Dynamics study of the operating behavior of hydrodynamic coupling by experimental and numerical simulation/Hidrodinamines jungties eksploatavimo eksperimentine ir skaitmenine dinamikos analize.
Khatir, T. ; Bouchetara, M. ; Boutchicha, D. 等
1. Introduction
Clutches or couplings have the task to receive and to transmit
power from engine to the driven machine [1]. This is achieved through
the transmission of power inside the fluid coupling composed of a
centrifugal pump and a turbine [2, 3]. It is often installed as a
vibration damping element or as a shock absorber to protect the engine
and the driven machine against overloads, for example in vehicles, ships
and fixed equipment [4, 5]. Fluid couplings can also act as hydrodynamic
brakes, dissipating rotational energy as heat through frictional forces
[6]. This type of hydrodynamic transmission is based on the principle of
Fottinger [7, 8].
A fluid coupling, sometimes also known as hydraulic coupling or
Voith fluid coupling, is a nonmechanical coupling used to transfer the
power from a prime mover, an electrical motor or an internal combustion
engine, to a driven machine [9].
Simulation of fluid coupling is an important tool for analysing and
evaluation of the dynamic behavior of engine--transmission system
[10-14]. Torque transmission is possible only if the sliding conditions
are ensured [15].
Among the main advantages of hydrodynamic couplings may be
mentioned [16-20]:
* in case of overload, the engine cannot stall because of the
sliding between the input shaft and the output shaft;
* hydraulic couplers, without being equivalent to torque limiters
are safety devices that protect the engine and the driven machine;
* hydrodynamic transmissions are simple in design, easy
maintenance; insensitive to wear [21-23].
The main aim of this study is to carry out a numerical simulation
of the transient behavior of a hydrodynamic coupling operating in two
different modes, start-up and braking.
Through numerical simulation developed, one presents the evolution
of the fluid velocity in the coupler and the rotational speed of the
primary and secondary shaft, and the variation of the torque of the pump
and the turbine as function of time.
To validate the results of the developed numerical simulation
model, we realized a test bench that simulates the different operating
modes of a hydrodynamic coupling.
2. Fundamental equation of unsteady motion of a hydrodynamic
transmission
2.1. Description of the hydrodynamic coupling
[FIGURE 1 OMITTED]
The primary shaft 1 linked to an engine that causes the primary
rotor P by its rotational movement.
Turbine T member or secondary rotor which is integral to the tight
envelope e of the set containing the liquid. Both wheels, the pump P and
the turbine T, are provided with radial blades a, Fig. 1.
The torus is the common waterproof body that meets and casing P and
T and replacing the pipes. The oil filling the torus is generally more
than 90% of its total capacity to avoid the oil dilution under the
influence of heat which can generate excessive pressure on the walls.
This phenomenon has caused the explosion of several couplers [24-27].
2.2. Equations of unsteady motion of a hydrodynamic coupling
To establish the basic equations of unsteady motion of a
hydrodynamic coupling (Fig. 2), it is assumed that:
* the fluid is incompressible;
* the fluid flows along the median line, because the analysis of
the phenomena under microscopic aspects is complicated;
* the flow is along the blade;
* the space between the pump and the turbine is negligible.
[FIGURE 2 OMITTED]
The mathematical formulation of a torque converter has been
developed by Ishihara and Emori Kotwicki, and Hrovat and Tobler [28-30].
The kinetic energy of the total mass of the fluid is:
[E.sub.c] = [??] [rho] [V.sup.2]/2 AdL, (1)
where [??] is integral for full closed fluid flow; A is meridian
section of the fluid flow, which is perpendicular to the meridian plane.
So the variation of the kinetic energy according to the time is:
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (2)
where z is length of the average current line.
As V = dz/dt then the relation (2) becomes:
d[E.sub.c]/dt = [rho][??] 1/2 d [V.sup.2]/d z dz/dt (3)
The absolute velocity V is expressed as follows:
[V.sup.2] = [U.sup.2] + [C.sup.2]; U = r [omega].
