Analysis of some extreme situations in exploitation of complex rotary systems/Dalies ekstremaliu situaciju, susidaranciu sudetingu rotoriniu sistemu eksploatacijos metu, analize.
Jonusas, R. ; Juzenas, E. ; Juzenas, K. 等
1. Introduction
Complex rotary systems (CRS), such as "flexible rotor on
sliding bearings connected through gearbox", are used in many
technological systems of industry and energetics. Their reliability is
crucial for quality and productivity of various technological processes,
as well as safety. An axial compressor (Fig. 1) from a chemical industry
plant [1,2] can be presented as a typical example of such system.
[FIGURE 1 OMITTED]
Present complex rotary systems have longer, more flexible rotors
and operate in high speeds, having very small allowed clearances
(especially in case of labyrinth or dry sealing). Exploitation speed
higher than the first critical and lower (in most cases) than the second
critical speed is the typical feature of such rotary systems. Therefore
some extreme situations can appear during exploitation of CRS in cases
of specific conditions: high amplitude components of subharmonic
vibrations may by generated, rubbing of rotor and housing elements
caused by increased eccentricity of shafts may appear, etc. All those
situations negatively affect reliability of complex rotary systems
exploitation. In the most cases, such situations are caused by several
defects [2-5].
Similarly rubbing of rotors has to be considered as the secondary
phenomenon, resulting from other defects. However it has specific
features and is highly dangerous. That makes this phenomenon very
important object for research together with other typical sources of
subharmonic and superharmonic vibrations.
2. Significance of the subharmonic vibrations
Influence of subharmonic vibrations on dynamics of complex rotary
systems has been analysed in various aspects [2-5], however this area
still is under intensive research [6-10]. It is established [2-4] that
the influence of subharmonic vibrations may be described as
"positive". Those vibrations cause reduction of amplitudes of
the resonance vibrations during transitional processes of rotary systems
(running up and running down when the first resonance frequency is
passed). However in the most cases this influence is
"negative", especially if high amplitude subharmonic
vibrations may be generated for longer periods of time. Those vibrations
can cause rubbing, fatigue and cracking of rotors elements. In this case
reliability of such rotary system would be reduced significantly and
fracture could lead to serious breakdowns.
Therefore two opposite trends are faced. On one hand, the situation
of intensive subharmonic vibrations of significant amplitudes leads to
reducing of amplitude of the first resonance vibrations. This phenomenon
can improve dynamical situation of a vibrating rotor in specific period
of time. On another hand, significant subharmonic vibrations (many
subharmonic components of considerable amplitudes) can lead to an
intensive fatigue of rotary system which (under additional influence of
the first resonance vibrations) may cause cracking of the rotor and
breakage of its elements. In the most practical cases, reduction of the
second tendency is more important. Therefore sources of generation of
high amplitudes subharmonic vibrations should be eliminated or reduced.
There are known various sources of subharmonic vibrations the
frequencies of which are lower (1/2X, 1/3X, 1/4X) than the frequency of
the first form vibrations (considering rotor as a flexible element). In
the most cases [2, 4, 11] those vibrations are caused by:
1) variable rigidity of rotor elements in different directions of
their cross-sections;
2) unsatisfactorily provided mounting of rotors on sliding bearings
(when rotors are eccentric in the respect of bearing axes);
3) trends of gradual degradation of mounting quality during
exploitation of a CRS;
4) significant thermal deformations of machines bodies what can
cause robbing of rotors and body elements in different directions;
5) peculiarities of technological processes (e.g. pulsation of gas
flows, etc.).
One of the most important causes is the first one, because it is
determined by inappropriate design or manufacturing quality of a rotor.
Therefore this source of vibrations can appear at the very beginning of
machines exploitation and can not be controlled technologically. The
rest of causes of subharmonic vibrations develop gradually during
exploitation of a CRS and their influence may be controlled in a certain
level.
Although it is practically impossible to eliminate all subharmonic
vibrations, conditions of machines elements mounting and adjustment
should ensure that amplitudes of those vibrations would be as low as
possible.
In the most cases, subharmonic resonances of frequencies equal to
one half of frequency of the rotor first form vibrations are registered.
However other significant amplitude subharmonic vibrations can also
appear in certain cases [2,4].
3. Object of the research
Dynamical characteristics of chemical plant compressor GTT3 (Fig.
1) are analysed. Rotor of the turbine-axial compressor (TAC) of this
machine is mounted on hydrodynamic bearings. The specific feature of
this turbine design and exploitation is that measurements of machines
vibrations are practically feasible only on rotor supports 11 and 12.
