[TECHNICAL FIELD]
[0001] The present teaching relates to a straddled vehicle.
[BACKGROUND ART]
[0002] For example, Patent Document 1 shows a control device for controlling a starter generator
of an engine that is mounted to a motorcycle. In the motorcycle of Patent Document
1, the starter generator is used as an electric motor. Upon a request for starting
the engine, the control device directs the starter generator to rotate a crankshaft
of the engine.
[0003] The control device of Patent Document 1 performs what is called "swing-back", for
the purpose of ensuring a rotation speed of the crankshaft before reaching a compression
stroke. The swing-back means a process in which the crankshaft is once driven in reverse
rotation and then driven in forward rotation. Performing the swing-back enables the
rotation speed to rise in the compression stroke.
[0004] Generally in a rotary electric machine such as a starter generator, once the rotation
speed rises to a certain extent, a generatable torque starts to decrease, and then
the generatable torque decreases as the rotation speed rises. In the starter generator
of Patent Document 1, the rotation speed at which the generatable torque of the starter
generator starts to decrease is set low, in consideration of suppressing a size increase
of the starter generator.
[0005] The control device of the Patent Document 1 is configured to, when directing the
starter generator to rotate the crankshaft, raise a voltage to be supplied to the
starter generator for the purpose of accelerating the crankshaft before reaching the
compression top dead center. For example, the control device of Patent Document 1
raises the voltage by using a step-up chopper circuit that is formed by connecting
a positive electrode of a battery to the neutral point where windings of the starter
generator are coupled, the step-up chopper circuit including the windings. By raising
the voltage, the control device of Patent Document 1 can widen a speed range where
the starter generator is able to output a torque.
[0006] The control device of Patent Document 1 directs the starter generator to rotate the
crankshaft with the raised voltage. Then, the control device starts a combustion control
while terminating the rotation implemented by the starter generator, and directs the
starter generator to generate power.
[0007] Patent Documents 2 and 3 shows other engine with compression release mechanism.
[PRIOR ART DOCUMENTS]
[PATENT DOCUMENTS]
[SUMMARY OF THE INVENTION]
[PROBLEMS TO BE SOLVED BY THE INVENTION]
[0009] The control device of Patent Document 1 aims to shorten a time period until start
of the combustion control after an engine start instruction, by widening a range of
rotation speed of the starter generator until start of the combustion control.
[0010] In a straddled vehicle, it is demanded that a time period be shortened over the entire
time period until completion of engine start after an engine start instruction.
[0011] An object of the present teaching is to provide a straddled vehicle that is able
to shorten a time period until completion of engine start after an engine start instruction.
[MEANS FOR SOLVING THE PROBLEMS]
[0012] The present inventors conducted studies on a process from an engine start instruction
to completion of the start at a time of engine start. The present inventors focused
on an operation of a compression release mechanism (decompression mechanism). Patent
Document 1 also mentions a compression release mechanism.
[0013] For example, the compression release mechanism opens an exhaust valve in a compression
stroke where a piston compresses air (mixed gas) contained in a cylinder. This is
how the compression release mechanism lowers a load torque. Adoption of the compression
release mechanism allows the piston to compress air with a weaker force.
[0014] It can therefore be contemplated that adoption of the compression release mechanism
helps removal of problems that are involved in lowness of the torque applied to the
crankshaft.
[0015] Patent Document 1, however, concludes that providing the compression release mechanism
cannot solve the problems that are involved in lowness of the torque applied to the
crankshaft.
[0016] The present inventors conducted further studies on the operation of the compression
release mechanism, resulting in discovery that shortening a time period until completion
of engine start may be difficult under some operating condition of the compression
release mechanism.
[0017] If the compression release mechanism operates in a compression stroke, air (mixed
gas) contained in the cylinder is partially discharged through the exhaust valve.
In a combustion stroke that follows the compression stroke, the piston operates in
response to power caused by combustion of the mixed gas. The crankshaft is rotated
along with the operation of the piston.
[0018] Due to the operation of the compression release mechanism, the amount of mixed gas
contained in the cylinder is reduced. That is, a reduced amount of mixed gas is combusted
in the combustion stroke. Power caused by the combustion is reduced accordingly.
[0019] Combustion occurring after reception of a start instruction allows the piston and
the crankshaft to continue operation until a compression stroke subsequent to the
combustion. During this operation, the piston and the crankshaft receives a resistance
such as a friction. In a time period from the combustion stroke to the compression
stroke, the piston and the crankshaft operate while consuming power caused in the
combustion stroke. During this operation, the rotation speed of the crankshaft continues
decreasing. Particularly in a single-cylinder engine, each of the combustion stroke
and the compression stroke comes only once in two rotations of the crankshaft. Therefore,
a time period from the combustion stroke to the next compression stroke is long.
[0020] In the compression stroke, the piston compresses air, and thus the rotation speed
of the crankshaft further decreases because of a compression reaction force.
[0021] If combustion power is reduced due to the operation of the compression release mechanism,
the rotation speed of the crankshaft further decreases in a second compression stroke
coming after the combustion.
[0022] For example, if the rotation speed in the second compression stroke is equal to or
less than an operation upper limit speed which defines the operation of the compression
release mechanism, the compression release mechanism re-operates in the second compression
stroke.
[0023] The re-operation of the compression release mechanism makes it easy for the piston
to complete the second compression stroke. When the compression release mechanism
operates in the second compression stroke, however, the amount of mixed gas contained
in the cylinder is reduced. The compression ratio of the mixed gas is also reduced
accordingly. This results in just small power being caused in a combustion stroke
subsequent to the second compression stroke. Thus, the rotation speed of the crankshaft
is low after the combustion stroke subsequent to the second compression stroke. As
a consequence, the compression release mechanism may re-operate in a compression stroke
included in a third combustion cycle.
[0024] Particularly a single-cylinder engine, in which a high-load region and a low-load
region occur during four strokes, has characteristics that a torque required for rotating
the crankshaft largely varies.
[0025] In the single-cylinder engine, the compression release mechanism is required to sufficiently
discharge air from the cylinder in order to enable the piston to complete its operation
in the compression stroke after reception of a start instruction. If, however, the
compression release mechanism discharges air from the cylinder to such an extent that
the piston is able to complete its operation in the compression stroke of the single-cylinder
engine, the amount and compression ratio of mixed gas combusted in the next combustion
stroke subsequent to the current compression stroke are likely to be insufficient.
As a result, the compression release mechanism tends to re-operate in the second compression
stroke coming after the combustion stroke.
[0026] Due to the operation of the compression release mechanism, the rotation speed of
the crankshaft decreases after the combustion stroke, and the rotation speed further
decreases until the compression stroke coming after the combustion stroke. This can
cause a cycle of operations of the compression release mechanism. Even if the number
of times the compression release mechanism operates is not large, a time period until
completion of engine start is prolonged according to a time period during which the
operation of the compression release mechanism is repeated a plurality of times.
[0027] The present inventors considered an option of continuously operating the piston by
using a motor after completion of air compression which is a primary purpose of operating
the piston by the motor.
[0028] After the piston compresses air, the piston operates in response to power caused
by combustion. After the piston compresses air, the motor applies a force to the piston,
the force cooperating with a combustion force to assist the operation of the piston.
