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Davidclaude Gollapudi, P.Veera Raju / International Journal of Engineering Research and
                   Applications (IJERA) ISSN: 2248-9622 www.ijera.com
                       Vol. 3, Issue 2, March -April 2013, pp.700-710

    Design And Dynamic Analysis Of Viscoelastic Structures For
                        Propellar Shaft
DAVIDCLAUDE GOLLAPUDI1                                   P.Veera Raju2 Associate professor at
                  Dept of Mechanical Engineering         G.I.E.T in the Dept of Mechanical
                   Pursuing M.Tech in G.I.E.T              Engineering, pursuing Ph.D in
                      Rajahmundry                             (JNTUK) KAKINADA


ABSTRACT
         High-technology structures often have           be analyzed by using Finite Element Analysis
stringent requirements for structural dynamics.
Suppressing vibrations is crucial to their               Keywords: laminated composite materials, damping
performance. Passive damping is used to suppress         factor, natural frequency, deflection using finite
vibrations by reducing peak resonant response.           element analysis.
Viscoelastic damping materials add passive
damping to structures by dissipating vibration           INTRODUCTION
strain energy in the form of heat energy. The            PROPULSION SHAFT:
incorporation of damping materials in advanced           The torque transmission capability of the propeller
composite materials offers the possibility of highly     shaft for ship should be larger than 3,500 Nm and
damped, light-weight structural components that          fundamental natural bending frequency of the
are vibration-resistant. The effect of damping on        propeller shaft should be higher than 6,500 rpm to
the performance of isotropic (like Steel) and            avoid whirling vibration. The outer diameter of the
orthotropic (like Carbon Epoxy & E-Glass Epoxy)          propeller shaft should not exceed 100 mm due to
structures are analysed by using Finite Element          space limitations. The propeller shaft of transmission
Analysis. Damping factors, fundamental natural           system is shown in figure for following specified
frequencies are increased for Steel Shaft, Carbon        design requirements as shown in Table. Due to space
Epoxy Shaft and E- Glass Epoxy Shaft                     limitations the outer diameter of the shaft is restricted
respectively, while embedding the rubber into the        to 90.24 mm. The one-piece hollow composite drive
structure. The deflection value is decreased for         shaft should satisfy three design specifications, such
same Shaft respectively, when rubber is embedded         as static torque transmission capability, torsional
into the structure. The effect of damping on the         buckling capacity and the fundamental natural
performance of isotropic (steel) and orthotropic         bending frequency. For given specification, the
(Carbon Epoxy & E-Glass Epoxy) structures is to          damping factor for Steel, carbon Epoxy and E-Glass
                                                         Epoxy are to be calculated and compared with and
                                                         without damping material (Rubber).

                         Table Problem Specification
      Sl. No.          Parameter              Notation            Units               Value
      1.              Torque                  T                   N-m                 3500
      2.              Max Speed               N                   RPM                 6500
      3.              Length                  L                   m                   1.250




                                                                                                   700 | P a g e
Davidclaude Gollapudi, P.Veera Raju / International Journal of Engineering Research and
                   Applications (IJERA) ISSN: 2248-9622 www.ijera.com
                       Vol. 3, Issue 2, March -April 2013, pp.700-710




         Pictorial representation of shaft transmission system.

Material Properties




COMPOSITE MATERIALS
          Composite materials are those containing more than one bonded material, each with different material
properties. The major advantages of composite materials are that they have a high ratio of stiffness to weight
and strength to weight. A principal advantage of composite materials lies in the ability of the designer to tailor
the material properties to the application.
       The matrix material may be a plastic or rubber polymer, a metal or a ceramic. The most common form in
which fiber reinforced composites are used in structural applications is called a laminate. It is obtained by
stacking a number of thin layers of fibers and matrix consolidating them to the desired thickness. Fiber
orientation in each layer as well as the stacking sequence of various layers can be controlled to generate a wide
range of physical and mechanical properties for the composite laminate.