Characteristics of the machines rotor: working speed is approximately
(it is slightly changing due to technological needs) 5040 r/min (84 Hz),
the first critical speed is 3276 r/min (54.6 Hz), mass of the rotor is
2500 kg. The general view of TAC rotor in opened body is presented in
Fig. 2. This rotor may be formally divided into two zones of gas turbine
and axial compressor. Rigidity of the rotors elements is the same in
different directions.
[FIGURE 2 OMITTED]
Generally, vibrations of the compressor are not high and correspond
to norms of the ISO 10816-1, when its assemblage is made appropriately
and conditions of exploitation are acceptable. Influence of various
components of vibrations is insignificant. However there are specific
problems of experimental research of such machines, related with precise
determination of vibration sources. Those difficulties are related with
the variety of defects what could possibly appear during exploitation:
defects of bearings, oil supply systems, sealants, etc. Different parts
of this complex machine (Fig. 1) are connected through gear reducer
(rigid and semirigid couplings are used). Therefore there may be
additional components of vibrations caused by defects of the reducer or
even other parts of the machine (compressor or electric motor). Thus it
is quite complicated to achieve the main task of condition
monitoring--to determinate causes of increased vibrations and predict
reliability of such machine.
Analytical dynamical model of this machine has been composed and
numerical modelling of machines dynamics, applying the methods of finite
elements has been made aiming to model dynamical situations in the
presence of various defects. Such models allow modelling of defects
development and helps in foreseeing of machines reliability [2,6,12,13].
4. Modelling of rotor dynamics
Rubbing of rotor to the machine body is one of the common defects
of such machines. Well known scientists (A. Muszynska, R.F. Benlty, F.
Chu and W. Lu, T.H. Patel and A.K. Darpe [2, 6-8], etc.) have made
significant efforts and reached important results in modelling of rub
phenomena. In the most cases partial or constant rub is modelled by
introducing non linear forces of excitation that are generated by
impacts of rotor to other elements of the machine. Therefore stiffness
of a rotor and tangential forces of friction between the rotor and
elements of machine body are changing. Radial force of rubbing can be
expressed [6-8]
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (1)
[F.sub.t] = [mu][F.sub.r] (2)
here Fr is radial forces of rubbing (impacting), Ft is tangential
force (forces of friction), e is radial displacement of the rotor, o is
the gap between the rotor and other elements, [k.sub.s] is stiffness of
machines body and [mu] is coefficient of friction. Values of those
forces are included into the right side of generalised dynamical Eq.
(3). Certain values of tangential and radial forces are placed for those
rotor elements which could have impacts with certain elements of machine
body. Therefore changes of rotor elements stiffness are modelled during
its rotation (this corresponds to the appearance of some virtual
temporal supports of the rotor while it is rubbing).
The rotor of centrifugal compressor and the adjacent gear shaft of
the reducer (Fig. 1) have been divided into 18 elements and analysed as
a system of flexible rotors on four permanent supports. Each element has
4 degrees of freedom. The general equation characterizing forced
vibrations of the modelled rotor is described in earlier woks [1,13]
(M + M ')U + ([omega]G + C)[??] + KU = F (3)
here M is the matrix of rotor masses; M' is the matrix of
masses characterizing rotation of the rotor cross-sections around the
axes of a coordinate system; G is gyroscopic matrix; C is damping
matrix; K is stiffness matrix; U is the matrix of rotor elements
displacements; F is the matrix of forces affecting the rotor (forces of
excitation); [omega] is angular velocity of the rotor. M matrix
represents the masses of beam elements and matrix M' allows
evaluating the rotation of their cross-sections. The structure of matrix
F depends on the type of exciting forces [7, 13] and includes Fr and Ft
elements in the case of rub analysis. Elements of F are functions of
time. Solution of the dynamical equation is obtained applying small
steps of time in order to avoid divergence of points where calculated
variables are discontinuous.
Such model allows formation of machines amplitude --frequency
characteristics (Fig. 3) the changes of which correspond to changes of
the machines conditions of operation (appearance of certain defects of
chosen rotors elements). Results of the modelling bring valuable
information concerning vibrations of internal elements of the rotor what
complements experimental data of vibrations of rotor supports.
However, the comparison of obtained results with experimental data
(Figs. 4 and 6) shows insufficient coincidence of those results, though
reliability of the modelling method is proved [7,8] with some simplified
experimental rotary systems.
[FIGURE 3 OMITTED]
Results of the modelling and their adequacy to exploitation
conditions of a real rotary system strongly depend on the validity of
initial parameters of the numerical model and their adequacy to physical
parameters of a machine. The possibility of alternations of various
parameters and presence of various (more or less significant) defects
makes it really complicated task to ensure this adequacy.
