected piston(s) 105,115 to become
once again coupled to the actuator 85 can be facilitated by re-opening the related
flow control valve(S) SV1, SV2 to allow flow into the related bore 110, 120 via the
input 112a, 113a. As the hydraulic fluid flow fills the bore 110, 120 (e.g. as driven
by a charge pump), the piston(s) 105, 115 will be pushed closer to the actuator 85
in order to reengage with the actuator 85, no matter what position the actuator 85
may be during the reengagement. For example, the actuator 85 can be travelling in
the same or opposite direction as the piston(s) 105, 115 during reengagement of the
piston(s) 105,115. During reengagement, in one case both the piston(s) 105, 115 and
the actuator 85 could both be moving towards BDC (i.e. both travelling in the same
direction during the intake stroke). In this manner the piston(s) 105, 115 will recouple
with the actuator 85 on their downward travel towards BDC, so that the recoupled piston(s)
105,115 will travel with the actuator 85 once again towards TDC (e.g. during the exhaust
stroke). Once recoupled, the piston(s) 105,115 continue their reciprocal motion 12,13
until such time as their flow control valve(s) SV1, SV2 become closed once again.
[0041] During reengagement, in another case both the piston(s) 105, 115 and the actuator
85 could both be moving in opposite directions (i.e. the actuator 85 towards TDC and
the piston(s) 105, 115 towards BDC during a designated exhaust stroke). In this manner
the piston(s) 105, 115 will recouple with the actuator 85 on their downward travel
towards BDC, as the actuator 85 comes up to meet the downward travelling piston(s)
105,115, so that the recoupled piston(s) 105,115 will travel with the actuator 85
once again towards TDC (e.g. during the exhaust stroke, in this case a partial exhaust
stroke measured from the point of reengagement somewhere between BDC and TDC). Once
recoupled, the piston(s) 105,115 would continue their reciprocal motion 12,13 until
such time as their flow control valve(s) SV1, SV2 become closed once again. Therefore,
it is recognized in this embodiment of reengagement, the exhaust stroke of the reengaged
piston(s) 105, 115 would only be a partial exhaust stroke (i.e. only a partial bore
volume of oil would be ejected from the outlet 126, 127 - in essence the amount of
oil in the bore 110, 120 at the point where the upwards travelling actuator 85 reengages
with the piston(s) 105, 115 somewhere between BDC and TDC).
[0042] It is recognized that in the case where both the piston(s) 105, 115 and the actuator
85 are moving in opposite directions, the re-engagement of the piston(s) 105, 115
to the actuator 85 is advantageously not disruptive (i.e. undesirable impact / collision
between the actuator 85 and the piston(s) 105, 115) due to one or more of the following;
a) layers of oil between the actuator surface 86 and the piston surface(S) 105b, 115b
can act as buffer or shock absorber; b) as the piston(s) 105, 115 changes direction
back towards TDC, following engagement with the upwards travelling actuator 85, the
piston(s) 105, 115 will not encounter a "dead-head" condition as a small volume of
oil can be released past the inlet check valve 112 while the inlet check valve is
closing (e.g. latency in the closing of the check valve 112 allows for oil to be pushed
back out the inlet check valve 112 at the time of reengagement of the downwards travelling
piston(s) 105,115 with the upwards travelling actuator 85). In this manner, reengagement
of the piston(s) 105, 115 advantageously may not need controlled / monitored timing
of the position of the actuator 85 when the flow control valve(s) SV1, SV2 is opened,
e.g. disengage or re-engage timing means may not be required.
[0043] It is also recognized that in a timed operational mode, the position of the actuator
85 could be monitored (e.g. by a position sensor, by a controller based on position
of the drive shaft 95, etc.) so that the flow control valve(s) SV1, SV2 would only
be reopened when the actuator 85 is at the TDC position.
[0044] Referring again to Figure 1, shown is one embodiment of the actuator 85 and the inlet
135 and the outlet 125, such that there is a common inlet oil gallery 130 and a common
outlet oil gallery (e.g. 125). In this manner, a plurality of the piston pair 105,
115 and associated cylinder pair 110,120 can be connected to one another for a multi-pair
hydraulic device 20. Further, each of the inlets 112, 113 have a respective entrance
112a, 113a, in order to isolate (e.g. starve) each inlet 112,113 of the multi-pair
hydraulic device 20 when the respective flow control valve(s) SV1, SV2 is / are closed.