                                                                                                    701 | P a g e
Davidclaude Gollapudi, P.Veera Raju / International Journal of Engineering Research and
                   Applications (IJERA) ISSN: 2248-9622 www.ijera.com
                       Vol. 3, Issue 2, March -April 2013, pp.700-710

ADVANTAGES OF COMPOSITES
High strength to weight ratio, High stiffness, High impact resistance, Better fatigue resistance, Improved
corrosion resistance, Good thermal conductivity
VISCOELASTIC MATERIAL
        A Viscoelastic material sometimes is called material with memory. This implies that a Viscoelastic
material's behavior depends not only on the current loading conditions, but also on the loading history. They are
characterized by possessing both viscous and elastic behavior. A purely elastic material is one in which all the
energy stored in the sample during loading is returned when the load is removed. As a result, the stress and
strain curves for elastic materials move completely in phase. For elastic materials, Hooke’s Law applies, where
the stress is proportional to the strain, and the modulus is defined at the ratio of stress to strain.




FEM

       The Basic concept in FEA is that the body or structure may be divided into smaller elements of finite
dimensions called “Finite Elements”. The original body or the structure is then considered as an assemblage of
these elements connected at a finite number of joints called “Nodes” or “Nodal Points”. Simple functions are
chosen to approximate the displacements over each finite element. Such assumed functions are called “shape
functions”. This will represent the displacement with in the element in terms of the displacement at the nodes of
the element

                                      7.1 table Specification for Steel Shaft



          Sl. No.                             Parameters                                  Values

             1                             Outer Diameter                               0.09024 m

             2                                Thickness                                    2.1 e -3




      Deflection of Steel Shaft without Rubber

. STEEL SHAFT WITH DAMPING MATERIAL



                                                                                                      702 | P a g e
Davidclaude Gollapudi, P.Veera Raju / International Journal of Engineering Research and
                   Applications (IJERA) ISSN: 2248-9622 www.ijera.com
                       Vol. 3, Issue 2, March -April 2013, pp.700-710

         In this type a damping material (i.e.) Rubber is inserted between the two layers of shaft and the
deflection value is calculated using ANSYS. The specification of the shaft with damping material is shown in
the Table.

Table Specifications for Steel Shaft with Rubber
           Sl. No.                          Parameters                               Values

                1                         Outer Diameter                           0.09024 m

                2                     Thickness of each layer                      1.05 e -3 m

                3                        Number of layers                               3

                4                        Damping Material                            Rubber

                5                            Element                                Shell 99




                              Fig Stacking Sequence for Steel Shaft with Rubber




CARBON EPOXY SHAFT WITHOUT DAMPING MATERIAL
         In this case Carbon Epoxy shaft is modeled with 13 layers by considering the shell element. The
specifications are shown in the Table .
                      Table Specification for Carbon Epoxy Shaft
         Sl. No.                            Parameters                                Values

            1                             Outer Diameter                             0.09024 m

            2                         Thickness of each layer                        1.5 e -4 m



                                                                                                  703 | P a g e
Davidclaude Gollapudi, P.Veera Raju / International Journal of Engineering Research and
                   Applications (IJERA) ISSN: 2248-9622 www.ijera.com
                       Vol. 3, Issue 2, March -April 2013, pp.700-710

             3                             Number of layers                                      13

             4                                  Element                                     Shell 99




                         Fig Stacking Sequence for Carbon Epoxy Shaft

In fig the stacking sequence of the Carbon Epoxy shaft without damping material is shown. Using ANSYS 11.0
the deflection value is calculated. The value is 0.93 e -4 m. The deformed shape of the shaft is shown in the Fig ..
Fig Static Deflection for Carbon Epoxy Shaft

CARBON EPOXY SHAFT WITH DAMPING MATERIAL
        In this case Carbon Epoxy shaft is modeled with damping material (Rubber) and it is incorporated in
between the layers. The specification of the shaft is shown in the Table .