Therefore a comprehensive experimental analysis of such real CRS
and its exploitation conditions is needed. The most significant defects
and presumptive locations of those defects should be evaluated as well
as real physical parameters of machine elements (e.g. location and
direction of possible rubbing, type of contact, etc.).
5. Experimental research of rotor to stator rubbing
Tendencies of degradation of the compressor rotor conditions at
exploitation show up in certain duration of time. Specific components of
vibrations appear and rise as well as general level of vibrations,
becoming significant to machines reliability. Fig. 4 presents spectrum
of turbine rotor 11th support (Fig. 1) vibrations.
The method of vibrations measurements applying proximity sensors
and analysing orbits of the rotor elements is used in many cases of
diagnostics [2, 5, 7]. How ever, in some practical cases there no
possibilities to use this methods and vibration are measured applying
seismic sensors. This method does not require specific installations,
but has some specific limitations.
[FIGURE 4 OMITTED]
Experimental results present dynamical situation of the CRS when
duration of the machine exploitation is similar to its typical
interservice period. The second type of subharmonic vibrations
(component of 27.3 Hz) can be seen as well as significant components of
rotors rotation frequency 84 and 110 Hz. Rubbing of labyrinth sealing
caused by thermal deformations of machine body is the possibly cause of
the last component of vibrations. In this case, increased component of
the rotation frequency is also caused by rubbing.
Spectrum of the machines 11th support vibrations after the
breakdown of several turbine blades (as a possible result of rubbing) is
presented in Fig. 5. Abnormally increased component of rotor rotation
frequency is caused by significant unbalance of the broken turbine.
Exploitation of the CRS is impossible in such conditions.
[FIGURE 5 OMITTED]
Such emergency situation could be foreseen analysing subharmonic
vibrations of the machine, because it had been forming gradually in
certain duration of time. Presumptively this situation was preceded by
impacting of the CRS rotor blades to machines body that should be
noticeable on the spectrum of vibrations as some increased subharmonic
components. Accordingly rotor to stator rubbing was preceded by
increased eccentricity of the rotor in bearings.
Fig. 6 presents spectrum of the 11th support vibrations in the case
of rotor and stator blades partial rubbing. Very complex spectrum with
multiple components of frequency of rotation as well as natural
frequency (27.3, 54.6, 218 Hz, etc. and 42, 84, 252 Hz, etc.) can be
noticed. There are also other subharmonic and super-harmonic, as well as
chaotic components. Exploitation conditions of the CRS are unacceptable.
Results of such machine failures (traces of rubbing) are presented in
Fig. 7.
[FIGURE 6 OMITTED]
[FIGURE 7 OMITTED]
Identification of the primary defects of the rotary system is very
important aim of diagnostics, because, as it was mentioned, rubbing of
rotors has to be considered as the secondary phenomenon, resulting from
other defects. In this case, rubbing was caused by the poor quality of
the machine assemblage. However those primary defects were relatively
insignificant and were not detected during condition monitoring of the
machine.
Such experimental research of the rubbing cases allows
determination of rotor elements that can be contacting with other
elements of the machine and are affected by additional forces. This
research also showed that rubbing appeared in the both--radial and axial
direction that should be evaluated in further modelling of the machines
dynamics. Only those complicated adaptations of the numerical model can
lead to satisfactory adequacy of modelled results and real conditions of
machines exploitation, helping determine its defects and foresee the
reliability.
6. Conclusions
Certain actions should be initiated in order to avoid extreme
situation of rotary system exploitation and in order to increase
reliability of a CRS.
1. To determinate and eliminate possible causes of generation of
subharmonic vibrations of significant amplitudes. Numerical modelling of
machines dynamical situations can be applied, however it is quite
complicated because of complexity of the problem and thorough
understanding of machines properties is needed.
2. To provide comprehensive analysis of CRS structure and elements
as well as conditions of its exploitation, determining possible
locations and elements of rotor to stator rubbing, type (direction,
duration, etc.) of contact and generation of additional forces.
Improved knowledge of machines dynamics should allow adapting of
dynamical model and evaluation of real conditions of machine
exploitation.
Received November 18, 2009 Accepted February 10, 2010
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R. Jonusas *, E. Juzenas **, K. Juzenas ***
* Kaunas University of Technology, Kcstuao 27, 44312 Kaunas,
Lithuania, E-mail: remigijus.jonusas@ktu.lt
** Kaunas University of Technology, Kcstuao 27, 44312 Kaunas,
Lithuania, E-mail: ejuzenas@ktu.lt
*** Kaunas University of Technology, Kcstucio 27, 44312 Kaunas,
Lithuania, E-mail: kjuzenas@ktu.lt