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  <front>
    <journal-meta />
    <article-meta>
      <title-group>
        <article-title>Simulation and Analysis of Dual Unbalanced Rotor Efects on Natural Frequency in a Digital Twin Shaft Model</article-title>
      </title-group>
      <contrib-group>
        <contrib contrib-type="author">
          <string-name>Fadhel Abbas Abdulla</string-name>
          <xref ref-type="aff" rid="aff0">0</xref>
        </contrib>
        <contrib contrib-type="author">
          <string-name>Ahmed Imad Abbood</string-name>
          <xref ref-type="aff" rid="aff0">0</xref>
        </contrib>
        <aff id="aff0">
          <label>0</label>
          <institution>Department of Mechanical Engineering, Mustansiriyah University</institution>
          ,
          <addr-line>Baghdad</addr-line>
          ,
          <country country="IQ">Iraq</country>
        </aff>
      </contrib-group>
      <fpage>32</fpage>
      <lpage>37</lpage>
      <abstract>
        <p>Blades are one of the basic components of a gas turbine and its main function is to rotate the shaft associated with the generator motor. Gas turbine model MS9001E used power plants at south Baghdad station, the blades are subjected to harsh working conditions such as high vibration, temperatures and pressures, thus highlighting the importance of studying the materials used in Manufacture of blades that work under harsh operating conditions. In this research, stress, strain and deformation produced by the centrifugal force that the blade is subjected to be studied, as well as studying the natural frequencies of the blades. Three-dimensional was created through the program solidwork 2018 and then exported to the program ansys 2019 for analyzing. Two alloys of materials (GTD-111) and (IN-738) were analyzed and compared between them, and the results showed that alloy (GTD-11) is the best and is suitable for use in the manufacture of blades.</p>
      </abstract>
      <kwd-group>
        <kwd>eol&gt;Rotors</kwd>
        <kwd>Natural frequency</kwd>
        <kwd>Deformation</kwd>
        <kwd>vibrations frequency</kwd>
        <kwd>Modal analysis</kwd>
      </kwd-group>
    </article-meta>
  </front>
  <body>
    <sec id="sec-1">
      <title>1. Introduction</title>
      <p>
        den accidents. Numerous researchers have focused on
investigating the impact of cracks on the eficiency of
The dynamic rotor plays a crucial role in the behavior rotating shafts. Some have conducted analytical analyses
of rotary machines, ranging from large-scale systems to study these issues, while others have approached them
like power plant rotors and turbo-generators to smaller approximately. One key factor in minimizing undesired
systems such as tooth drills, pumps, and air compressors vibrations is efectively controlling the rotor’s geometric
[
        <xref ref-type="bibr" rid="ref3 ref4 ref5">1, 2, 3</xref>
        ]. Understanding the history of rotor dynamics is imbalance [
        <xref ref-type="bibr" rid="ref14">20, 21, 22</xref>
        ]. By employing calculations and
essential as it highlights the fundamental challenges in understanding the mass of unbalance during rotation,
developing and implementing rolling bearings for vari- it is possible to measure the vibration response of any
ous applications [
        <xref ref-type="bibr" rid="ref10 ref6 ref7 ref8 ref9">4, 5, 6, 7, 8</xref>
        ] when stability and quality system. Multiple researchers have conducted studies on
must be assured [
        <xref ref-type="bibr" rid="ref11">9</xref>
        ]. The study of dynamic behavior the impact of externally applied axial force and torque on
in rotating machinery began in the early years of the the lateral vibration of shafts. Alaa et al. [
        <xref ref-type="bibr" rid="ref15">23</xref>
        ] derived the
19th century when the industrial revolution increased equation of motion for a flexible rotating shaft subjected