The integral Eq. (3) becomes:
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (4)
with Q = Ac and [PHI] = [??] ([A.sub.2]/A) dL; [A.sub.2] is
meridian section of the fluid flow; [C.sub.2] is meridian speed at the
entering of turbine.
The moment of the pump is expressed as follows:
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII]. (5)
The moment of the turbine will be:
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII]. (6)
The hydraulic power of the pump and the turbine will be
respectively:
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII]; (7)
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII]. (8)
During the fluid circulation in the coupling, there are energy
losses EL due to the frictions in the blades, and to the shocks during
sudden change of the direction of inlet velocity at the pump and
particularly at inlet of the turbine. Energy losses EL are expressed per
unit of time as:
d[E.sub.L]/dt = 1/2 [rho]Q[([r.sup.2.sub.1] +
[r.sup.2.sub.2])[([[omega].sub.1] - [[omega].sub.2]).sup.2] +
L[C.sup.2.sub.2]], (9)
where L is total friction coefficient by full circulation.
The equation of non-steady motion of fluid is obtained by
substituting the Eqs. (4), (7)-(9) in the following relationship:
d[E.sub.c]/dt = [P.sub.1] + [P.sub.2] - d[E.sub.L]/dt. (10)
It follows:
[PHI] d[E.sub.L]/dt = 1/2 [([r.sup.2.sub.1] +
[r.sup.2.sub.2])([[omega].sub.1] - [[omega].sub.2]) + L[C.sup.2.sub.2]].
(11)
To obtain the motion equation of the pump, the inertial moment of
the pump and of all rotating mechanical parts without the presence of
oil, which is denoted J[.
The fluid act on the pump with a reaction time is expressed by Eq.
(5).
Equation of motion of the pump:
[J'.sub.1] d[[omega].sub.1]/dt = [M.sub.p] - [rho]
[A.sub.2][c.sub.2]([r.sup.2.sub.2][[omega].sub.1] -
[r.sup.2.sub.1][[omega].sub.2]). (12)
Equation of motion of the turbine:
[J'.sub.2] d[[omega].sub.2]/dt = [rho] [A.sub.2][c.sub.2]
([r.sup.2.sub.2][[omega].sub.1] - [r.sup.2.sub.1][[omega].sub.2]) -
[M.sub.T], (13)
[J'.sub.1] is inertia moment of the rotating parts of the pump
side without the presence of oil; [J'.sub.1] is inertia moment of
the rotating parts of the turbine side without the presence of oil;
a1--angular velocity of the pump wheel; [[omega].sub.2] is angular
velocity of the turbine wheel; [M.sub.P] is output torque on the pump;
[M.sub.T] is output torque on the turbine.
By neglecting the inertia moment of the fluid acting on the pump
and the turbine, we obtain:
[J'.sub.1] = [J.sub.1] and [J'.sub.2] = [J.sub.2],
where [J.sub.1] is inertia moment of the pump side with oil,
[J.sub.2] is inertia moment of the turbine side with oil.
Finally, the motion equations of the pump and the turbine will be
respectively:
[J.sub.1] d[[omega].sub.1]/dt = [M.sub.P] - [rho]
[A.sub.2][c.sub.2] ([r.sup.2.sub.2][[omega].sub.1] -
[r.sup.2.sub.1][[omega].sub.2]) (14)
[J.sub.2] d[[omega].sub.2]/dt = [rho] [A.sub.2][c.sub.2]
([r.sup.2.sub.2][[omega].sub.1] - [r.sup.2.sub.1][[omega].sub.2]) -
[M.sub.T] (15)
2.3. Resolution of the equation system
The system of fundamental equations of non-steady movement of the
hydrodynamic coupling is written as follows:
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII]. (16)
We have a system of Eq. (3) to Eq. (5) unknowns, namely:
[[omega].sub.1] is angular velocity of the wheel pumps, rad / s;
[[omega].sub.2] is angular velocity of the wheel turbines, rad / s;
[c.sub.2] is meridian velocity of the fluid, m / s; MP is output torque
of the pump, daNm; [M.sub.T] is output torque of the turbine, daNm.