Table Specification for Carbon Epoxy Shaft with Rubber
             Sl. No.                           Parameters                                 Values
                 1                          Outer Diameter                               .09024 m
                 2                      Thickness of each layer                          1.5 e -4 m
                 3                         Number of layers                                 14
                 4                         Damping Material                               Rubber
                 5                              Element                                  Shell 99

The stacking sequence of the Carbon Epoxy shaft with damping material (Rubber) is shown in the fig. Here the



                                                                                                       704 | P a g e
Davidclaude Gollapudi, P.Veera Raju / International Journal of Engineering Research and
                   Applications (IJERA) ISSN: 2248-9622 www.ijera.com
                       Vol. 3, Issue 2, March -April 2013, pp.700-710

                                            8th layer is the rubber.




                  Fig Stacking Sequence for Carbon Epoxy Shaft




              Fig Static Deflection for Carbon Epoxy Shaft with Rubber
Using ANSYS 11.0 the deflection value is calculated.The value is 0.930 e -4 m. The deformed shape of the shaft
is shown in the Fig .


E-GLASS EPOXY SHAFT WITHOUT DAMPING MATERIAL
         In this case E-Glass Epoxy shaft is modeled with 23 layers by using the shell 99 element. The
specifications are shown in the Table .Table Specification for E- Glass Epoxy Shaft

      Sl. No.                         Parameters                                Values

         1                          Outer Diameter                             .09024 m

         2                      Thickness of each layer                        1.5 e -4 m

         3                         Number of layers                               23

         4                              Element                                Shell 99




                                                                                                705 | P a g e
Davidclaude Gollapudi, P.Veera Raju / International Journal of Engineering Research and
                   Applications (IJERA) ISSN: 2248-9622 www.ijera.com
                       Vol. 3, Issue 2, March -April 2013, pp.700-710




Fig Stacking Sequence Layers from 1 to 15




Fig Stacking Sequence Layers from 16 to 23
        The stacking sequence of the Carbon Epoxy shaft without damping material is shown in fig .




                                                                                               706 | P a g e
Davidclaude Gollapudi, P.Veera Raju / International Journal of Engineering Research and
                  Applications (IJERA) ISSN: 2248-9622 www.ijera.com
                      Vol. 3, Issue 2, March -April 2013, pp.700-710




Fig Static Deflection for E-Glass Epoxy Shaft
Using ANSYS 11.0 the deflection value is calculated. The value is 0.282 e -3 m. The deformed shape of the
shaft is shown in the Fign

E-GLASS EPOXY SHAFT WITH DAMPING MATERIAL
        In this case E-Glass epoxy shaft is modeled with damping material (Rubber) and it is incorporated in
between the layers. The specification of the shaft is shown in the Table .
Table Specification for E- Glass Epoxy Shaft with Rubber


            Sl. No.                        Parameters                               Values

               1                         Outer Diameter                           .09024 m

               2                     Thickness of each layer                       1.5 e -4 m

               3                        Number of layers                              14

               4                        Damping Material                           Rubber

               5                             Element                               Shell 99




                                                                                                707 | P a g e
Davidclaude Gollapudi, P.Veera Raju / International Journal of Engineering Research and
                   Applications (IJERA) ISSN: 2248-9622 www.ijera.com
                       Vol. 3, Issue 2, March -April 2013, pp.700-710




   Fig Stacking Sequence Layers from 16 to 24 The stacking sequence of the E-Glass Epoxy shaft with
                               damping material (Rubber) is shown in fig
                                    Here the 12th layer is the rubber.




Fig Static Deflection for E-Glass Epoxy Shaft with Rubber
Using ANSYS 11.0 the deflection value is calculated. The value is 0.263 e -3 m. The deformed shape of the
shaft is shown in the Fig .