[0045] In this manner, it is recognized that each of the piston pairs 105, 115 would have
a respective lock mechanism 14 (e.g. a respective set of flow control valves SV1,SV2).
In this manner, each piston 105, 115 of each piston pair 105,115 can be controlled
in either a locked or unlocked manner. Also, it is preferred to have valves (e.g.
check valves CV) at each entrance and exit of the cylinder bores 110,120, in order
to facilitate proper flow (e.g. prevent cross talk between adjacent pairs of the pistons
105, 115) of the hydraulic fluid between the inlet 135 and the outlet 125 during operation
of the hydraulic device 20. Thus, shown is a head end-cap 140, as well as the inlet
and outlet check valves CV. In this manner, a first check valve CV can be positioned
in the first input 112, a second check valve CV positioned in the first output 127,
a third check valve CV positioned in the second input 113 and a fourth check valve
CV positioned in the second output 126.
[0046] Referring again to Figure 1, the actuator 85 can be an eccentric actuator mounted
on a main shaft 95, such that an offset cam 100 (mounted on the shaft 95) drives the
actuator 85 (with surface 86) as the main shaft 95 rotates (e.g. is driven by a primary
mover such as an electric motor - not shown). Further, a set of bearings 90 (e.g.
roller bearings) can be positioned between the actuator block 85 and the offset cam
100. In this manner, as the shaft 95 rotates, the offset cam 100 moves the actuator
block 85 between the TDC and the BDC positions. Further, as noted above by example,
the piston(s) 105, 115 are shown locked in their TDC position. It is recognized that
unlocking of the flow control valve(s) SV1, SV2 could be timed off the main shaft
95 (or remain untimed as discussed above as one embodiment) so that the unlocking
of a locked piston would coincide with the proper positioning of the actuator block
85 (i.e. the surface 86 would be in position adjacent to the end 105b, 115b at TDC)
when the respective flow control valve SV1,SV2 is unlocked. Alternatively, in the
untimed mode, there is no need to time the position of the actuator 85 on reengaging
with the piston(s) 105, 115 after lockdown, which would result in the partial exhaust
stroke on reengagement of the piston(s) with the actuator 85.
[0047] Referring to Figures 10A,B, shown is a further embodiment of the hydraulic device
20, such that the housing 25 has a pair of inlets 112, 113 and a pair of outlets 126,127,
such that each piston 105, 115 has a respective individual inlet 112, 113 and a respective
individual outlet 127, 126. In this manner, the output flows (e.g. first portion and
second portion) are separate from one another and thus can remain separate or otherwise
combined exterior to the housing 25. In Figure 10A, both pistons 105, 115 are at BDC
and are starting an exhaust stroke. In Figure 10B, both pistons 105, 115 are at TDC
and are thus at the end of their exhaust strokes, resulting in a first portion of
the hydraulic fluid output exiting the first outlet 127 and a second portion of the
hydraulic fluid output exiting the separate (from the first outlet 127) second outlet
126.
[0048] In general it is recognized that the actuator 85 can include an eccentric cam 100
driven off the shaft 95, the eccentric cam 100 having a first cam surface 100a for
contacting the second main end 105a and a second cam surface 100b for contacting the
second secondary end 115b during the first reciprocal motion 12 and the second reciprocal
motion 13, such that the first cam surface 100a is offset from the second cam surface
100b. Referring to Figures 13A,B, shown is a further embodiment of the actuator 85,
having an offset cam having a first cam 100a offset (e.g. by 180 degrees) from a second
cam 100b, such that both the first cam 100a and the second cam 100b are mounted on
the same shaft 95. In this manner, as the cams 100a, 100b rotate, the pistons 105,115
alternate separately between their TDC and BDC positions. For example, when offset
by 180 degrees, the main piston 105 would be at BDC when the secondary piston 115
is at TDC, see Figure 13A. Once the cams 110a, 100b are further rotated by the shaft
95, then the positions of the pistons 105, 115 would eventually switch, i.e. the main
piston 105 would be at TDC when the secondary piston 115 is at BDC, see Figure 13B.
As shown in Figure 13A,B, the locking mechanism 14 (see Figure 2) is unactivated (both
flow valves SV1 and SV2 are open) and thus both pistons 105, 115 are reciprocating
12,13 as the drive shaft 95 rotates.