Due to the assistance of the motor, a decrease in the rotation speed of the crankshaft
is suppressed. Suppression of a decrease in the rotation speed of the crankshaft makes
it possible to avoid operating the compression release mechanism in a compression
stroke coming after the combustion. As a result, a larger amount of air (mixed gas)
is combusted in the combustion stroke, as compared with when the compression release
mechanism operates. Accordingly, the rotation speed of the crankshaft increases by
a large increment.
[0029] Once the rotation speed of the crankshaft increases by a large increment, an operation
of the compression release mechanism in compression strokes included in subsequent
combustion cycles is further avoided. Accordingly, the rotation speed of the crankshaft
further increases.
[0030] The control device of Patent Document 1, when starting a combustion control, terminates
rotation caused by the starter generator, and directs the starter generator to generate
power. That is, upon completion of air compression which is a primary purpose of operating
the piston, the operation of the piston performed by the starter generator is stopped.
In the next combustion cycle, therefore, the compression release mechanism operates,
which makes it likely that combustion of a small amount of mixed gas continues. A
time period required for increasing the rotation speed of the crankshaft tends to
be prolonged.
[0031] In the present teaching, on the other hand, the compression release mechanism is
operated in a first compression stroke, and upon completion of compression which is
one of primary purposes of operating the piston, a force is intentionally applied
to the piston by using the motor. Thus, characteristics obtained when the compression
release mechanism operates and characteristics obtained when the compression release
mechanism does not operate are exerted at appropriate times. As a result, the rotation
speed of the crankshaft increases in a short time. This shortens a time period until
completion of engine start after start of the combustion control.
[0032] The present teaching is a teaching accomplished based on the findings described above.
[0033] To solve the problems described above, the present teaching adopts the configuration
according to the wording of the enclosed claim 1.
[0034] In the single-cylinder engine of the straddled vehicle of (1), the piston provided
in the cylinder is moved to and fro by combustion of the mixed gas. The crankshaft
is rotated along with the to-and-fro movement of the piston. The drive wheel receives
the rotational force of the crankshaft, to drive the straddled vehicle.
[0035] The rotor of the permanent magnet type motor is connected to the crankshaft. The
rotor is provided with the permanent magnet. The plurality of switching parts arranged
between the permanent magnet type motor and the battery control the current flowing
between the battery and the permanent magnet type motor. The switching parts are controlled
by the control device. The control device is able to control a force to be supplied
from the permanent magnet type motor to the piston via the crankshaft. The compression
release mechanism reduces pressure in the cylinder in a compression stroke. The compression
release mechanism reduces pressure in the cylinder in a case where the rotation speed
of the crankshaft is equal to or less than the pressure-reduction upper limit speed.
[0036] Upon reception of the start instruction, the control device starts the single-cylinder
engine. The control device directs the permanent magnet type motor to apply a force
to the piston via the crankshaft, to move the piston. In the first combustion cycle
coming after the start instruction, the rotation speed of the crankshaft is equal
to or less than the pressure-reduction upper limit speed. As a result, the compression
release mechanism operates in the compression stroke of the first combustion cycle.
That is, the compression release mechanism reduces pressure in the cylinder in the
compression stroke. The pressure reduction in the cylinder allows the piston to compress
air contained in the cylinder. Thus, the piston and the crankshaft overcome the peak
of a compression reaction force, and complete the compression stroke. In a combustion
stroke coming after the compression stroke, air contained in the cylinder is combusted,
so that a combustion force is applied to the piston and the crankshaft.
[0037] The control device controls the switching parts so as to direct the permanent magnet
type motor to apply a force to the piston such that, in the second combustion cycle,
the rotation speed of the crankshaft exceeds the pressure-reduction upper limit speed.
The piston is therefore moved by energy caused by combustion in the first combustion
cycle and energy supplied from the permanent magnet type motor. The permanent magnet
type motor is controlled such that the rotation speed of the crankshaft in the second
combustion cycle exceeds the pressure-reduction upper limit speed. Thus, the compression
release mechanism does not operate in the compression stroke of the second combustion
cycle. Reduction of the mixed gas contained in the cylinder is suppressed in the compression
stroke. Reduction of the compression ratio of the mixed gas contained in the cylinder
is also suppressed.
[0038] In a combustion stroke of the second combustion cycle, as compared with in the first
combustion cycle, a larger amount of mixed gas is combusted, because the compression
release mechanism does not operate. Accordingly, a stronger combustion force is obtained
as compared with in the first combustion cycle. The rotation speed of the crankshaft
increases by a greater increment as compared with in the first combustion cycle. The
increase in the rotation speed makes it further less likely that the compression release
mechanism operates in subsequent combustion cycles. The rotation speed of the crankshaft
further increases.
[0039] The straddled vehicle of (1), in which the rotation speed increases by a large increment,
provides a shortened time period until completion of engine start. Accordingly, a
time period until completion of engine start after an engine start instruction can
be shortened.
[0040] A combustion cycle of the single-cylinder engine of the present teaching is a time
period starting at an intake stroke and ending at an exhaust stroke. One combustion
cycle corresponds to two rotations of the crankshaft.
[0041] (2) The straddled vehicle of (1), in which
the control device controls the plurality of switching parts in such a manner that
the permanent magnet type motor continues application of a force to the piston via
the crankshaft until at least a compression stroke of the second combustion cycle.
[0042] In the configuration of (2), the permanent magnet type motor continues application
of a force to the piston until the compression stroke of the second combustion cycle.
This ensures that the permanent magnet type motor applies a force to the piston for
a long period before the compression stroke of the second combustion cycle. Particularly
in a single-cylinder engine, a low-load region is, when viewed based on the rotation
angle of the crankshaft as a reference, wider than a high-load region in which a load
on operations of the piston and the crankshaft increases along with air compression.
This ensures that the permanent magnet type motor applies a force to the piston for
a particularly long period. Therefore, for example, even when the permanent magnet
type motor is downsized from the viewpoint of mountability to the straddled vehicle,
movement of the piston is assisted to such an extent as to suppress an operation of
the compression release mechanism in the compression stroke of the second combustion
cycle. Early-start ability of the single-cylinder engine is enabled with improvement
in mountability of the permanent magnet type motor.
[0043] (3) The straddled vehicle of (2), in which
the control device controls the plurality of switching parts to such an extent that
the rotation speed of the crankshaft does not increase but decreases after a combustion
stroke that follows the compression stroke of the first combustion cycle and until
the compression stroke of the second combustion cycle.
[0044] If the rotation speed of the crankshaft increases to a sufficient level in the combustion
stroke that follows the compression stroke of the first combustion cycle, it is possible
to, even when the rotation speed of the crankshaft subsequently decreases, ensure
that the rotation speed of the crankshaft be higher than the pressure-reduction upper
limit speed for the compression release mechanism. Thus, the configuration of (3)
allows the permanent magnet type motor to be downsized to such an extent that the
rotation speed of the crankshaft decreases after the aforesaid combustion stroke.
The configuration of (3) enables early-start ability of the single-cylinder engine
with improvement in mountability of the permanent magnet type motor.