RESULTS AND DISCUSSIONS DISCUSSIONS ON PROBLEM
       In this case all the results of Static, Modal and Transient Dynamic Analysis of Steel Shaft, Carbon
Epoxy Shaft and E-Glass Epoxy shaft with and without damping polymer are tabulated and compared

COMPARISON OF STEEL SHAFT WITH AND WITHOUT DAMPING MATERIAL
Comparison of Results for Steel Shaft
    Type of the
                                                          Steel with Viscoelastic             Deviation
         Shaft              Steel without Viscoelastic
                                                                 Material                       (%)
Results                              Material
Static Deflection
                                     0.117 e-3                   0.961 e -4             17.86
          (in m)
 Fundamental      Natural
Frequency                             57.368                      64.011                       10.38
         (in Hz)
Damping Factor                        0.04297                    0.05037                       14.69
From the above results shown in the Table
     a. The damping value and the fundamental natural frequency of the steel shaft is increased to 14.69% and
         10.38 % respectively, when the shaft is embedded with viscoelastic polymer.


                                                                                               708 | P a g e
Davidclaude Gollapudi, P.Veera Raju / International Journal of Engineering Research and
                   Applications (IJERA) ISSN: 2248-9622 www.ijera.com
                       Vol. 3, Issue 2, March -April 2013, pp.700-710

    b.   The static deflection value of the steel shaft is decreased by 17.86% when the damping material is
         embedded.

COMPARISON OF CARBON EPOXY SHAFT WITH AND WITHOUT DAMPING MATERIAL
Comparison of Results for Carbon Epoxy Shaft

      Type of the
           Shaft                                         Carbon Epoxy with               Deviation
   Results                    Carbon Epoxy without       Damping Material                  (%)
                                Damping Material

   Static Deflection
            (in m)                  0.930 e -4                0.814 e -4                   12.47
   Modal Frequency
          (in Hz)                     64.049                   68.568                      6.59

   Damping Factor                    0.08268                   0.08945                     7.57
From the above results shown in the Table
    a. The damping value and the fundamental natural frequency of the Carbon Epoxy shaft is increased to
        7.57 % and 6.59 % respectively, when the shaft is embedded with viscoelastic polymer.
    b. The static deflection value of the Carbon Epoxy shaft is decreased by 12.47 % when the damping
        material is embedded.

COMPARISON OF E-GLASS EPOXY SHAFT WITH AND WITHOUT DAMPING MATERIAL

Comparison of Results for E- Glass Epoxy Shaft
      Type of the
                                                                                        Deviation
            Shaft              Glass Epoxy without       Glass Epoxy with
                                                                                          (%)
   Results                      Damping Material         Damping Material
   Static Deflection
                                     0.285 e -3               0.268 e -3                   5.96
            (in m)
   Modal Frequency
                                        32.9                      33.50                    1.8
           (in Hz)
   Damping Factor                    0.02702                  0.02842                      4.93

From the above results shown in the Table
    a. The damping value and the fundamental                              Steel, Carbon Epoxy and E- Glass
        natural frequency of the E- Glass Epoxy                           Epoxy Shafts respectively.
        Shaft is increased to 4.93 % and 1.8 %                         The fundamental natural frequency
        respectively, when the shaft is embedded                          increased by 10.38%, 6.59% and
        with viscoelastic polymer.                                        1.8% for Steel, Carbon Epoxy and
    b. The static deflection value of the E- Glass                        E- Glass Epoxy Shafts respectively.
        Epoxy Shaft is decreased by 5.96 % when                        The deflection value decreased by
        the damping material is embedded.                                 17.84%, 12.48% and 5.69% for
                                                                          Steel , Carbon Epoxy and E- Glass
  CONCLUSIONS                                                             Epoxy Shafts respectively.
        The damping factor has been found out for                     The increase in damping factor
         Steel Shaft, Carbon Epoxy Shaft and E-                           results in further suppression of
         Glass Epoxy Shaft with and without                               vibrations and hence results in
         Viscoelastic polymer (Rubber).                                   increased structural life.
        The Static, Modal and Transient Dynamic                   An optimal relation between design
         Analyses have been carried out using                       parameters such as the length, diameter,
         Finite Element Analysis.                                   spacing, and Young’s modulus of fibers
        The following observations were made by                    and the shear modulus of viscoelastic
         embedding the Viscoelastic polymer                         matrix has been derived for achieving
         (Rubber) into the structure.                               maximum damping performance. It has
            Damping factor increased by                            been found that for maximum damping
                14.69%, 7.57% and 4.93% for                         performance, the characteristic value of
                                                                    the composite should be set to 0.75.