[0049] Referring to Figures 14A,B, shown is the further embodiment of the actuator 85, having
the offset cam having the first cam 100a offset (e.g. by 180 degrees) from the second
cam 100b, such that both the first cam 100a and the second cam 100b are mounted on
the same shaft 95. In this manner, the pistons 105,115 can be alternated between their
TDC and BDC positions. As shown in Figure 14A,B, the locking mechanism 14 (see Figure
3) is activated (flow valve SV1 is open and flow valve SV2 is closed) and thus the
main piston 105 is reciprocating 12 as the drive shaft 95 rotates while the secondary
piston 115 remains locked (i.e. held in position at TDC). For example, when offset
by 180 degrees, the main piston 105 is at BDC when the secondary piston 115 is held
at TDC, see Figure 14A. Once the cams 110a, 100b are further rotated by the shaft
95, then the position of the main piston 105would change, i.e. the main piston 105
would be at TDC while the secondary piston 115 remains stationary at TDC (and is decoupled
from the cam 110b), see Figure 14B.
[0050] Referring to Figures 15A,B, shown is the further embodiment of the actuator 85, having
the offset cam having the first cam 100a offset (e.g. by 180 degrees) from the second
cam 100b, such that both the first cam 100a and the second cam 100b are mounted on
the same shaft 95. In this manner, the pistons 105,115 can be alternated between their
TDC and BDC positions. As shown in Figure 15A,B, the locking mechanism 14 (see Figure
4) is activated (flow valve SV1 is closed and flow valve SV2 is open) and thus the
secondary piston 115 is reciprocating 13 as the drive shaft 95 rotates while the main
piston 105 remains locked (i.e. held in position at TDC). For example, when offset
by 180 degrees, the secondary piston 115 is at TDC when the main piston 105 is held
at TDC, see Figure 15A. Once the cams 110a, 100b are further rotated by the shaft
95, then the position of the secondary piston 115would change, i.e. the secondary
piston 115 would be at BDC while the main piston 115 remains stationary at TDC (and
is decoupled from the cam 110a), see Figure 15B.
[0051] In view of the above, it is recognized that the hydraulic device 20 can be a pump
as shown or can also be a motor. In a motor mode of the hydraulic device 20, the reciprocation(s)
12,13 of the piston(s) 105, 115 would drive the rotation of the shaft 95 by the respective
end(s) 105b, 115b driving the contact surface(s) 86. In this manner, the input of
the hydraulic fluid into the input(s) 112, 113 would be used to drive the reciprocation(s)
12, 13 and thus the rotation of the shaft 95. It is therefore recognized in the motor
mode that variable displacement (e.g. using the locking mechanism 14 as described
above) could be used by the hydraulic device 20 to moderate the torque and / or speed
of the motor operation, as desired.
[0052] Further, it is recognized in the above that the pistons 110, 115 have a fixed stroke
length when reciprocating in their respective bores (i.e. cylinders 110,120). As such,
a distance between a Top Dead Center TDC and Bottom Dead Center BDC remains constant
when the locking mechanism 14 (e.g. flow control valves SV1,SV2)is operated between
a closed / locked state and an open / unlocked state. The position TDC can be defined
as when the piston 110, 115 reaches the end of the exhaust stroke for ejecting fluid
out of the cylinder 110, 120, and thus the beginning of the intake stroke for injecting
fluid into the cylinder 110, 120. The position BDC can be defined as when the piston
110, 115 reaches the end of the intake stroke for injecting fluid into the cylinder
110, 120, and thus the beginning of the exhaust stroke for ejecting fluid out of the
cylinder 110, 120. The configuration of the piston 105 - cylinder 110 and piston 115
- cylinder 120 arrangements can be referred to as an axial configuration.
[0053] Referring to Figures 16,17, shown are embodiments of the hydraulic device 20 having
a plurality of piston 105 - cylinder 110 and piston 115 - cylinder 120 arrangements.
For example, it is envisioned that the hydraulic device 20 can have any number of
piston- cylinder arrangements, e.g. 5, 7, 9, etc.
[0054] Further, it is also recognized that each internal piston 115 (or a multi piston device
20) can be of different surface area than the next one, which could provide for allows
for the outlet flow reduction (i.e. variable displacement) to be nonlinear.