It is more practical to make the system of equations in
dimensionless form. The system (16) becomes then:
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII]. (17)
x = [c.sub.2]/[r.sub.2] [[omega].sub.0] is dimensionless speed;
[[omega].sub.0] is engine angular speed; [T.sub.1] =
[M.sub.P]/[rho][A.sub.2][r.sup.3.sub.2][[omega].sup.2.sub.0] is
dimensionless moment of the pump wheel; [T.sub.2] =
[M.sub.T]/[rho][A.sub.2][r.sup.3.sub.2][[omega].sup.2.sub.0] is
dimensionless moment on the turbine wheel, [Q.sub.1] =
[J.sub.1]/[rho][A.sub.2][r.sup.3.sub.2] is dimensionless moment of
inertia of the pump side; [Q.sub.2] =
[j.sub.2]/[rho][A.sub.2][r.sup.3.sub.2] is dimensionless moment of
inertia of the turbine side; p = [PHI]/[r.sub.2] is dimensionless
parameter length.
[FIGURE 3 OMITTED]
The system (17) becomes then:
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII]. (18)
[t.sub.11] = [[omega].sub.0]t is dimensionless time.
It allows solving the system of dimensionless equations (Fig. 3).
3. Description of the test bench of a hydrodynamic clutch
The purpose of this study is to develop a numerical model for
simulating the hydraulic coupling operations that allows the analysing
of the dynamic behavior of the hydrodynamic coupling, respectively in
the starting and braking phase. To validate the elaborated numerical
simulation model, we proceed to the realization of a test bench to
measure the input and output parameters of a hydrodynamic coupling
according to defined operating modes.
[FIGURE 4 OMITTED]
On the bench, there are two shafts: the first provides the pump
torque and the second the turbine torque. Fig. 4 shows the installation
of the used test bench of a hydrodynamic coupling.
Tables 1 and 2 are shown respectively the hydraulic Parameters and
the technical characteristics of the tested hydrodynamic coupling.
4. Experimental tests
4.1. Starting tests
Mode 1. Operating steps and test conditions (Fig. 5):
* initially the engine is under normal operating conditions, the
turbine is blocked;
* clutch, pump motor, turbine is still blocked;
* unlock the turbine, the pump and the engine under normal
operating conditions.
[FIGURE 5 OMITTED]
Mode 2. Operating steps and test conditions (Fig. 6):
* initially engine under normal operating conditions the turbine is
unlocked;
* clutch, pump-motor, turbine remains unlocked (free).
[FIGURE 6 OMITTED]
[FIGURE 7 OMITTED]
Mode 3. Operating steps and test conditions (Fig. 7):
* initially engine is off and the turbine is blocked;
* let in the clutch;
* motor stopped and turbine is still blocked;
* starting the engine and unlock the turbine.
Mode 4. Operating steps and test conditions (Fig. 8):
* engine initially on the march normal, and the turbine is freed;
* clutch, turbine is still unlocked and engine at the stop;
* engine is on, the turbine is blocked and the pump running under
normal conditions.
[FIGURE 8 OMITTED]
4.2. Braking test
Operating steps and test conditions (Fig. 9):
* engine, pump, turbine during normal operation;
* block the turbine engine and pump during normal operation.
[FIGURE 9 OMITTED]
5. Analysis and discussion of results
From the Figs. 5-8, the following comments and conclusions can be
deduced:
In the modes 1 and 3, the turbine torque MT evolves into 4 phases:
linear increase, stabilization [M.sub.T] = constant, nearly linear
decreasing and until the end of the operation.