[0045] The straddled vehicle of the present teaching includes a drive wheel. Examples of
the straddled vehicle of the present teaching include motorcycles, motor tricycles,
and ATVs (All-Terrain Vehicles). The straddled vehicle of the present teaching includes,
for example, a compression release mechanism for which the pressure-reduction upper
limit speed is set as follows: upon completion of a first combustion, the rotation
speed of the crankshaft exceeds the pressure-reduction upper limit speed, and if the
permanent magnet type motor does not apply a force to the piston in a second combustion
cycle, the rotation speed of the crankshaft can possibly decrease to or below the
pressure-reduction upper limit speed.
[0046] The engine of the present teaching includes a cylinder, a piston, a crankshaft, and
a connecting rod. Examples of the crankshaft of the present teaching include a crankshaft
coupled to the piston with the connecting rod, and a crankshaft coupled to the piston
with another member in addition to the connecting rod. The crankshaft is configured
such that, for example, movement of the piston is converted into rotational motion
which is then transmitted to the crankshaft.
[0047] The engine of the present teaching causes the piston to move by combusting a mixed
gas including air and a fuel. The engine of the present teaching includes engines
of direct injection type and engines of intake manifold injection type.
[0048] The compression release mechanism of the present teaching includes a device configured
to reduce pressure in the cylinder by opening the exhaust valve in the compression
stroke, a device configured to reduce pressure in the cylinder by opening the intake
valve in the compression stroke, and the like. The compression release mechanism of
the present teaching may be a device configured to reduce pressure in the cylinder
by opening a pressure release valve in the compression stroke, the pressure release
valve provided separately from the exhaust valve and the intake valve.
[0049] In the present teaching, whether or not the rotation speed of the crankshaft in n-th
combustion cycle is equal to or less than the pressure-reduction upper limit speed
for the compression release mechanism is determined based on, for example, whether
or not the rotation speed obtained at a time of decision to operate the compression
release mechanism in the n-th combustion is equal to or less than the pressure-reduction
upper limit speed. Here, "n" is a positive integer. For example, in a case where decision
to operate the compression release mechanism is made based on the rotation speed in
the compression stroke; whether or not the rotation speed of the crankshaft is equal
to or less than the pressure-reduction upper limit speed is determined based on whether
or not the rotation speed in the compression stroke is equal to or less than the pressure-reduction
upper limit speed. Alternatively, for example, whether or not the rotation speed of
the crankshaft is equal to or less than the pressure-reduction upper limit speed may
be determined based on the rotation speed in a stroke other than the compression stroke.
[0050] The permanent magnet type motor of the present teaching is a motor including a permanent
magnet. The permanent magnet type motor of the present teaching includes a stator
and a rotor. The rotor of the permanent magnet type motor of the present teaching
includes a permanent magnet. The rotor of the permanent magnet type motor of the present
teaching includes no winding. The stator of the permanent magnet type motor of the
present teaching includes windings. The permanent magnet type motor of the present
teaching includes windings corresponding to a plurality of phases. The permanent magnet
type motor of the present teaching may include windings corresponding to two phases,
four phases, or more, for example. The permanent magnet type motor of the present
teaching, however, is able to easily perform a vector control and a phase control
when provided with windings corresponding to three phases, for example. The windings
of the stator are wound on a stator core. The rotor is rotated with the permanent
magnet facing the stator core with an air gap therebetween. The permanent magnet type
motor of the present teaching includes a motor of radial gap type and a motor of axial
gap type. The motor of radial gap type, which is the permanent magnet type motor of
the present teaching, includes a motor of outer rotor type and a motor of inner rotor
type, the motor of outer rotor type provided with a rotor that rotates outside a stator,
the motor of inner rotor type provided with a rotor that rotates inside a stator.
[0051] The permanent magnet type motor of the present teaching may generate power, for example.
The permanent magnet type motor of the present teaching includes a permanent magnet
type motor having a function as a generator and a permanent magnet type motor not
having a function as a generator.
[0052] In the present teaching, the rotor of the permanent magnet type motor includes a
rotor connected directly to the crankshaft, a rotor connected indirectly to the crankshaft
with interposition of a transmission mechanism, and the like. Examples of the transmission
mechanism include belts, chains, gears, speed reducers, speed increasers, and the
like. The rotor of the present teaching is preferably connected to the crankshaft
with its speed ratio fixed relative to the crankshaft.
[0053] The inverter of the present teaching includes the plurality of switching parts by
which a current outputted from the battery to the permanent magnet type motor is controlled.
The switching parts are transistors, for example. The switching parts include FETs
(Field Effect Transistors), thyristors, and IGBTs (Insulated Gate Bipolar Transistors),
for example. The inverter includes a bridge inverter composed of a plurality of switching
parts, for example.
[0054] The control device of the present teaching includes a control device configured to
control operations of the engine, for example. The control device of the present teaching,
however, also includes a control device different from a device configured to control
operations of the engine, for example.
[0055] The start instruction of the present teaching is an instruction to start the single-cylinder
engine. The start instruction is inputted from a starter switch to the control device
upon actuation of the starter switch, for example. In a case of the straddled vehicle
having an idling stop function, the control device determines a predefined engine
start condition, and executes a restart instruction by itself. Fulfillment of the
predefined engine start condition is included in the input of the start instruction.
[0056] For example, the control device of the present teaching may perform swing-back by,
after reception of a start instruction, driving the crankshaft once in reverse rotation
and then in forward rotation. For example, the control device may perform such processing
that forward rotation of the crankshaft in response to a start instruction is started
from a position where forward rotation of the crankshaft has stopped in response to
an engine stop instruction.
[0057] For example, the permanent magnet type motor of the present teaching may be configured
to continue application of a force to the piston, which application has been started
subsequent to a start instruction, even after a compression stroke of a first combustion
cycle. For example, the permanent magnet type motor of the present teaching may be
configured to stop application of a force after a compression stroke of a first combustion
cycle, and restart the application before a compression stroke of a second combustion
cycle.
[0058] How the control device of the present teaching controls the switching part so as
to direct the permanent magnet type motor to rotate the crankshaft includes, for example,
performing a direct control of a voltage phase corresponding to a rotor position,
performing a vector control in which a current component divided into a component
contributing to a torque and another component is controlled, or performing 120-degree
conduction.
[EFFECTS OF THE INVENTION]
[0059] The present teaching is able to shorten a time period until completion of engine
start after an engine start instruction.
[BRIEF DESCRIPTION OF THE DRAWINGS]
[0060]
FIG. 1 shows an external appearance of a straddled vehicle according to an embodiment
of the present teaching.
FIG. 2 is a partial cross-sectional view schematically showing an outline configuration
of an engine unit shown in FIG. 1.
FIG. 3 is an illustrative diagram schematically showing the relationship between a
crank angle position and a required torque of a single-cylinder engine.
FIG. 4 is a cross-sectional view of a permanent magnet type motor shown in FIG. 2,
as sectioned perpendicular to its rotation axis line.
FIG. 5 is a block diagram outlining an electrical configuration of the straddled vehicle
shown in FIG. 1.
FIG. 6 is a flowchart illustrating operations concerning start of the straddled vehicle.
FIG. 7(A) is a timing chart showing a state at a time of start of a single-cylinder
engine according to this embodiment; and FIG. 7(B) is a timing chart showing a state
at a time of start of a single-cylinder engine according to a comparative example.