[0055] Referring to Figure 16, shown is the housing 25 of the hydraulic device 20 having
conceptually a plurality of pairs of pistons, such that each pair of pistons includes
the outer piston 105 and the inner piston 115. It is recognized that one or more of
the pairs of pistons 105, 115 can have different diameters (with corresponding bores),
the differing numerical sizes of the pistons 105, 115 shown by example only. In this
manner, depending upon which piston(s) 105, 115 is/are decoupled from the actuator
85 (not shown in Figure 16 for simplicity, rather see Figure 1 for an example of the
actuator 85), the hydraulic device 20 could have a selected difference in the variable
displacement provided. For example, it is recognized that decoupling the 17mm inner
piston 115 would subtract less from the total output of the hydraulic device 20 (in
the case of a pump) than in the case of decoupling the 21mm piston 115. In this manner,
not only the decision to decouple a piston 115 (or corresponding piston 105 for that
matter) can be made by the operator of the hydraulic device 20, but also the size
of the piston 105, 115.
[0056] Referring to Figure 17, shown is an alternative embodiment of the hydraulic device
20 having multiple trio-sets of pistons, namely piston 105 is the outer most piston,
piston 115 is the intermediate piston and the piston 115B is the inner most piston.
Shown in Figure 17 is a plurality of different sizes of the pistons 105, 115, 115B,
however it is also recognized that similar sized pistons 105, 115, 115B can be provided,
as desired (e.g. similar to the embodiment of Figure 1 for pairs 105, 115 of pistons).
As such, each piston 115 and piston 115B can be of a different bore diameter to each
other. In other words, a piston 115B of diameter 21mm will, per revolution, displace
a lesser volume than piston 115B of 23mm and so forth. Similarly piston 115 of 23mm
will, per revolution, displace a lesser volume than piston 115 of 25mm and so forth.
[0057] Referring to Figure 18, shown is an alternative embodiment of the hydraulic device
20 (e.g. configured as a hydraulic pump). The hydraulic device 20 has multiple sets
of piston in pistons 105A,B,C,D, for example three sets shown in the housing 25. For
example, each set of pistons (e.g. nested pistons) has an outer piston 105A, a first
piston 105B positioned inside the outer piston 105A, a second piston 105C positioned
inside the first piston 105B and a third piston 105D positioned within the second
piston 105C. Each of the pistons is positioned within a corresponding bore 107A, 107B,
107C, 107D, such that at least a portion of bore 107B is within the outer piston 105A,
at least a portion of bore 107C is within the first piston 105B, and at least a portion
of bore 107D is within the second piston 105C. The bore 107A is within the housing
25. it is recognized that the bores 107A,B,C,D are not in fluid communication with
one another, rather any fluid communication between the bores 107A,B,C,D of the same
piston set 105A,B,C,D is inhibited by the bodies of the intervening pistons 105A,B,C,D.
[0058] Each of the pistons 105A, 105B, 105C, 105D are configured to reciprocate axially
along the reciprocation axis 11, see Figure 1, in conjunction with the actuator ACT1,
ACT2, ACT3. It is recognized that each set of piston in pistons 105A,B,C,D has a corresponding
shared actuator ACT1,2,3 (e.g. each actuator ACT1,ACT2,ACT3 drives / is driven with
respect to the set of pistons 105A,B,C,D). Not shown is Figure 18 for the purpose
of ease of portrayal only, is the shaft 95 and cam 100 (see Figure 1) as part of the
actuators ACT1, ACT2, ACT3. For example, each actuator ACT1,2,3 is driven off the
same shaft 95 by a respective cam 100 (not shown). SLE refers to the set of piston
bores 107A, B, C, D.
[0059] Referring again to Figure 18, the bores 107A,B,C,D are not in fluid communication
with one another, rather any fluid communication between the bores 107A,B,C,D of the
same piston set 105A,B,C,D is inhibited by the bodies of the intervening pistons 105A,B,C,D.
For example, the body of first piston 105B is positioned during its reciprocation
such that the body of the first piston 105B inhibits fluid communication between the
bore 107A and the bore 107B (recognizing that piston seals - not shown - between the
pistons 105A,B,C,D and the walls of the respective bores 107A,B,C,D can also thus
facilitate the inhibition of fluid communication between the bores 107A,B,C,D). Further,
the body of second piston 105C is positioned during its reciprocation such that the
body of the second piston 105C inhibits fluid communication between the bore 107B
and the bore 107C. Further, the body of third piston 105D is positioned during its
reciprocation such that the body of the third piston 105D inhibits fluid communication
between the bore 107C and the bore 107D.