the demand for analyzing rotational motion also in the to a constant compressive axial load by incorporating
robotic industry [
        <xref ref-type="bibr" rid="ref12 ref13">10, 11, 12, 13</xref>
        ]. Since the fifties, numer- gyroscopic moments consistently. In the study [
        <xref ref-type="bibr" rid="ref16">24</xref>
        ]
examous researchers have conducted studies on crack prop- ined the stability of a rotating cantilever shaft carrying
agation in shafts, and some of these findings have been a rigid disk at its free end, considering follower axial
extended to real-world rotors, providing valuable insights force and torque loads. Chen and Sheu [
        <xref ref-type="bibr" rid="ref17">25</xref>
        ] analytically
for designers [14, 15, 16]. Typically, rotors operate un- investigated the stability behavior of a rotating
Timoder cyclic pressure, making them susceptible to various shenko shaft with an intermediate attached disk under
operational issues, such as fatigue cracks. These cracks longitudinal force, providing frequency equations for
vartend to occur when the rotors’ natural frequencies and ious boundary conditions and numerically determining
critical speeds increase as the shaft length decreases and critical axial and follower forces. Chen et al. [
        <xref ref-type="bibr" rid="ref18">26</xref>
        ] The
the cross-sectional area increases [17]. It is crucial to influence of inertial forces on shafts and beams can result
identify the vibration characteristics of cracked shafts in axial stresses. Researchers have also examined the
to develop a control system that can detect operational rotation of beams around an axis perpendicular to their
errors and early-stage cracks [18, 19] and prevent sud- beam axis, where centrifugal force directly induces axial
stress in the beam. In this study [
        <xref ref-type="bibr" rid="ref19">27</xref>
        ] utilized the dynamic
IInCfYoRrmIMaEtic2s,02M4a:th9tehmaIntitcesr,naantidonEanlgiCnoeenrfienrgen.CceatoafnYiae,aJrulylyR2e9p-oArutsguosnt stifness matrix for an Euler-Bernoulli beam subjected to
1, 2024 axial force to analyze the vibration of rotating uniform
* Corresponding author. and tapered beams. In the investigation reported [
        <xref ref-type="bibr" rid="ref20 ref21">28, 29</xref>
        ]
$ fadhel975@uomustansiriyah.edu.iq (F. A. Abdulla); derived the governing equation for the linear vibration of
ahm00e0d0.a-b00b0o2o-d7@84u0o-0m6u5s9ta(Fn.sAir.iyAabhd.eudllua.)i;q0(0A0.9I-.0A00b6b-o8o7d6)3-7160 a rotating Timoshenko beam, considering the coupling
(A. I. Abbood) between extensional and flexural deformation by
lineariz© 2024 Copyright for this paper by its authors. Use permitted under Creative Commons License ing the fully geometrically nonlinear beam theory. They
Attribution 4.0 International (CC BY 4.0).
proposed a power series solution method to determine of 1200mm, while the rotors have diameters of 230mm,
the natural frequency of the rotating Timoshenko beam. as shown in Figure (1a). The bearings are positioned at
This study introduces a new phenomenon that can influ- three locations, with the midspan position being
particence the performance of rotating shafts. The change in ularly interesting for identifying the optimal position.
natural frequency is attributed to the position of rotors The system’s geometry was created using SolidWorks
and the midspan between double rotors. Unlike previous 2020 and then exported to ANSYS 2019 software. The
studies, the disks located equal spaces between fixtures rotor system geometry was discretized in the initial stage
and rotors. To accomplish this objective, the lateral de- using tetrahedral elements. The model comprises 160,022
formation and natural frequency need to be calculated, nodes and 40,196 elements, as depicted in Figure (1b).
then evaluating the impact of this distance on the
lateral natural frequency of the shaft. The paper presents a
numerical solution to evaluate the systems.
