3. Results and Discussion
The results of solving the equations of motion (17) and (18) and calculating the mixing and whipping force power (19), as graphs of dependencies φ=φ(t), , and at different parameters of the system, are shown in Figures 2–25.
If the engine power (torque a) is insufficient for the rotary motion of the crank, then the crank will perform a damped oscillation process. The crank, under the action of torque a, initially rotates upwards by some angle and then falls downwards, before reaching the neutral equilibrium position under the action of torque it rises again, etc., until the oscillations are completely damped out.
The greater the
a engine torque, the greater the initial maximum crank angle (
Figure 2). The crank deflection angle
φ tends to a limit constant value
φ1 as time elapses after completing the oscillating process. The greater the
a engine torque, the greater the value of the crank angle
. This means that the crank makes damped oscillations not around the neutral equilibrium position, but around a certain value
of angle
φ. This is caused by the fact that at the rotational speed of the crank
its angle of rotation is
. With constant magnitude of
and coefficient
the limiting angle of rotation of the crank
~
(where
). Considering that the maximum crank angle is 1.57
rad, that the larger
a the engine torque, the larger the limiting crank angle
φl and the oscillation period.
The rotational speed of the crank
also makes damped oscillations around the zero value with initial and subsequent amplitudes, the less, the less the corresponding torque value with decreased period (
Figure 3).
Dependency graphs
P=
P(
φ) and
in
Figure 4 and
Figure 5 show that during the upward rotation of the crank, the pressure force on the piston from above increases, and, accordingly, the power of the mixing-whipping force, and the value of
P reaches its maximum in further increasing the crank angle, it decreases (
Figure 4). In this case, the rate of increase of the rotational speed of the excitation source shaft will be greatly attenuated and the motor shaft rotational speed will decrease by the end of the cycle (
Figure 5). From the relations (19):
~
. The general character of dependence
P=
P(
φ) (
Figure 4) is determined by the relation
~
, but the amplitude and periodicity of the function
are influenced by the value
, to be more precise, by the value
a. Since
and
(
Figure 3), then
(
Figure 2). The smaller is the value of the
a engine torque, the smaller is the amplitude and period of oscillation of the mixing-whipping force power
P depending on the angle of rotation φ of the crank according to the graphical
Figure 4.
Dependence P=P(φ) for different values of a.
Figure 4.
Dependence P=P(φ) for different values of a.
Figure 5.
Dependence for different values of a.
Figure 5.
Dependence for different values of a.
relationships
φ=
φ(
t) and
in
Figure 2 and
Figure 3. Maximum magnitudes of the values
φ and
in the graphical dependencies
φ(
t) and
(
Figure 2 and
Figure 3) determine the right boundaries of the dependencies
P=
P(
φ) and
(
Figure 4 and
Figure 5), the the minimum values
φl and
(
) (
Figure 2 and
Figure 3) the left boundaries of the power graphical dependencies.
Thus, the graphs in Figures 2-5 show the results of the action of the power parameters of the excitation source on the kinematic parameters of the driving member of the device and on the energy characteristic of the dynamics of the operating member.
In Figures 6 and 7 lines 1, 2 and 3, which are oscillatory characteristics of the librational mode of engine shaft motion, depend on the piston mass. The values of the mass of the piston m are taken in relation to the rotating torque of the motor a for the effect of an oscillationally and aperiodically damped mode of crank movement. As the piston mass increases, the amplitude of oscillations of the angle , and the period of its damped oscillations decrease. After a lapse of time, the lines practically straighten out and the angle of rotation
tends to the limit values. The limiting value of the rotation angle
~
(where
), in turn
~
. As the mass of the piston increases, this value
of the angle
φ decreases (
Figure 6).
The vibrational characteristics of the motor shaft rotation depend on the parameters of the device members. At relatively small piston masses, the engine shaft performs a rotational motion. In
Figure 7, at sufficiently large piston masses, the shaft of the force source makes a damped oscillation of the engine shaft speed
. As the piston mass increases, the initial and subsequent amplitudes and period of oscillation
decrease, the line around which the oscillation process occurs is defined by the zero magnitude value
. The greater the magnitude of the force moment resulting from the piston gravity (or piston mass) directed opposite to the
a engine torque, the smaller the maximum magnitudes of the oscillations
and
, the smaller the repeatability of their oscillations.
It follows from formula (4) that the power of the mixing and whipping force is~ .
Then, in turn, the limit value of the excitation source shaft rotation angle based on equation (17) or (18) is:
~
. At
(
– engine shaft rotational speed limit value) limit magnitude value is
~
taking into account
~
. The limit values of the rotation angle corresponding to the power value
coincide with the values of this angle in the dependencies
φ=
φ(
t) in
Figure 6. Dependency graphs
and
in
Figure 8 and
Figure 9 show that the larger the mass of the piston, the smaller the maximum power values of the mixing and whipping forces
. The decrease of the maximum value of
P with increasing mass
m is accompanied by a shift of the corresponding magnitudes of the values
and
to the beginning of the abscissa. The graphs in
Figure 9 show that, with approaching to the end of the oscillating damping process, the technological process of whipping intensifies, which is demonstrated by a sharp increase in the force of mixing and whipping and its power and at some of their values and a sharp drop in their values. At
:
(
Figure 9). The rightmost limits of the graphs
P=
P(
φ) and
are limited by the maximum values of
φ and
. The leftmost limits of the graphs
P=
P(
φ) and
are defined by the minimum values of
φ and
.
The device parameters, including the crank length, influence the kinematic oscillation parameters of the engine shaft motion (
Figure 10 and
Figure 11). After a lapse of time, the rotation angle of the driven engine shaft oscillates around the values to which it tends to oscillate, with an amplitude and period of oscillation smaller the longer the length of the driving member. As it is known that the limiting value of the rotation angle
φ:
~
while
~
.