                                                                                                  709 | P a g e
Davidclaude Gollapudi, P.Veera Raju / International Journal of Engineering Research and
                 Applications (IJERA) ISSN: 2248-9622 www.ijera.com
                     Vol. 3, Issue 2, March -April 2013, pp.700-710

                                                           Adhesively Bonded Joints for Composite
BIBLIOGRAPHY                                               Propeller shafts”, Journal of Composite
 [1]   Autar K. Kaw, "Mechanics of Composite               Materials, Vol.35, No.11, pp. 999-1021.
       Materials", CRC press, 1997.                 [7]    T. E. Alberts and Houchun Xia, “Design
 [2]   Ahid D. Nashif, David I. G. Jones and               and Analysis of Fiber Enhanced
       John P. Henderson, “Vibration Damping”,             Viscoelastic Damping Polymers”, Journal
       John Wiley & Sons Publication, 1985,                of Vibration and Acoustics, Vol. 117,
       Newyork.                                            October 1995, pp. 398-404.
 [3]   C. T. Sun and Y. P. Lu, "Vibration           [8]    K. J. Buhariwala and J. S. Hansen,
       Damping of Structural Elements",                    "Dynamics of Viscoelastic Structures",
       Prentince Hall PTR, New Jeresy, 1995.               AIAA          Journal, Vol. 26, February
 [4]   K. L. Napolitano, W. Grippo, J. B.                  1988, pp 220-227.
       Kosmatka and C. D. Johnson, “A               [9]    J. B. Kosmatka and S. L. Liguore,
       comparison of two cocured damped                    “Review of Methods for Analyzing
       composite torsion shafts”, Composite                Constrained Layer Damped Structures”,
       Structures, Vol. 43, 1998, pp. 115-125.             Journal of Aerospace Engineering, Vol.6,
 [5]   J. M. Biggerstaff and J. B. Kosmatka,               No.3, July 1993, pp. 268-283.
       “Damping Performance of Cocured              [10]   T. C. Ramesh and N. Ganesan, “Vibration
       Composite Laminates with Embedded                   and Damping Analysis of Cylindrical
       Viscoelastic     Layers”,    Journal    of          Shells with Constrained Damping
       Composite Materials, Vol. 32, No.21/                Treatment- A Comparison of Three
       1998.                                               Theories”, Journal of Vibration and
 [6]   Jin Kook Kim, Dai Gil Lee, and Durk                 Acoustics, Vol. 117, April 1995, pp. 213 –
       Hyun Cho, 2001, “Investigation of                   219.