[0060] Referring again to Figure 18, it is recognized that there is a set of shared control
valves (e.g. solenoids) SOL1, SOL2, SOL3, SOL4, which is different from the individual
(e.g. unshared) control valves SV1, SV2 embodiment of Figure 1. In Figure 18, for
example, the reciprocation of a selected piston from each set of pistons 105A,B,C,D
is controlled by a shared control valve SOL1, SOL2, SOL3, SOL4. For example, control
valve SOL1 controls the reciprocation state (locked or unlocked) of all outer pistons
105A, such that operation of the flow control valve SOL1 either locks all outer pistons
105A from all the sets of pistons 105A,B,C,D or unlocks all outer pistons 105A from
all the sets of pistons 105A,B,C,D. For example, control valve SOL2 controls the reciprocation
state (locked or unlocked) of all first pistons 105B, such that operation of the flow
control valve SOL2 either locks all first pistons 105B from all the sets of pistons
105A,B,C,D or unlocks all first pistons 105B from all the sets of pistons 105A,B,C,D.
For example, control valve SOL3 controls the reciprocation state (locked or unlocked)
of all second pistons 105C, such that operation of the flow control valve SOL3 either
locks all second pistons 105C from all the sets of pistons 105A,B,C,D or unlocks all
second pistons 105C from all the sets of pistons 105A,B,C,D. For example, control
valve SOL34 controls the reciprocation state (locked or unlocked) of all third pistons
105D, such that operation of the flow control valve SOL4 either locks all third pistons
105D from all the sets of pistons 105A,B,C,D or unlocks all third pistons 105D from
all the sets of pistons 105A,B,C,D.
[0061] In the manner described above, it is recognized that each flow control valve SOL1,SOL2,SOL3,SOL4
controls two or more pistons 105A,105B,105C,105D, such that the two or more pistons
105A, 105B, 105C, 105D controlled are from different sets of pistons 105A,B,C,D. This
configuration is different form the hydraulic device 20 shown in Figure 1, whereby
each flow control valves SV1,SV2 only controls one respective piston 105, 115. In
this manner, the flow control valves SOL1,SOL2,SOL3,SOL4 are configured in a one to
many setup (e.g. one flow control valve for many pistons) while the flow control valves
SV1,SV2 are configured in a one to one setup (e.g. one flow control valve for one
piston).
[0062] Referring again to Figure 18, the passage IN is a common gallery for the housing
25 whereby hydraulic fluid is either facilitated to enter the bore 107A,B,C,D by the
respective flow control valves SOL1,SOL2,SOL3,SOL4 (e.g. in an open / unlocked state)
or is either restricted from entering the bore 107A,B,C,D by the respective flow control
valves SOL1,SOL2,SOL3,SOL4 (e.g. in a closed / locked state). In other words, the
passage IN can be referred to as an inlet or feed port for the hydraulic device 20.
Further, P1 represents the outlet port for each of the flow control valves SOL1,SOL2,SOL3,SOL4
while P2 represents the inlet port for each of the flow control valves SOL1,SOL2,SOL3,SOL4
(e.g. when a flow control valve SOL1,SOL2,SOL3,SOL4 is closed / locked, hydraulic
oil is inhibited from flowing through its inlet port P2 and out of its outlet port
P1).
[0063] Referring again to Figure 18, POR1, POR2, POR3, POR4 are the respective inlet passages
connecting the respective outlet port P1 of each of the flow control valves SOL1,SOL2,SOL3,SOL4
with a respective common gallery CG1,CG2,CG3,CG4. For example, passage POR1 is used
to direct hydraulic oil from the outlet port P1 of flow control valve SOL1 to each
of the bores 107A of the outer pistons 105A. For example, passage POR2 is used to
direct hydraulic oil from the outlet port P1 of flow control valve SOL2 to each of
the bores 107B of the outer pistons 105B. For example, passage POR3 is used to direct
hydraulic oil from the outlet port P1 of flow control valve SOL3 to each of the bores
107C of the outer pistons 105C. For example, passage POR4 is used to direct hydraulic
oil from the outlet port P1 of flow control valve SOL4 to each of the bores 107D of
the outer pistons 105D.