[EMBODIMENTS FOR CARRYING OUT THE INVENTION]
[0061] Hereunder, the present teaching is described based on preferred embodiments with
reference to the drawings.
[0062] FIG. 1 shows an external appearance of a straddled vehicle according to an embodiment
of the present teaching.
[0063] A straddled vehicle 1 shown in FIG. 1 includes a vehicle body 2 and wheels 3a, 3b.
The straddled vehicle 1 is, to be specific, a motorcycle.
[0064] The straddled vehicle I includes an engine unit EU. The engine unit EU includes a
single-cylinder engine 10 (see FIG. 2).
[0065] The rear wheel 3b is a drive wheel. The wheel 3b receives a rotational force outputted
from the single-cylinder engine 10, to drive the straddled vehicle 1.
[0066] The straddled vehicle 1 includes a main switch 5. The main switch 5 is a switch for
supplying power to each part of the straddled vehicle 1. The straddled vehicle 1 includes
a starter switch 6. The starter switch 6 is a switch for starting the single-cylinder
engine 10. The straddled vehicle 1 includes an acceleration command part 8. The acceleration
command part 8 is an operation element for instructing acceleration of the straddled
vehicle 1 in accordance with an operation thereon. The acceleration command part 8
is, to be specific, an accelerator grip.
[0067] The straddled vehicle 1 includes a battery 4. The straddled vehicle 1 includes a
control device 60 that controls each part of the straddled vehicle 1.
[0068] FIG. 2 is a partial cross-sectional view schematically showing an outline configuration
of the engine unit EU shown in FIG. 1.
[0069] The engine unit EU includes the single-cylinder engine 10 and a permanent magnet
type motor 20.
[0070] The single-cylinder engine 10 includes a crank case 11, a cylinder 12, a piston 13,
a connecting rod 14, and a crankshaft 15. The piston 13 is arranged in the cylinder
12 such that the piston 13 is freely movable to and fro.
[0071] The crankshaft 15 is rotatably arranged in the crank case 11. The crankshaft 15 is
coupled to the piston 13 with the connecting rod 14. A cylinder head 16 is attached
to an upper portion of the cylinder 12. The cylinder 12, the cylinder head 16, and
the piston 13 define a combustion chamber.
[0072] The cylinder head 16 is provided with an exhaust valve 18 and an intake valve (not
shown). The exhaust valve 18 controls discharge of an exhaust gas from the cylinder
12. The intake valve controls supply of a mixed gas to a combustion chamber provided
in the cylinder 12. The exhaust valve 18 and the intake valve are moved by operations
of a cam (not shown) provided to a cam shaft Cs which is rotatable together with the
crankshaft 15.
[0073] The crankshaft 15 is supported on the crank case 11 via a pair of bearings 17 in
a freely rotatable manner. The permanent magnet type motor 20 is attached to one end
portion 15a of the crankshaft 15. A transmission CVT is attached to the other end
portion 15b of the crankshaft 15. The transmission CVT is configured to change the
gear ratio which is the ratio of an output rotation speed to an input rotation speed.
The transmission CVT is configured to change the gear ratio corresponding to the rotation
speed of the wheel relative to the rotation speed of the crankshaft 15.
[0074] The engine unit EU includes a compression release mechanism D. FIG. 2 schematically
illustrates the compression release mechanism D. The compression release mechanism
D is operable to reduce pressure in the cylinder 12 in a compression stroke. In the
compression stroke, the compression release mechanism D opens the exhaust valve 18,
to discharge part of the mixed gas from the cylinder 12. The compression release mechanism
D is configured to open the exhaust valve 18 in the compression stroke if the rotation
speed of the crankshaft 15 is equal to or less than a pressure-reduction upper limit
speed which is set for the compression release mechanism D.
[0075] The compression release mechanism D opens the exhaust valve 18 by means of a mechanism
provided to the cam shaft Cs which is rotatable together with the crankshaft 15. For
example, the compression release mechanism D performs the operation of opening the
exhaust valve 18 by using a centrifugal force generated by rotation of the cam shaft
Cs.
[0076] As the compression release mechanism D reduces pressure of the mixed gas contained
in the cylinder 12 in the compression stroke, a compression reaction force received
by the piston 13 is reduced. A load put on operation of the piston 13 is lowered in
a high-load region.
[0077] The engine unit EU is also provided with a throttle valve (not shown) and a fuel
injector device J (see FIG. 5). The degree to which the throttle valve opens is based
on the amount of operation on the acceleration command part 8 (see FIG. 1). The throttle
valve adjusts the amount of air flowing therethrough in accordance with the degree
of opening, thus adjusting the amount of air to be supplied into the cylinder 12.
The fuel injector device J injects a fuel, so that the fuel is supplied to a combustion
chamber provided in the cylinder 12. A mixed gas, which is a mixture of the air flowing
through the throttle valve and the fuel injected from the fuel injector device J,
is supplied to the combustion chamber provided in the cylinder 12.
[0078] The single-cylinder engine 10 is provided with a spark plug 19. The spark plug 19
ignites the mixed gas contained in the cylinder 12, so that the mixed gas is combusted.
[0079] The single-cylinder engine 10 is an internal combustion engine. The single-cylinder
engine 10 is supplied with a fuel. The single-cylinder engine 10 outputs a rotational
force by performing a combustion operation in which the mixed gas is combusted.
[0080] More specifically, the mixed gas containing the fuel supplied to the combustion chamber
is combusted, to move the piston 13. The combustion of the mixed gas makes the piston
13 move to and fro. The crankshaft 15 is rotated along with the to-and-fro movement
of the piston 13. The rotational force is outputted to the outside of the single-cylinder
engine 10 via the crankshaft 15. The wheel 3b (see FIG. 1) receives the rotational
force outputted from the single-cylinder engine 10 via the crankshaft 15, to drive
the straddled vehicle 1.
[0081] The single-cylinder engine 10 outputs the rotational force via the crankshaft 15.
The rotational force of the crankshaft 15 is transmitted to the wheel 3b via the transmission
CVT and a clutch CL (see FIG. 1). The straddled vehicle 1 is driven by the wheel 3b
receiving the rotational force from the single-cylinder engine 10 via the crankshaft
15.
[0082] FIG. 3 is an illustrative diagram schematically showing the relationship between
a crank angle position and a required torque of the single-cylinder engine 10. FIG.
3 shows the torque required for rotating the crankshaft 15 under a state where the
single-cylinder engine 10 does not perform the combustion operation.
[0083] The single-cylinder engine 10 is a four-stroke engine. The single-cylinder engine
10 has, during four strokes which correspond to one combustion cycle, a high-load
region TH in which a high load is put on rotation of the crankshaft 15 and a low-load
region TL in which a load put on rotation of the crankshaft 15 is lower than that
of the high-load region TH. The high-load region means a region in one combustion
cycle of the single-cylinder engine 10 where a load torque is higher than an average
value Av of the load torque over the one combustion cycle. From the viewpoint of the
rotation angle of the crankshaft 15, the low-load region TL is equal to or wider than
the high-load region TH. To be specific, the low-load region TL is wider than the
high-load region TH. In other words, a rotation angle region corresponding to the
low-load region TL is wider than a rotation angle region corresponding to the high-load
region TH. During rotation, the single-cylinder engine 10 repeats a combustion stroke
(expansion stroke), an exhaust stroke, an intake stroke, and a compression stroke.