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  • 1. Davidclaude Gollapudi, P.Veera Raju / International Journal of Engineering Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com Vol. 3, Issue 2, March -April 2013, pp.700-710 Design And Dynamic Analysis Of Viscoelastic Structures For Propellar Shaft DAVIDCLAUDE GOLLAPUDI1 P.Veera Raju2 Associate professor at Dept of Mechanical Engineering G.I.E.T in the Dept of Mechanical Pursuing M.Tech in G.I.E.T Engineering, pursuing Ph.D in Rajahmundry (JNTUK) KAKINADA ABSTRACT High-technology structures often have be analyzed by using Finite Element Analysis stringent requirements for structural dynamics. Suppressing vibrations is crucial to their Keywords: laminated composite materials, damping performance. Passive damping is used to suppress factor, natural frequency, deflection using finite vibrations by reducing peak resonant response. element analysis. Viscoelastic damping materials add passive damping to structures by dissipating vibration INTRODUCTION strain energy in the form of heat energy. The PROPULSION SHAFT: incorporation of damping materials in advanced The torque transmission capability of the propeller composite materials offers the possibility of highly shaft for ship should be larger than 3,500 Nm and damped, light-weight structural components that fundamental natural bending frequency of the are vibration-resistant. The effect of damping on propeller shaft should be higher than 6,500 rpm to the performance of isotropic (like Steel) and avoid whirling vibration. The outer diameter of the orthotropic (like Carbon Epoxy & E-Glass Epoxy) propeller shaft should not exceed 100 mm due to structures are analysed by using Finite Element space limitations. The propeller shaft of transmission Analysis. Damping factors, fundamental natural system is shown in figure for following specified frequencies are increased for Steel Shaft, Carbon design requirements as shown in Table. Due to space Epoxy Shaft and E- Glass Epoxy Shaft limitations the outer diameter of the shaft is restricted respectively, while embedding the rubber into the to 90.24 mm. The one-piece hollow composite drive structure. The deflection value is decreased for shaft should satisfy three design specifications, such same Shaft respectively, when rubber is embedded as static torque transmission capability, torsional into the structure. The effect of damping on the buckling capacity and the fundamental natural performance of isotropic (steel) and orthotropic bending frequency. For given specification, the (Carbon Epoxy & E-Glass Epoxy) structures is to damping factor for Steel, carbon Epoxy and E-Glass Epoxy are to be calculated and compared with and without damping material (Rubber). Table Problem Specification Sl. No. Parameter Notation Units Value 1. Torque T N-m 3500 2. Max Speed N RPM 6500 3. Length L m 1.250 700 | P a g e
  • 2. Davidclaude Gollapudi, P.Veera Raju / International Journal of Engineering Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com Vol. 3, Issue 2, March -April 2013, pp.700-710 Pictorial representation of shaft transmission system. Material Properties COMPOSITE MATERIALS Composite materials are those containing more than one bonded material, each with different material properties. The major advantages of composite materials are that they have a high ratio of stiffness to weight and strength to weight. A principal advantage of composite materials lies in the ability of the designer to tailor the material properties to the application. The matrix material may be a plastic or rubber polymer, a metal or a ceramic. The most common form in which fiber reinforced composites are used in structural applications is called a laminate. It is obtained by stacking a number of thin layers of fibers and matrix consolidating them to the desired thickness. Fiber orientation in each layer as well as the stacking sequence of various layers can be controlled to generate a wide range of physical and mechanical properties for the composite laminate. 701 | P a g e
