On the dynamic modelling of a planetary chain speed increaser for R.E.S.
Saulescu, Radu ; Jaliu, Codruta ; Neagoe, Mircea 等
1. INTRODUCTION
Most small hydropower plants include a gearbox to increase the
speed of the turbine shaft to the generator. The range in which the
input angular speed must be increased is 3 - 5 (Harvey, 2005; Jaliu et
al., 2008). There are two basic types of gearboxes used in hydro-plants:
parallel-shaft gearboxes and planetary gearboxes. In the first case, the
higher the transmission ratio is, the bigger the overall dimensions are.
In the second case, the input and output shafts are coaxial, reducing
the overall dimension; the gearboxes are relatively light and compact
but the cost of the transmission increases. New innovative solutions of
planetary speed increasers were proposed by the authors in the previous
papers (Diaconescu, 2005; Jaliu et al., 2008; Neagoe et al., 2008), with
the aim to compensate the existent gearboxes disadvantages. This paper
presents the dynamic modelling of a proposed planetary chain increaser
for renewable energy systems (RES); the dynamics of the increaser
represents the starting point for the control system design. The authors
will accomplish the design, manufacturing and testing of the speed
increaser for stand-alone hydropower stations, in the frame of a
research project.
2. STRUCTURAL AND KINEMATICAL ASPECTS
A first step in dynamical modelling is done by defining the
structural and kinematical aspects of the transmission.
[FIGURE 1 OMITTED]
Thus, the planetary transmission consists of: a fixed sun gear
(3,3'), a satellite gear (2), a semi-coupling with pins (1) and a
carrier (H); it has two exterior links (L=2): 1-input, H output.As a
consequence of this aspect the obtained degree-of freedom equals 1, thus
this planetary unit is being defined by: M=1, a single external
independent motion: [[phi].sub.13], [[omega].sub.13],
[[epsilon].sub.13];
a force transmission function [T.sub.1] = [T.sub.1]
([[phi].sub.13], [T.sub.H]); L-M=1 a movement transmission function:
[[phi].sub.H3] = [[phi].sub.H3] ([[phi].sub.13]), [[omega].sub.H3]
= [[omega].sub.H3] ([[omega].sub.13]), [[epsilon].sub.H3] =
[[epsilon].sub.H3] ([[epsilon].sub.13]);
an external independent force [T.sub.H].
The force transmission function is being determined by means of the
internal kinematical ratio:
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (1)
where: [i.sup.z.sub.xy] is the transmission ratio from element x to
element y, while element z is considered blocked; [[omega].sub.xy]
represents the relative speed between elements x and y;
The transmission ratio of the planetary transmission is given by
relation (2), while the multiplication ratio, as the reverse of the
previous one, by relation (3):
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (2)
i = 1/[i.sup.3.sub.1H] = 1 [1 - [i.sub.0] (3)
The kinematical modelling is solved using relation (2):
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (4)
3. DIYNAMIC ASPECTS
The interior efficiency ( [[eta].sub.0] ) of the planetary
transmission must be determined, in order to obtain the dynamic
modelling:
[[eta].sub.0] = [[eta].sup.H.sub.13] = [[eta].sup.H.sub.12] x
[[eta].sup.H.sub.23] (5)
The efficiency of the transmission is:
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (6)
in which the exponent w is being calculated with:
[FIGURE 2 OMITTED]
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII]
From (6) the force transmission function results as:
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (7)
The kinematical and static functions for the planetary chain
transmissions are given in relations (4) and (7). An aggregate composed
from a turbine, the analyzed planetary speed increaser and a generator
is considered for the dynamic simulations.
4. PREMISES FOR DYNAMIC MODELLING
The dynamic modelling relies on the following premises:
* In the dynamic modelling, the inertial effects due to the
satellite gears rotation are neglected (their masses being considered in
the axial inertial moment of the afferent carrier shaft), while the
inertial effects of the mobile central elements are considered
integrated into the shafts that materialize the external links of the
planetary gears; under this premise, the static correlations between the
external torques of each planetary gear are valid, while the dynamic
correlations interfere only for the shafts that materialize the
planetary gears external links. The mechanical inertia momentums of the
two shafts are (see Fig. 1 - Saulescu et al, 2009):
[J.sub.1] = 0,03; [J.sub.H] = 0,02 [[Kgm.sup.2]] (8)
* the rubbing effect is considered by means of the efficiency
[eta];
* The real machine (water turbine--speed increaser generator) is
replaced on the experimental stand by a machine of type: DC
Motor--increaser--brake, in which the motor and the brake have the
following mechanical characteristics:
[T.sub.m] =-0,1237[[omega].sub.m] +10; [T.sub.b] = -[[omega].sub.b]
[Nm] (9)
* In the numerical simulations, the following values for the
kinematical and dynamic parameters are considered:
--the satellite and sun gears teeth numbers are [z.sub.2] = 30,
[z.sub.3] = 24,
- the efficiencies of the pin coupling and chain transmission are
[[eta].sub.12] = 0.995, [[eta].sub.23] = 0,92.
5. CONCLUSIONS
The theoretical aspects from which was deducted the analytical
kinematical and static calculus were presented in the paper; the
mechanical momentums of inertia and the motor's mechanical
characteristics (belonging to the turbine) and brake's mechanical
characteristics (belonging to the generator) were considered in the
dynamic modelling. As the dynamic modelling is being accomplished in
order to compare the theoretical results with the experimental ones,
obtained on the stand, the turbine is being replaced with a DC engine,
and the generator is being replaced with a brake. The considered inertia
mechanical momentums (see Fig. 1,a and 2) have as an input element 1,
the engines rotor, the entering shaft with it's appropriate rolls,
while for the output element H, the exit shaft, brake's rotor and
the inertial effect of the satellite considered as the concentrated
mass.
The presented parameters are being used in order to design the
dynamic model, (Saulescu et al., 2009).
The dynamical model is conceived on a DC motor type
machine--planetary chain speed increaser--brake (see Fig.2), on a
representative case, in which the multiplication ratio is the one
recommended in the specialized literature (Harvey, 2005; Von Schon,
2007; Jaliu et al., 2008; Amer, 2005) for small hydro.
The dynamical modelling is done to be used for pushing forward the
researches on two directions:
* The theoretic direction, meaning: attaining a controlling program
for the system;
* The experimental direction, meaning: obtaining the main product
(the planetary chain increaser) and implementing it on a system of type:
turbine - transmission - generator, for a particular case.
6. ACKNOWLEDGEMENT
The authors will accomplish the design, manufacturing and testing
of the speed increaser for stand-alone hydropower stations in the
framework of the research project "Innovative mechatronic systems
for micro hydros, meant to the efficient exploitation of hydrological potential from off-grid sites", ID_140. The preparation and
publishing of this paper were possible with the financial support of
this research project.
7. REFERENCES
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chain speed increaser for RES, Proceedings of 20th DAAAM International
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