[0064] Further to the above, respective passages POR5,6,7,8 are used to direct hydraulic
fluid from the respective common galleries CG1,2,3,4. For example, hydraulic fluid
entering from passage POR1 into common gallery CG1 then exits into passage POR5. For
example, hydraulic fluid entering from passage POR2 into common gallery CG2 then exits
into passage POR6. For example, hydraulic fluid entering from passage POR3 into common
gallery CG3 then exits into passage POR7. For example, hydraulic fluid entering from
passage POR4 into common gallery CG4 then exits into passage POR8.
[0065] Further, the respective passages POR5,6,7,8 fluidly connect each respective common
gallery CG1,2,3,4 with a respective passage connecting point CPO1,2,3,4. It is recognized
that the passage connecting point CPO1,2,3,4 provides for fluid communication between
adjacent passages POR9,10,11,12 (e.g. passage connecting points CPO1 fluidly connect
passage POR5 with passages POR9, passage connecting points CPO2 fluidly connect passage
POR6 with passages POR10, passage connecting points CPO3 fluidly connect passage POR7
with passages POR11, passage connecting points CPO4 fluidly connect passage POR8 with
passages POR12).
[0066] Further, the common gallery CG1 can be used to connect the respective passage POR1
with a respective passage POR9, thus functioning as a fluid connecting point. Further,
the common gallery CG2 can be used to connect the respective passage POR2 with a respective
passage POR10, thus functioning as a fluid connecting point. Further, the common gallery
CG3 can be used to connect the respective passage POR3 with a respective passage POR11,
thus functioning as a fluid connecting point. Further, the common gallery CG4 can
be used to connect the respective passage POR4 with a respective passage POR12, thus
functioning as a fluid connecting point.
[0067] Referring again to Figure 18, each of the symbols referenced by the reference indicator
NCPO refers to a non-connecting point, such that the crossed passages are not in fluid
communication with one another within the housing 25. For example, the symbol NCPO
shown indicates that the passage POR7 is not in fluid communication with the passage
POR12, the passage POR6 is not in fluid communication with the passages POR11, 12,
etc.
[0068] In view of the above, the respective common galleries CG1,2,3,4 direct hydraulic
fluid to each of their respective connecting points CG1,2,3,4. For example, common
gallery CG1 fluidly communicates with all the connecting points CPO1, common gallery
CG2 fluidly communicates with all the connecting points CPO2, common gallery CG3 fluidly
communicates with all the connecting points CPO3, and common gallery CG4 fluidly communicates
with all the connecting points CPO4. Also, via the respective connecting points CPO1,2,3,4,
each of the respective common galleries CG1,2,3,4 fluidly communicates with the respective
passages POR9,10,11,12.
[0069] Further, each OUT is an outlet passage from the various sets of pistons 105A,B,C,D.
It is recognized that in operation of the hydraulic device 20 of Figure 18, each of
the flow control valves SOL1,SOL2,SOL3,SOL4 can be normally opened (e.g. deenergized)
so supply hydraulic fluid can fill all bores 107A,B,C,D (in the case of a hydraulic
pump). If one (or more) of the flow control valves SOL1,SOL2,SOL3,SOL4 is closed (e.g.
energized), hydraulic fluid flow to all related bores is truncated. For example, if
the flow control valve SOL1 is closed then hydraulic fluid cannot flow to all the
bores 107A for all the outer pistons 105A. For example, if the flow control valve
SOL2 is closed then hydraulic fluid cannot flow to all the bores 107B for all the
first pistons 105B. For example, if the flow control valve SOL3 is closed then hydraulic
fluid cannot flow to all the bores 107C for all the second pistons 105C. For example,
if the flow control valve SOL4 is closed then hydraulic fluid cannot flow to all the
bores 107D for all the third pistons 105D. It is recognized that one or more of the
flow control valves SOL1,SOL2,SOL3,SOL4 can be closed at the same time. It is recognized
that one or more of the flow control valves SOL1,SOL2,SOL3,SOL4 can be open at the
same time.
[0070] Further, when referring to Figure 18 for the hydraulic device 20 as a hydraulic motor,
each of the inlets (e.g. IN, P2) would function as an outlet and each of the outlets
(e.g. OUT, P1) could function as an inlet. Further, it is recognized that the rotation
of the driveshaft 95 can be reversible, i.e. done is a clockwise or in counterclockwise
rotation as desired.