The compression stroke overlaps the high-load region TH.
[0084] One combustion cycle of the single-cylinder engine 10 includes one combustion stroke,
one exhaust stroke, one intake stroke, and one compression stroke.
[0085] In the intake stroke, the mixed gas is supplied to the combustion chamber. In the
compression stroke, the piston 13 compresses the mixed gas contained in the combustion
chamber. In the expansion stroke, the mixed gas ignited by the spark plug 19 is combusted,
and pushes the piston 13. In the exhaust stroke, an exhaust gas existing after the
combustion is discharged from the combustion chamber.
[0086] FIG. 4 is a cross-sectional view of the permanent magnet type motor 20 shown in FIG.
2, as sectioned perpendicular to its rotation axis line.
[0087] The permanent magnet type motor 20 is described with reference to FIGS. 2 and 4.
[0088] The permanent magnet type motor 20 is a three-phase brushless motor of permanent
magnet type. The permanent magnet type motor 20 functions also as a three-phase brushless
generator of permanent magnet type.
[0089] The permanent magnet type motor 20 includes a rotor 30 and a stator 40. The permanent
magnet type motor 20 of this embodiment is of radial gap type. The permanent magnet
type motor 20 is of outer rotor type. That is, the rotor 30 is an outer rotor, and
the stator 40 is an inner stator.
[0090] The rotor 30 includes a rotor body part 31. The rotor body part 31 is made of, for
example, a ferromagnetic material. The rotor body part 31 is in the shape of a cylinder
with a bottom. The rotor body part 31 includes a cylindrical boss portion 32, a disk-shaped
bottom wall portion 33, and a back yoke portion 34 having a cylindrical shape. The
bottom wall portion 33 and the back yoke portion 34 are integrally formed. Here, it
may also be acceptable that the bottom wall portion 33 and the back yoke portion 34
are formed as separate parts. The bottom wall portion 33 and the back yoke portion
34 are secured to the crankshaft 15 via the cylindrical boss portion 32. A winding
to which a current is supplied is not provided in the rotor 30.
[0091] The rotor 30 includes a permanent magnet part 37. The rotor 30 includes a plurality
of magnetic pole portions 37a. The plurality of magnetic pole portions 37a are formed
by the permanent magnet part 37. The plurality of magnetic pole portions 37a are provided
on an inner circumferential surface of the back yoke portion 34. In this embodiment,
the permanent magnet part 37 includes a plurality of permanent magnets. That is, the
rotor 30 includes a plurality of permanent magnets. The plurality of magnetic pole
portions 37a are provided in the plurality of permanent magnets, respectively.
[0092] The permanent magnet part 37 may alternatively be configured as a single annular
permanent magnet. In such a configuration, the single permanent magnet is magnetized
such that the plurality of magnetic pole portions 37a appear side by side on the inner
circumferential surface.
[0093] The plurality of magnetic pole portions 37a are provided such that N pole and S pole
appear alternately with respect to the circumferential direction of the permanent
magnet type motor 20. In this embodiment, the number of magnetic poles of the rotor
30 opposed to the stator 40 is twenty-four. The number of magnetic poles of the rotor
30 means the number of magnetic poles opposed to the stator 40. No magnetic material
is arranged between the magnetic pole portions 37a and the stator 40.
[0094] The magnetic pole portions 37a are provided outside the stator 40 with respect to
the radial direction of the permanent magnet type motor 20. The back yoke portion
34 is provided outside the magnetic pole portions 37a with respect to the radial direction.
The number of magnetic pole portions 37a included in the permanent magnet type motor
20 is more than the number of teeth 43.
[0095] The rotor 30 may be of interior permanent magnet type (IPM type) in which the magnetic
pole portions 37a are embedded in a magnetic element, but it preferably is of surface
permanent magnet type (SPM type) in which the magnetic pole portions 37a are exposed
from a magnetic element as illustrated in this embodiment.
[0096] A cooling fan F is provided to the bottom wall portion 33 of the rotor 30.
[0097] The stator 40 includes a stator core ST and a plurality of stator windings W. The
stator core ST includes a plurality of teeth 43 arranged at intervals with respect
to the circumferential direction. The plurality of teeth 43 integrally extend from
the stator core ST toward radially outside. In this embodiment, eighteen teeth 43
in total are arranged at intervals with respect to the circumferential direction.
In other words, the stator core ST has eighteen slots SL in total that are arranged
at intervals with respect to the circumferential direction. The teeth 43 are arranged
at equal intervals with respect to the circumferential direction.
[0098] The number of magnetic pole portions 37a included in the rotor 30 is more than the
number of teeth 43. The number of magnetic pole portions is equal to 4/3 of the number
of slots.
[0099] The stator winding W is wound around each of the teeth 43. That is, the multi-phase
stator windings W are arranged through the slots SL. In the state shown in FIG. 4,
the stator windings W are in the slots SL. Each of the multi-phase stator windings
W belongs to any of U-phase, V-phase, and W-phase. The stator windings W are arranged
in the order of U-phase, V-phase, and W-phase, for example.
[0100] The rotor 30 includes, on its outer surface, a plurality of detection object parts
38 for detection of the rotation position of the rotor 30. Magnetic effects are used
to detect the plurality of detection object parts 38. The plurality of detection object
parts 38 arranged at intervals with respect to the circumferential direction are provided
on the outer surface of the rotor 30. The detection object parts 38 are made of a
ferromagnetic material.
[0101] The rotor position detection device 50 is a device that detects the position of the
rotor 30. The rotor position detection device 50 is provided at a position allowed
to be opposed to the plurality of detection object parts 38. The rotor position detection
device 50 includes a pick-up coil and a magnet. The rotor position detection device
50 magnetically detects the detection object parts 38. The rotor position detection
device for detecting the position of the rotor may be implemented as a Hall IC configured
to detect the magnetic pole portions 37.
[0102] The rotor 30 of the permanent magnet type motor 20 is connected to the crankshaft
15 such that the rotor 30 is rotated along with rotation of the crankshaft 15. More
specifically, the rotor 30 of the permanent magnet type motor 20 is connected to the
crankshaft 15 such that the rotor 30 is rotated with its speed ratio fixed relative
to the crankshaft 15. The rotor 30 is directly connected to the crankshaft 15 of the
single-cylinder engine 10.
[0103] In this embodiment, the rotor 30 is attached to the crankshaft 15 without interposition
of a power transmission mechanism (such as a belt, a chain, a gear, a speed reducer,
or a speed increaser). The rotor 30 is rotated with a speed ratio of 1:1 relative
to the crankshaft 15. The permanent magnet type motor 20 is configured such that the
rotor 30 is driven in forward rotation at a time of combustion operation of the single-cylinder
engine 10.
[0104] The rotation axis line of the permanent magnet type motor 20 is substantially coincident
with the rotation axis line of the crankshaft 15.