  • 3. Davidclaude Gollapudi, P.Veera Raju / International Journal of Engineering Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com Vol. 3, Issue 2, March -April 2013, pp.700-710 ADVANTAGES OF COMPOSITES High strength to weight ratio, High stiffness, High impact resistance, Better fatigue resistance, Improved corrosion resistance, Good thermal conductivity VISCOELASTIC MATERIAL A Viscoelastic material sometimes is called material with memory. This implies that a Viscoelastic material's behavior depends not only on the current loading conditions, but also on the loading history. They are characterized by possessing both viscous and elastic behavior. A purely elastic material is one in which all the energy stored in the sample during loading is returned when the load is removed. As a result, the stress and strain curves for elastic materials move completely in phase. For elastic materials, Hooke’s Law applies, where the stress is proportional to the strain, and the modulus is defined at the ratio of stress to strain. FEM The Basic concept in FEA is that the body or structure may be divided into smaller elements of finite dimensions called “Finite Elements”. The original body or the structure is then considered as an assemblage of these elements connected at a finite number of joints called “Nodes” or “Nodal Points”. Simple functions are chosen to approximate the displacements over each finite element. Such assumed functions are called “shape functions”. This will represent the displacement with in the element in terms of the displacement at the nodes of the element 7.1 table Specification for Steel Shaft Sl. No. Parameters Values 1 Outer Diameter 0.09024 m 2 Thickness 2.1 e -3 Deflection of Steel Shaft without Rubber . STEEL SHAFT WITH DAMPING MATERIAL 702 | P a g e
  • 4. Davidclaude Gollapudi, P.Veera Raju / International Journal of Engineering Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com Vol. 3, Issue 2, March -April 2013, pp.700-710 In this type a damping material (i.e.) Rubber is inserted between the two layers of shaft and the deflection value is calculated using ANSYS. The specification of the shaft with damping material is shown in the Table. Table Specifications for Steel Shaft with Rubber Sl. No. Parameters Values 1 Outer Diameter 0.09024 m 2 Thickness of each layer 1.05 e -3 m 3 Number of layers 3 4 Damping Material Rubber 5 Element Shell 99 Fig Stacking Sequence for Steel Shaft with Rubber CARBON EPOXY SHAFT WITHOUT DAMPING MATERIAL In this case Carbon Epoxy shaft is modeled with 13 layers by considering the shell element. The specifications are shown in the Table . Table Specification for Carbon Epoxy Shaft Sl. No. Parameters Values 1 Outer Diameter 0.09024 m 2 Thickness of each layer 1.5 e -4 m 703 | P a g e
  • 5. Davidclaude Gollapudi, P.Veera Raju / International Journal of Engineering Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com Vol. 3, Issue 2, March -April 2013, pp.700-710 3 Number of layers 13 4 Element Shell 99 Fig Stacking Sequence for Carbon Epoxy Shaft In fig the stacking sequence of the Carbon Epoxy shaft without damping material is shown. Using ANSYS 11.0 the deflection value is calculated. The value is 0.93 e -4 m. The deformed shape of the shaft is shown in the Fig .. Fig Static Deflection for Carbon Epoxy Shaft CARBON EPOXY SHAFT WITH DAMPING MATERIAL In this case Carbon Epoxy shaft is modeled with damping material (Rubber) and it is incorporated in between the layers. The specification of the shaft is shown in the Table . Table Specification for Carbon Epoxy Shaft with Rubber Sl. No. Parameters Values 1 Outer Diameter .09024 m 2 Thickness of each layer 1.5 e -4 m 3 Number of layers 14 4 Damping Material Rubber 5 Element Shell 99 The stacking sequence of the Carbon Epoxy shaft with damping material (Rubber) is shown in the fig. Here the 704 | P a g e
  • 6. Davidclaude Gollapudi, P.Veera Raju / International Journal of Engineering Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com Vol. 3, Issue 2, March -April 2013, pp.700-710 8th layer is the rubber. Fig Stacking Sequence for Carbon Epoxy Shaft Fig Static Deflection for Carbon Epoxy Shaft with Rubber Using ANSYS 11.0 the deflection value is calculated.The value is 0.930 e -4 m. The deformed shape of the shaft is shown in the Fig . E-GLASS EPOXY SHAFT WITHOUT DAMPING MATERIAL In this case E-Glass Epoxy shaft is modeled with 23 layers by using the shell 99 element. The specifications are shown in the Table .Table Specification for E- Glass Epoxy Shaft Sl. No. Parameters Values 1 Outer Diameter .09024 m 2 Thickness of each layer 1.5 e -4 m 3 Number of layers 23 4 Element Shell 99 705 | P a g e