[0071] Further, it is recognized that a further embodiment, not shown, is where the configuration
of flow control valves SV1,SV2 of Figure 1 and the configuration of the flow control
valves SOL1,SOL2,SOL3,SOL4 is mixed. For example, in Figures 1, 16, each of the outer
pistons 105 could be controlled by a respective flow control valve SV1 (e.g. a one
control valve SV1 to one piston 105 configuration for each set of pistons). Additionally,
in Figures 1, 16, all of the inner pistons 115 could be controlled by a shared flow
control valve SOL2 (e.g. a one control valve SOL2 to many pistons 115 configuration
for each set of pistons).
[0072] Further, it is recognized that the flow control valves SOL1,SOL2,SOL3,SOL4 can be
referred to as one example of a locking mechanism (e.g. a hydraulic locking mechanism).
As such it is recognized that any / all of the flow control valves SOL1,SOL2,SOL3,SOL4
could be substituted for a mechanical locking mechanism type, such as shown by example
in Figures 9A-F).
Although the present invention is defined in the claims, it should be understood that
the present invention can also (alternativley) be defined in accordance with the following
embodiments:
1. A variable displacement hydraulic device comprising:
a housing having an inlet for receiving hydraulic fluid and an outlet for outputting
the hydraulic fluid, the housing having a reciprocation axis;
a first cylinder positioned in the housing along the reciprocation axis, the first
cylinder having a first input for receiving the hydraulic fluid on a first intake
stroke and a first output for ejecting the hydraulic fluid on a first exhaust stroke;
a first piston positioned for a first reciprocal motion within the first cylinder,
the first piston having a first main end exposed to the hydraulic fluid and a second
main end coupled to an actuator, the actuator for driving the second main end when
coupled to the actuator for causing the first reciprocal motion to induce a first
portion of said outputting of the hydraulic fluid;
a second cylinder positioned in the first piston along the reciprocation axis, the
second cylinder having a second input for receiving the hydraulic fluid on a second
intake stroke and a second output for ejecting the hydraulic fluid on a second exhaust
stroke;
a second piston positioned for a second reciprocal motion within the second cylinder,
the second piston having a first secondary end exposed to the hydraulic fluid and
a second secondary end coupled to the actuator, the actuator for driving the second
secondary end when coupled to the actuator for causing the second reciprocal motion
to induce a second portion of said outputting of the hydraulic fluid; and
a locking mechanism for inhibiting the first reciprocal motion of the first piston;
wherein when engaged the locking mechanism inhibits the first portion of said outputting
of the hydraulic fluid by decoupling the first piston from the actuator while continued
operation of the actuator provides the second portion of said outputting of the hydraulic
fluid by the second piston.
2. The hydraulic device of embodiment 1, wherein the second piston is concentrically
positioned within the first piston on the reciprocation axis.
3. The hydraulic device of embodiment 1, wherein the first output and the second output
are fluidly coupled at the outlet.
4. The hydraulic device of embodiment 1, wherein the first input and the second input
are fluidly coupled at the inlet.
5. The hydraulic device of embodiment 1, wherein the actuator includes an eccentric
cam driven off a shaft, the eccentric cam having a cam surface for contacting the
second main end and the second secondary end during the first reciprocal motion and
the second reciprocal motion.
6. The hydraulic device of embodiment 5, wherein the cam surface decouples from the
second main end while retaining contact with the second secondary end when the locking
mechanism is engaged with the first piston.
7. The hydraulic device of embodiment 1, wherein the actuator includes an eccentric
cam driven off a shaft, the eccentric cam having a first cam surface for contacting
the second main end and a second cam surface for contacting the second secondary end
during the first reciprocal motion and the second reciprocal motion, such that the
first cam surface is offset from the second cam surface.
8. The hydraulic device of embodiment 7, wherein the first cam surface decouples from
the
second main end while the second cam surface retains contact with the second secondary
end when the locking mechanism is engaged with the first piston.
9. The hydraulic device of embodiment 1, wherein the locking mechanism is a hydraulic
locking mechanism, such that the hydraulic locking mechanism inhibits at least one
of: the first input from receiving the hydraulic fluid on the first intake stroke;
and the first output from ejecting the hydraulic fluid on the first exhaust stroke.