[0105] At a time of engine start, the permanent magnet type motor 20 drives the crankshaft
15 in forward rotation to start the single-cylinder engine 10. At a time of combustion
operation of the single-cylinder engine 10, the permanent magnet type motor 20 is
driven by the single-cylinder engine 10 to generate power. That is, the permanent
magnet type motor 20 has both the function for driving the crankshaft 15 in forward
rotation to start the single-cylinder engine 10 and the function for being driven
by the single-cylinder engine 10 to generate power at a time of combustion operation
of the single-cylinder engine 10. During at least part of a time period following
the start of the single-cylinder engine 10, the permanent magnet type motor 20 is
driven in forward rotation by the crankshaft 15 to function as a generator.
[0106] FIG. 5 is a block diagram outlining an electrical configuration of the straddled
vehicle 1 shown in FIG. 1.
[0107] The straddled vehicle 1 includes an inverter 61. The control device 60 controls components
of the straddled vehicle 1 including the inverter 61.
[0108] The permanent magnet type motor 20 and the battery 4 are connected to the inverter
61. When the permanent magnet type motor 20 operates as a motor, the battery 4 supplies
power to the permanent magnet type motor 20. The battery 4 is charged with power generated
by the permanent magnet type motor 20.
[0109] The battery 4 is connected to the inverter 61 and a power consuming apparatus via
the main switch 5. The power consuming apparatus 70 is an apparatus that consumes
power when operating. The power consuming apparatus 70 includes a headlight 7 (see
FIG. 1), for example.
[0110] The inverter 61 includes a plurality of switching parts 611 to 616. In this embodiment,
the inverter 61 includes six switching parts 611 to 616.
[0111] The switching parts 611 to 616 constitute a three-phase bridge inverter. The plurality
of switching parts 611 to 616 are connected to the respective phases of the multi-phase
stator windings W. More specifically, among the plurality of switching parts 611 to
616, every two switching parts that are connected in series constitute a half bridge.
The half bridge corresponding to each phase is connected in parallel with the battery
4. Ones of the switching parts 611 to 616 constituting the half bridge of each phase
are connected to the corresponding phase of the multi-phase stator windings W.
[0112] The switching parts 611 to 616 control a current flowing between the battery 4 and
the permanent magnet type motor 20. The switching parts 611 to 616 selectively allow
or block the passing of a current between the battery 4 and the multi-phase stator
windings W.
[0113] In more detail, when the permanent magnet type motor 20 functions as a motor, switching
between causing and stopping conduction of the multi-phase stator windings W is implemented
by on/off-operation of the switching parts 611 to 616.
[0114] When the permanent magnet type motor 20 functions as a generator, switching between
allowing and blocking the passing of a current between each of the stator windings
W and the battery 4 is implemented by on/off-operation of the switching parts 611
to 616. By switching on/off the switching parts 611 to 616 one after another, a control
of a voltage and a rectification of a three-phase AC outputted from the permanent
magnet type motor 20 are performed. The switching parts 611 to 616 control a current
outputted from the permanent magnet type motor 20 to the battery 4.
[0115] Each of the switching parts 611 to 616 has a switching element. The switching element
is, for example, a transistor and in more detail, an FET (Field Effect Transistor).
[0116] The fuel injector device J, the spark plug 19, and the battery 4 are connected to
the control device 60.
[0117] The rotor position detection device 50 is also connected to the control device 60.
The control device 60 obtains the rotation speed of the crankshaft 15 based on a result
of detection performed by the rotor position detection device 50.
[0118] The control device 60 obtains the amount of operation on the acceleration command
part 8 and the rate of increase in the amount of operation based on, for example,
a result of detection performed by a throttle position sensor (not shown).
[0119] The control device 60 includes a starter power-generator control unit 62 and a combustion
control unit 63.
[0120] The starter power-generator control unit 62 controls on/off-operation of each of
the switching parts 611 to 616, to control the operation of the permanent magnet type
motor 20. The starter power-generator control unit 62 includes a start control unit
621 and a power generation control unit 622.
[0121] The combustion control unit 63 controls the spark plug 19 and the fuel injector device
J, to control the combustion operation of the single-cylinder engine 10. The combustion
control unit 63 controls the spark plug 19 and the fuel injector device J, to control
a rotational force of the single-cylinder engine 10. The combustion control unit 63
controls the spark plug 19 and the fuel injector device J in accordance with the degree
of opening of the throttle valve SV which is represented by an output signal of the
throttle position sensor.
[0122] The control device 60 is composed of a computer including a central processing unit
(not shown) and a storage device (not shown). The central processing unit executes
arithmetic processing based on a control program. The storage device stores data relating
to programs and arithmetic operations.
[0123] The combustion control unit 63 and the starter power-generator control unit 62 including
the start control unit 621 and the power generation control unit 622 are implemented
by a computer (not shown) and a control program executable by the computer. Thus,
below-described operations performed respectively by the combustion control unit 63
and the starter power-generator control unit 62 including the start control unit 621
and the power generation control unit 622 can be considered as operations performed
by the control device 60. The starter power-generator control unit 62 and the combustion
control unit 63 may be, for example, either configured as separate devices placed
at a distance from each other, or integrated as a single device.
[0124] The starter switch 6 is connected to the control device 60. The starter switch 6
is actuated by a rider at a time of starting the single-cylinder engine 10.
[0125] The main switch 5 supplies power to the control device 60 in accordance with operations
performed thereon.
[0126] The starter power-generator control unit 62 and the combustion control unit 63 of
the control device 60 control the single-cylinder engine 10 and the permanent magnet
type motor 20. The starter power-generator control unit 62 controls the inverter 61.
[0127] FIG. 6 is a flowchart illustrating operations concerning engine start of the straddled
vehicle 1.
[0128] Operations of the straddled vehicle 1 are described with reference to FIGS. 5 and
6. The operations of the straddled vehicle 1 are controlled by the control device
60.
[0129] Upon reception of a start instruction for starting the single-cylinder engine 10
(S11:Yes), the control device 60 starts the single-cylinder engine 10. More specifically,
when the main switch 5 is in on-state and the starter switch 6 is in on-state, the
control device 60 starts the single-cylinder engine 10. In starting the single-cylinder
engine 10, the control device 60 operates the piston 13 (S12). To be exact, the start
control unit 621 of the starter power-generator control unit 62 operates the piston
13 (S12). The start control unit 621 controls the switching parts 611 to 616 of the
inverter 61 such that the permanent magnet type motor 20 rotates the crankshaft 15.
The permanent magnet type motor 20 applies a force to the piston 13 via the crankshaft
15. As a result, the piston 13 is operated.
[0130] In operating the piston 13, the control device 60 performs on/off-operation of the
plurality of switching parts 611 to 616 at predefined timings such that the permanent
magnet type motor 20 is rotated with power of the battery 4.
[0131] The control device 60 rotates the permanent magnet type motor 20 such that, in a
first combustion cycle following a start instruction, the rotation speed of the crankshaft
15 is equal to or less than the pressure-reduction upper limit speed for the compression
release mechanism D. More specifically, the control device 60 rotates the permanent
magnet type motor 20 such that the rotation speed of the crankshaft 15 in a compression
stroke of the first combustion cycle be equal to or less than the pressure-reduction
upper limit speed. The rotation speed of the crankshaft 15, in general, increases
after start of the rotation. After start of the rotation, the permanent magnet type
motor 20 rotates the crankshaft 15 such that the increased rotation speed is equal
to or less than the pressure-reduction upper limit speed in the compression stroke.