The physical interpretation of this curve profile is as follows:
* during the period of blocking, MT cross from zero to MT1, where
[M.sub.T1] is the moment on the turbine wheel and remains fixed as long
as they're blocking;
* just after the releasing, we have noticed the diminution of MT,
this is due to the absence of the resisting moment of blocking;
* in the last phase, the effect of the moments of resisting inertia
decreases and thus the moment on the wheel turbines will be equal at the
transmitted moment which stays stable regime;
* for modes 2 and 4, the curve of the moment of the turbine wheel
MT evolves in 3 phases to be known: growth in the presence of a peak,
decreasing, stabilization.
Even this can be explained as a result:
* the turbine was unlocked (free), the effect of blocking
resistance moment is zero, and in this case, the time for the turbine
wheel to increase the value of the moment of inertia due to the inertia
of the turbine and fluid movement, and later MT decreases to the normal
operating period;
* for braking, it is almost the same as the first phase of start-up
(mode 1 and 3), but the difference lies in the initial values
[[omega].sub.P], [[omega].sub.T], [M.sub.T] the physical phenomenon is
almost the same;
* in the normal operating regime, [[omega].sub.P], [[omega].sub.T],
[M.sub.T] have fixed, just after braking (blocking the turbine)
[[omega].sub.T] decreases to zero value, while [M.sub.T] increases and
stabilizes at a time equal to the braking torque.
6. Conclusion and future work
1. The developed numerical simulation model represents an efficient
tool for analysis and evaluation of the dynamical behavior of
hydrodynamic couplings; it can be used to describe the correlation
between the input and output main parameters of hydrodynamic
transmissions.
2. Due to the increasing use of hydrodynamic transmissions, the
present study focused on the analysis of unsteady behavior of
hydrodynamic couplings.
3. The numerical simulation developed in this study is based on the
elaboration of a system of differential equations describing the
unsteady behavior of the hydraulic coupling.
4. To resolve the system of nonlinear differential equations, the
method of finite differences was used.
5. The elaborated computing program allows to determine the
evolution of speed and torque of the turbine as a function of time by
knowing the input parameters of the pump or the engine.
6. The designed test bench has allowed to carry out measurements of
the speed and torque on the input and output side of the hydrodynamic
coupling as a function of time and imposed operating modes. The
experimental and numerical results are almost identical, proving that
the test bench and the numerical simulation model were successfully
realized.
7. This test bench can be used for other experimental
investigations such as the vibration or thermal behavior of hydrodynamic
couplings.
Received January 28, 2014
Accepted June 18, 2014
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T. Khatir *, M. Bouchetara **, D. Boutchicha ***
* University of Science and Technology of Oran Mohammed Boudiaf,
L.P 1505 EL-Menaour, USTO 31000 Oran, Algeria, E-mail:
[email protected]
** University of Science and Technology of Oran Mohammed Boudiaf,
L.P 1505 EL-Menaour, USTO 31000 Oran, Algeria, E-mail:
[email protected]
*** University of Science and Technology of Oran Mohammed Boudiaf,
L.P 1505 EL-Menaour, USTO 31000 Oran, Algeria, E-mail:
[email protected]
http://dx.doi.org/ 10.5755/j01.mech.20.4.6297
Table 1
Hydraulic parameters characterizing the hydrodynamic
coupling
Motor power [P.sub.m], kW 4.00
Nominal rotation speed [n.sub.m], rpm 1436
Specific velocity, [n.sub.s] 65
Oil density [rho], kg/[m.sup.3] 800
Number of blades of the pump wheel [Z.sub.p] 37
Number of blades of the turbine wheel [Z.sub.p] 40
Table 2
Technical characteristics of a hydrodynamic coupling
Material Density
[rho], kg/[m.sup.3]
Hydrodynamic Pump Aluminum alloy 2705
clutch Turbine Aluminum alloy 2705
Torus Cast iron 7500
Lid Steel 7000
Used fluid Special fluid 800
Total filling
capacity
[V.sub.t], [dm.sup.3]
Hydrodynamic Pump 2.3
clutch Turbine
Torus
Lid
Used fluid
Service
capacity
[V.sub.s], [dm.sup.3]
Hydrodynamic Pump 1.84
clutch Turbine
Torus
Lid
Used fluid