10. The hydraulic device of embodiment 1, wherein the hydraulic locking mechanism
includes at least one of: a first valve positioned on the first input for inhibiting
receipt of the hydraulic fluid on the first intake stroke; a second valve positioned
on the first output for inhibiting ejection of the hydraulic fluid on the first exhaust
stroke.
11. The hydraulic device of embodiment 1, wherein the locking mechanism is a mechanical
locking mechanism, such that the mechanical locking mechanism inhibits the first reciprocal
motion.
12. The hydraulic device of embodiment 11, wherein the mechanical locking mechanism
includes a mechanical element positioned adjacent to a sidewall of the first piston,
such that contact of the mechanical element with the sidewall is used to inhibit the
first reciprocal motion.
13. The hydraulic device of embodiment 1, wherein the locking mechanism is a magnetic
locking mechanism, such that the magnetic locking mechanism inhibits the first reciprocal
motion.
14. The hydraulic device of embodiment 13, wherein the magnetic locking mechanism
includes a solenoid element positioned adjacent to a sidewall of the first piston,
such that operation of the solenoid element is used to inhibit the first reciprocal
motion.
15. The hydraulic device of embodiment 1, wherein the first main end and the second
main end are offset from one another when the first main end is at a first Top Dead
Center of the first reciprocal motion and the first secondary end is at a second Top
Dead Center of the second reciprocal motion.
16. The hydraulic device of embodiment 1, wherein the first main end and the second
main end are offset from one another by 180 degrees.
17. The hydraulic device of embodiment 1, wherein the first output is fluidly coupled
to the outlet and the second output is fluidly coupled to a second outlet of the housing,
such that the first portion is ejected from the outlet and the second portion is ejected
separately from the second outlet, the first output fluidly coupled to the outlet
and the second output fluidly coupled to the second outlet.
18. The hydraulic device of embodiment 1 further comprising a first check valve positioned
in the first input, a second check valve positioned in the first output, a third check
valve positioned in the second input and a fourth check valve positioned in the second
output.
19. The hydraulic device of embodiment 1 further comprising a second locking mechanism
for inhibiting the second reciprocal motion of the second piston.
20. The hydraulic device of embodiment 1, wherein reengagement of the first piston
with the actuator occurs when the actuator is travelling towards TDC and the first
piston is travelling towards BDC after the locking mechanism is disengaged.
21. The hydraulic device of embodiment 19, wherein reengagement of the second piston
with the actuator occurs when the actuator is travelling towards TDC and the second
piston is travelling towards BDC after the second locking mechanism is disengaged.
23. The hydraulic device of embodiment 1, wherein the hydraulic device is a pump.
24. The hydraulic device of embodiment 1, wherein the hydraulic device is a motor.
25. The hydraulic device of embodiment 1, wherein rotation of a driveshaft coupled
to the actuator is in a clockwise direction or a counter clockwise direction.
26. The hydraulic device of embodiment 1, wherein first reciprocal motion of the first
piston is controlled by the locking mechanism as a first locking mechanism and the
second reciprocal motion of the second piston is controlled by a second locking mechanism.
27. The hydraulic device of embodiment 1, wherein the first piston and the second
piston are a first piston pair of the housing and a third piston and a fourth piston
are a second piston pair of the housing, such that the fourth piston is positioned
in the third piston.
28. The hydraulic device of embodiment 27, wherein first reciprocal motion of the
first piston is controlled by the locking mechanism as a first locking mechanism,
the second reciprocal motion of the second piston is controlled by a second locking
mechanism, a third reciprocal motion of the third piston is controlled by a third
locking mechanism, and a fourth reciprocal motion of the fourth piston is controlled
by a fourth locking mechanism.
29. The hydraulic device of embodiment 27, wherein first reciprocal motion of the
first piston is controlled by the locking mechanism as a first locking mechanism,
the second reciprocal motion of the second piston is controlled by a second locking
mechanism, a third reciprocal motion of the third piston is controlled by the first
locking mechanism, and a fourth reciprocal motion of the fourth piston is controlled
by the second locking mechanism.
30. The hydraulic device of embodiment 27, wherein first reciprocal motion of the
first piston is controlled by the locking mechanism as a first locking mechanism,
the second reciprocal motion of the second piston is controlled by a second locking
mechanism, a third reciprocal motion of the third piston is controlled by a third
locking mechanism, and a fourth reciprocal motion of the fourth piston is controlled
by the second locking mechanism.