[0132] The control device 60 rotates the permanent magnet type motor 20 such that, in a
second combustion cycle, the rotation speed of the crankshaft 15 exceeds the pressure-reduction
upper limit speed for the compression release mechanism D. Combustion that occurs
subsequent to the compression stroke of the first combustion cycle results in application
of a force to the piston 13, the force rotating the crankshaft 15 at a rotation speed
higher than the pressure-reduction upper limit speed. The permanent magnet type motor
20 rotates the crankshaft 15 to such an extent that the rotation speed of the crankshaft
15 does not fall to or below the pressure-reduction upper limit speed. The control
device 60 rotates the permanent magnet type motor 20 to such an extent that the rotation
speed of the crankshaft 15 does not increase but decreases after the combustion stroke
that follows the compression stroke of the first combustion cycle and until a compression
stroke of the second combustion cycle.
[0133] The control device 60 drives the permanent magnet type motor 20 with power of the
battery 4 by, for example, controlling the switching parts 611 to 616 based on a vector
control scheme. For example, the control device 60 controls a command value that contributes
to a torque of the permanent magnet type motor 20, to control the torque to be outputted
from the permanent magnet type motor 20. Thus, the control device 60 controls a force
to be applied from the permanent magnet type motor 20 to the piston 13 via the crankshaft
15.
[0134] The permanent magnet type motor 20 rotates the crankshaft 15 to such an extent that
the rotation speed of the crankshaft 15 decreases but does not fall to or below the
pressure-reduction upper limit speed after the combustion stroke that follows the
compression stroke of the first combustion cycle and until the compression stroke
of the second combustion cycle. During this operation, the permanent magnet type motor
20 does not increase the rotation speed of the crankshaft 15. This allows a small-size
motor to be adopted as the permanent magnet type motor 20.
[0135] Then, the control device 60 performs initial combustion operation processing (S13).
To be exact, the combustion control unit 63 performs the initial combustion operation
processing.
[0136] In the initial combustion operation processing of step S13 mentioned above, the combustion
control unit 63 supplies a fuel to the single-cylinder engine 10 when the crankshaft
15 is at a predefined fuel supply position within the combustion cycle. The combustion
control unit 63 directs the fuel injector device to inject the fuel. The fuel supply
position of this embodiment is, for example, a position before the intake stroke.
The combustion control unit 63 directs the fuel injector device to inject the fuel
before the intake stroke. The combustion control unit 63 counts the number of times
the fuel is injected after the start instruction.
[0137] In the initial combustion operation processing of step S13 mentioned above, the combustion
control unit 63 ignites a mixed gas contained in the cylinder 12 when the crankshaft
15 is at a predefined ignition position within the combustion cycle. The ignition
position is a position near the top dead center. The combustion control unit 63 directs
the spark plug 19 to ignite the mixed gas when the crankshaft 15 is at the ignition
position.
[0138] Then, the control device 60 determines whether or not the number of times the fuel
is injected is equal to or greater than a predefined initial injection frequency (S14).
For example, the initial injection frequency is set to a value equal to or greater
than "2". In one example, the initial injection frequency is set to "2". In another
example, the initial injection frequency may be set to a value equal to or greater
than "3".
[0139] If the number of times the fuel is injected is less than at least the initial injection
frequency, the control device 60 directs the permanent magnet type motor 20 to continue
the operation of the piston 13 (S12) and the initial combustion operation (S13). The
permanent magnet type motor 20 continues the application of the force to the piston
13 via the crankshaft 15 until the compression stroke of the second combustion cycle.
[0140] If the number of times the fuel is injected is equal to or greater than the initial
injection frequency (S14:Yes), the control device 60 determines whether or not the
rotation speed of the crankshaft 15 is equal to or more than a predefined start completion
speed (S15).
[0141] For example, the start completion speed is set so as to ensure that the rotation
speed in the compression stroke be higher than the pressure-reduction upper limit
speed for the compression release mechanism D when the rotation speed of the crankshaft
15 decreases after the permanent magnet type motor 20 terminates the application of
the force. The start completion speed is a speed lower than an engagement speed of
the clutch CL.
[0142] Upon determination in step S15 that the rotation speed of the crankshaft 15 is equal
to or less than the start completion speed (S15:No), the control device 60 directs
the permanent magnet type motor 20 to continue the operation of the piston 13 (S12)
and the initial combustion operation (S13).
[0143] In the operation of the piston 13 performed by the permanent magnet type motor 20
(S12), the control device 60 controls the plurality of switching parts 611 to 616
included in the inverter 61 such that power is supplied from the battery 4 to the
permanent magnet type motor 20. In this manner, the control device 60 directs the
permanent magnet type motor 20 to move the piston 13 to and fro. The control device
60 causes power running of the permanent magnet type motor 20. After combustion occurs
in the single-cylinder engine 10, the permanent magnet type motor 20 applies a force
to the piston 13 via the crankshaft 15, thus cooperating with a combustion force of
the single-cylinder engine 10 to move the piston 13 to and fro.
[0144] Upon determination in step S15 mentioned above that a maximum rotation speed of the
crankshaft 15 exceeds the start completion speed (S15:Yes), the control device 60
directs the permanent magnet type motor 20 to stop operating the piston 13 (S16).
[0145] Depending on results of determination made in steps S14 and S15 mentioned above,
the control device 60 directs the permanent magnet type motor 20 to continue the operation
of the piston 13 (S12) and the initial combustion operation (S13), thus applying a
force to the piston 13 via the crankshaft 15 such that, in the second combustion cycle,
the rotation speed of the crankshaft 15 exceeds the pressure-reduction upper limit
speed. More specifically, the control device 60 directs the permanent magnet type
motor 20 to continue the operation of the piston 13 (S12) until expectation is obtained
that the rotation speed of the crankshaft 15 in the compression stroke of the second
combustion cycle will exceed the pressure-reduction upper limit speed.
[0146] Upon determination in step S15 mentioned above that the rotation speed of the crankshaft
15 exceeds the start completion speed (S15:Yes), the control device 60 directs the
permanent magnet type motor 20 to stop operating the piston 13 (S16). Also, the control
device 60 starts a power generation control (S17). To be exact, the power generation
control unit 622 of the starter power-generator control unit 62 performs the power
generation control. In the power generation control, the control device 60 controls
the switching parts 611 to 616 such that the permanent magnet type motor 20 acts as
a generator. As the permanent magnet type motor 20 generates power, the battery 4
is charged.
[0147] Then, the control device 60 starts a normal combustion operation (S18). In the normal
combustion operation, the control device 60 controls the amount of fuel supply based
on the amount of air supplied into the cylinder 12. The control device 60 also controls
the amount of fuel supply based on the amount of operation on the acceleration command
part 8.
[0148] FIGS. 7(A) and 7(B) are timing charts showing states at a time of start of the single-cylinder
engine 10. FIG. 7(A) schematically shows a state of the single-cylinder engine 10
according to this embodiment. FIG. 7(B) shows a state according to a comparative example.
[0149] In the charts of FIG. 7, the rotation speeds V1, V2 of the crankshaft are shown.