      </p>
    </sec>
    <sec id="sec-2">
      <title>2. Materials and Method</title>
      <p>
        A modal analysis was conducted on a structural steel
shaft, and commercially available rotors were used. The
material properties of the structural steel are provided
in Table 1. Finite element analysis (FEA) was chosen
as it ofers more comprehensive results compared to
experimental studies, with the added benefits of speed and
cost-efectiveness [
        <xref ref-type="bibr" rid="ref22 ref23 ref24">30, 31, 32</xref>
        ] also in term of missing data
reconstruction or imputation [33, 34]. The FEA employed
a finite element discretization approach to solve complex
structural equations by dividing the structure into
specific finite elements[
        <xref ref-type="bibr" rid="ref23 ref24">31, 32, 35, 36</xref>
        ]. The unbalanced rotors
were designed using FEA, utilizing a mesh system
composed of interconnected nodes. The model, created in
SOLIDWORKS 2020, was exported to ANSYS 2019
software. The ANSYS model then meshed, and boundary
conditions were applied. The software solved the system
equations to determine the model’s natural frequencies.
      </p>
    </sec>
    <sec id="sec-3">
      <title>3. Modelling and Analysis of</title>
    </sec>
    <sec id="sec-4">
      <title>Rotating shaft and Dual Rotors</title>
      <p>The model developed aims to simulate rotating
machinery with unbalanced rotating components. The model
consists of two main components to simplify the
system: the rotors and the shaft. The shaft has a length</p>
      <p>The geometry of the rotor is afected by the unbalanced
mass and the rotating velocity of 200 RPM in ANSYS
Modal. The boundary conditions shown in Figure (2), the
two ends of the shaft are fixed support and the position
of bearings are BEARING boundary conditions in ANSYS
Model. The geometry of the rotor and shaft are meshed
with ELEMENT 186 to adept to diferent shapes.</p>
      <p>ANSYS Modal analysis uses the following equations
to solve vibration problems:
1. Mass Matrix Equation: [ ] + [] = 0
2. In this equation: [M] is the mass matrix, which
represents the distribution of masses in the system.  is
the vector of mode shapes or modal displacements. [K]
is the stifness matrix, which represents the stifness of
the system.</p>
      <p>3. Eigenvalue Equation: [] =  [ ]
4. In this equation:  represents the eigenvalues, which
determine the natural frequencies of the system. [K] is
the stifness matrix.  is the vector of mode shapes.</p>
      <p>By solving the above equations, ANSYS Modal
analysis calculates the natural frequencies (eigenvalues) and
corresponding mode shapes (modal displacements) of the
system.</p>
    </sec>
    <sec id="sec-5">
      <title>4. Results and Discussion</title>
      <p>The outcomes derived from ANSYS 2019R3 depend on
various elements such as the system’s shape, length of the
shaft, elastic characteristics, rotor spacing, and boundary
conditions. These factors impact the inherent frequency
of the system. A higher inherent frequency signifies an
improved design by reducing vibration amplitude and
lowering the likelihood of component malfunction [37].
The modal analysis ofers a valuable understanding of
these outcomes, aiding in assessing and enhancing the
system’s performance. Figure (3) shows the mode shapes
for the first five modes for the 916mm midspan.
Deformation (11.69 mm) at a frequency (162.43Hz) 1st mode,
and deformation (12.22 mm) at a frequency (418.48Hz)
2nd mode. The following three modes show an increase
in frequency, and deformation will reach the peak at 4th
mode for the 3rd ,4th, and 5th modes; the frequency and
deformation are 569.65Hz, 35.22mm; 601.04Hz, 35.74mm;
and 648.08Hz, 29.22mm respectively.
(e) 5ℎ mode 648.08Hz</p>
    </sec>
    <sec id="sec-6">
      <title>5. Conclusions</title>
      <p>The following conclusions can be derived from the
findings of this study:</p>
      <p>1. Using midspan at the highest value increase the
value of natural frequency and reduces the efect of
whirling.</p>
      <p>2. The position of the rotors does afect much on the
rotating shaft’s natural frequency because of the
deformation in the rotating disk, which has the same dimensions.</p>
      <p>3. The second mode is afected by the position of rotors
which give high natural frequency at a high midspan
value.</p>
      <p>4. As well as the distance between two rotating discs
is higher, the system balance increases too.</p>
      <p>In future works, new optimization methods based on</p>
    </sec>
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