From the formula (4), we obtain
~
. From this dependence the first thing noticed is the proportionality
~
. Despite this dependence, based on the graphical relationships in
Figure 12 and
Figure 13, the predominant relationship is
~
, i.e., the value
is proportional to the minus
n-th degree of
, the value
is proportional to the minus
m-th degree of
, the total should be
n+
m>3.
On the other hand, the limit values of the excitation source shaft angle
~
for different values of
r, to which the value of
φ at the end of the oscillating damping process will tend, are the same in
Figure 10 and
Figure 12. The rightmost limits of the curves
P=
P(
φ) along the axis
φ at various values of
r in
Figure 12 are determined by the maximum values of
φ in the graphical patterns
φ=
φ(
t) in
Figure 10. The curves
P=
P(
φ) end at those points that correspond to the limit values
~
of the rotation angle
. Likewise, the right borders of the curves
in
Figure 13 are determined by the maximum values of rotational speed
, the left borders - by the minimum values
in
Figure 11. The sections
P=
P(
φ) in
Figure 12, where there is a "decrease" of
φ along the abscissa axis, correspond to the sections of the dependences
φ=
φ(
t) in
Figure 10 after the maximum values of
φmax.
The limit value of the shaft angle of a nonideal engine is
~
. The value is
~
. Therefore, the lines
φ(
t), that correspond to the values of
ρ are positioned so densely (
Figure 14), that at the end of the oscillating and aperiodic damped oscillation the lines
φ(
t) merge into a single line and
. Dense placement of lines of dependence of
at various values of fluid density
ρ is also observed in
Figure 15. It follows from formula (19) that
~
. The general character of the dependence
P=
P(
φ) in
Figure 16 is determined by the graph of the periodic function
, its amplitude is affected by
. Regardless of the fact that there are dependencies
and
, the density of the fluid
ρ slightly affects the oscillation period of
P=
P(
φ). This effect has been well observed in the graphical relationships
φ=
φ(
t) and
in
Figure 14 and
Figure 15.
It is obvious from graphical dependences
P=
P(
φ) and
in
Figure 16 and
Figure 17, that the more density of fluid, the more force and its power will be required for implementation of technological processes of mixing and whipping. In contrast to similar graphical dependences
P=
P(
φ) and
, the values of abscissas
φ and
, corresponding to the maximum values of power, with increasing density of fluid remain almost unchanged. Approximately the same for all curves
φ=
φ(
t) and
at various values of density of fluid in
Figure 14 and
Figure 15 maximum values
φmax=1.25
rad and
determine the rightmost limits of graphical dependences
P=
P(
φ) and
in
Figure 16 and
Figure 17, the limit value of
rad and value
(
Figure 14 and
Figure 15) of the endpoints graphs.
The effect of the number of
piston holes on
the dependencies is
graphically presented in
Figure 18 and
Figure 19. The greater the number of holes
, the less the resistance to the movement of the piston and, accordingly, the less the stirring-beating force (19.1) and the initial maximum angle of deflection of the motor shaft. At the rotational speed of the crank
its angle of rotation
(where
), in turn the value
depends on
according to the formula (16.2). The limit values of
, to which the angle
φ tends during the damped oscillatory process are different from zero (
Figure 18).
At the force source shaft angle of : engine shaft rotational speed is.
As seen from Fig. 20, the greater the number of holes
, the less the maximum power of the upward lifting force of the piston will be required. This is obvious from the dependence of the power of the stirring-beating force on the number of holes
n2 of the piston (19.2). The maximum deflection angles of
φ in
Figure 18 define the right limits of the dependence
P=
P(
φ) at various values of
, and the limit values of
the left end limits. The value
affects the rotation angle
φ in the relation of
~
, since
Figure 20.
Dependence P=P(φ) at m=25 kg and various values of .
Figure 20.
Dependence P=P(φ) at m=25 kg and various values of .
and
, and therefore the periodicity of the function
. The larger
, the larger is the period of the function
(
Figure 20).
Figure 21.
Dependence at m=25 kg and various values of .
Figure 21.
Dependence at m=25 kg and various values of .
The radius of the holes on the piston
has little effect on the dependences
φ=
φ(
t) and
(
Figure 22 and
Figure 23). Therefore, the
values are taken to obtain more visual graphs. These graphical dependences have almost the same period of oscillation, the initial and subsequent amplitudes are larger. The angle of rotation
φ over time tends to
the limits, which are determined by the relation which are determined by the relation, where . Obviously, at (Figure 23).
Figure 23.
Dependence at m=30 kg and various values of .
Figure 23.
Dependence at m=30 kg and various values of .
When the piston hole expands, less power of the mixing-whipping force is utilized, because the resistance of the fluid to the piston motion will be reduced (
Figure 24 and
Figure 25). The higher the amplitudes of oscillations of
(
Figure 22), the wider the right boundary and larger the left final boundary of the dependence
P=
P(
φ) and larger the period of oscillations (
Figure 24). The appearance of the negative parts of the dependence
P=
P(
φ)
Figure 24.
Dependence P=P(φ) at m=30 kg and various values of .
Figure 24.
Dependence P=P(φ) at m=30 kg and various values of .
and
is associated with the decrease of the value of
after the initial maximum (
Figure 22) and the negative part of the dependence
(
Figure 23). Obviously, the right boundary of the dependence
(
Figure 25) is determined by the maximum value of
(
Figure 23).
Figure 25.
Dependence at m=30 kg and various values of
Figure 25.
Dependence at m=30 kg and various values of