In the charts of FIG. 7, the degrees E1, E2 of opening of the exhaust valve, and time
periods PI, P2 during which the piston 13 is operated by the permanent magnet type
motor 20 are shown, too. Open of the exhaust valve occurs mainly in an exhaust stroke.
In a case of the compression release mechanism D operating, the exhaust valve is opened
in a compression stroke.
[0150] As shown in FIG. 7(A), upon reception of a start instruction at time t11, the permanent
magnet type motor 20 moves the piston 13 by applying a force to the piston 13 via
the crankshaft 15. The rotation speed V1 of the crankshaft 15 rises from "0". The
permanent magnet type motor 20 rotates the crankshaft 15 such that the rotation speed
V1 of the crankshaft 15 is equal to or less than the pressure-reduction upper limit
speed Ld in a first combustion cycle after the reception of the start instruction.
More specifically, the permanent magnet type motor 20 rotates the crankshaft 15 such
that, in a compression stroke of the first combustion cycle, the rotation speed V1
of the crankshaft 15 is equal to or less than the pressure-reduction upper limit speed
Ld.
[0151] In this embodiment, the crankshaft 15 starts rotation at a position at least before
an intake stroke. Thus, a fuel injection is performed before the intake stroke.
[0152] As a result, at time t12, the compression release mechanism D operates. At time t12,
the degree E1 of opening of the exhaust valve rises from 0, which indicates that the
exhaust valve is opened. Since the exhaust valve is opened in the compression stroke,
the mixed gas contained in the cylinder 12 is partially discharged. This enables the
piston 13 to compress the mixed gas contained in the cylinder 12, so that the compression
top dead center can be overcome.
[0153] In a combustion stroke that follows the compression stroke, the mixed gas contained
in the cylinder 12 is combusted. Since the piston 13 receives a combustion force,
the rotation speed V1 of the crankshaft 15 rises.
[0154] The permanent magnet type motor 20 continues the application of the force to the
piston 13 via the crankshaft 15. After the combustion subsequent to the compression
stroke of the first combustion cycle, the crankshaft 15 and the piston 13 are driven
by energy of the combustion as well as the force applied from the permanent magnet
type motor 20. Here, the combustion subsequent to the compression stroke of the first
combustion cycle means combustion occurring in a combustion stroke of a second combustion
cycle.
[0155] The permanent magnet type motor 20 applies a force to the piston 13 via the crankshaft
15 such that, in the second combustion cycle, the rotation speed of the crankshaft
15 exceeds the pressure-reduction upper limit speed Ld for the compression release
mechanism D. The permanent magnet type motor 20 applies a force to the piston 13 via
the crankshaft 15. This ensures that, in a compression stroke of the second combustion
cycle, the rotation speed of the crankshaft 15 exceeds the pressure-reduction upper
limit speed Ld for the compression release mechanism D. As a result, at time t14 which
is in the compression stroke of the second combustion cycle, compression of the mixed
gas is assisted by the permanent magnet type motor 20.
[0156] After the combustion stroke of the second combustion cycle, the permanent magnet
type motor 20 applies a force to the piston 13 to such an extent that the rotation
speed of the crankshaft 15 does not increase but decreases until the compression stroke
of the second combustion cycle. Accordingly, the rotation speed of the crankshaft
15 does not increase but decreases in a period from the combustion stroke of the second
combustion cycle to the compression stroke of the second combustion cycle.
[0157] At time t14 which is in the compression stroke of the second combustion cycle, the
compression release mechanism D does not operate, because the rotation speed of the
crankshaft 15 exceeds the pressure-reduction upper limit speed Ld. At time t14, therefore,
the exhaust valve is not opened.
[0158] At time t15 which is in a combustion stroke of a third combustion cycle, combustion
occurs so that the rotation speed of the crankshaft 15 further rises.
[0159] In the comparative example shown in FIG. 7(B), the permanent magnet type motor 20
stops application of a force to the piston 13 in a combustion stroke of a first combustion
cycle. A combustion force makes the rotation speed of the crankshaft 15 exceed the
pressure-reduction upper limit speed Ld for the compression release mechanism D at
time t23. The rotation speed of the crankshaft 15, however, decreases and falls below
the pressure-reduction upper limit speed Ld. In a second combustion cycle, therefore,
the compression release mechanism D re-operates. As indicated by the degree E2 of
opening of the exhaust valve, the exhaust valve is opened at time t24 which is in
a compression stroke of the second combustion cycle.
[0160] At time t25 which is in a combustion stroke of the second combustion cycle, combustion
occurs so that the rotation speed of the crankshaft 15 further rises. In the immediately
preceding compression stroke, however, the mixed gas contained in the cylinder 12
is reduced. The compression ratio of the mixed gas is also reduced.
[0161] This is why just small power is caused in the combustion stroke which follows the
compression stroke. Thus, the rotation speed of the crankshaft 15 after the combustion
stroke of the second combustion cycle is lower than that shown in FIG. 7(A).
[0162] A low rotation speed of the crankshaft 15 in the second combustion cycle results
in the rotation speed of the crankshaft 15 falling below the pressure-reduction upper
limit speed Ld again in a third combustion cycle, though not shown in FIG. 7(B). The
compression release mechanism may sometimes re-operate in a compression stroke of
the third combustion cycle.
[0163] In the comparative example shown in FIG. 7(B), as described above, a time period
until completion of engine start is prolonged in accordance with the number of combustion
cycles in which the compression release mechanism D operates.
[0164] In the example of this embodiment shown in FIG. 7(A), on the other hand, the rotation
speed of the crankshaft 15 in the second combustion cycle exceeds the pressure-reduction
upper limit speed. Therefore, pressure of the mixed gas contained in the cylinder
is not reduced, which is otherwise caused by the operation of the compression release
mechanism D. A stronger combustion force is obtained as compared with in the first
combustion cycle. The rotation speed of the crankshaft, which is rotated along with
the piston to which the stronger force is applied, further increases. This results
in shortening a time period until completion of engine start.
[0165] It should be understood that the terms and expressions used in the above embodiments
are for descriptions and not to be construed in a limited manner, do not eliminate
any equivalents of features shown and mentioned herein, and allow various modifications
falling within the scope of the enclosed claims. The present teaching may be embodied
in many different forms. The present disclosure is to be considered as providing embodiments
of the principles of the teaching. The embodiments are described herein with the understanding
that such embodiments are not intended to limit the teaching to preferred embodiments
described herein and/or illustrated herein. The embodiments described herein are not
limiting. The present teaching includes any and all embodiments having equivalent
elements, modifications, omissions, combinations, adaptations and/or alterations as
would be appreciated by those in the art based on the present disclosure.
[0166] The limitations in the claims are to be interpreted broadly based on the language
employed in the claims and not limited to embodiments described in the present specification
or during the prosecution of the present application. The present teaching is to be
interpreted broadly based on the language employed in the claims.
[DESCRIPTION OF THE REFERENCE SIGNS]
[0167]
- 1
- straddled vehicle
- 3b
- wheel (drive wheel)
- 4
- battery
- 8
- acceleration command part
- 10
- single-cylinder engine
- 12
- cylinder
- 13
- piston
- 15
- crankshaft
- 20
- permanent magnet type motor
- 30
- rotor
- 40
- stator
- 60
- control device
- 61
- inverter
- 611 to 616
- switching part