  • 7. Davidclaude Gollapudi, P.Veera Raju / International Journal of Engineering Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com Vol. 3, Issue 2, March -April 2013, pp.700-710 Fig Stacking Sequence Layers from 1 to 15 Fig Stacking Sequence Layers from 16 to 23 The stacking sequence of the Carbon Epoxy shaft without damping material is shown in fig . 706 | P a g e
  • 8. Davidclaude Gollapudi, P.Veera Raju / International Journal of Engineering Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com Vol. 3, Issue 2, March -April 2013, pp.700-710 Fig Static Deflection for E-Glass Epoxy Shaft Using ANSYS 11.0 the deflection value is calculated. The value is 0.282 e -3 m. The deformed shape of the shaft is shown in the Fign E-GLASS EPOXY SHAFT WITH DAMPING MATERIAL In this case E-Glass epoxy shaft is modeled with damping material (Rubber) and it is incorporated in between the layers. The specification of the shaft is shown in the Table . Table Specification for E- Glass Epoxy Shaft with Rubber Sl. No. Parameters Values 1 Outer Diameter .09024 m 2 Thickness of each layer 1.5 e -4 m 3 Number of layers 14 4 Damping Material Rubber 5 Element Shell 99 707 | P a g e
  • 9. Davidclaude Gollapudi, P.Veera Raju / International Journal of Engineering Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com Vol. 3, Issue 2, March -April 2013, pp.700-710 Fig Stacking Sequence Layers from 16 to 24 The stacking sequence of the E-Glass Epoxy shaft with damping material (Rubber) is shown in fig Here the 12th layer is the rubber. Fig Static Deflection for E-Glass Epoxy Shaft with Rubber Using ANSYS 11.0 the deflection value is calculated. The value is 0.263 e -3 m. The deformed shape of the shaft is shown in the Fig . RESULTS AND DISCUSSIONS DISCUSSIONS ON PROBLEM In this case all the results of Static, Modal and Transient Dynamic Analysis of Steel Shaft, Carbon Epoxy Shaft and E-Glass Epoxy shaft with and without damping polymer are tabulated and compared COMPARISON OF STEEL SHAFT WITH AND WITHOUT DAMPING MATERIAL Comparison of Results for Steel Shaft Type of the Steel with Viscoelastic Deviation Shaft Steel without Viscoelastic Material (%) Results Material Static Deflection 0.117 e-3 0.961 e -4 17.86 (in m) Fundamental Natural Frequency 57.368 64.011 10.38 (in Hz) Damping Factor 0.04297 0.05037 14.69 From the above results shown in the Table a. The damping value and the fundamental natural frequency of the steel shaft is increased to 14.69% and 10.38 % respectively, when the shaft is embedded with viscoelastic polymer. 708 | P a g e
  • 10. Davidclaude Gollapudi, P.Veera Raju / International Journal of Engineering Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com Vol. 3, Issue 2, March -April 2013, pp.700-710 b. The static deflection value of the steel shaft is decreased by 17.86% when the damping material is embedded. COMPARISON OF CARBON EPOXY SHAFT WITH AND WITHOUT DAMPING MATERIAL Comparison of Results for Carbon Epoxy Shaft Type of the Shaft Carbon Epoxy with Deviation Results Carbon Epoxy without Damping Material (%) Damping Material Static Deflection (in m) 0.930 e -4 0.814 e -4 12.47 Modal Frequency (in Hz) 64.049 68.568 6.59 Damping Factor 0.08268 0.08945 7.57 From the above results shown in the Table a. The damping value and the fundamental natural frequency of the Carbon Epoxy shaft is increased to 7.57 % and 6.59 % respectively, when the shaft is embedded with viscoelastic polymer. b. The static deflection value of the Carbon Epoxy shaft is decreased by 12.47 % when the damping material is embedded. COMPARISON OF E-GLASS EPOXY SHAFT WITH AND WITHOUT DAMPING MATERIAL Comparison of Results for E- Glass Epoxy Shaft Type of the Deviation Shaft Glass Epoxy without Glass Epoxy with (%) Results Damping Material Damping Material Static Deflection 0.285 e -3 0.268 e -3 5.96 (in m) Modal Frequency 32.9 33.50 1.8 (in Hz) Damping Factor 0.02702 0.02842 4.93 From the above results shown in the Table a. The damping value and the fundamental Steel, Carbon Epoxy and E- Glass natural frequency of the E- Glass Epoxy Epoxy Shafts respectively. Shaft is increased to 4.93 % and 1.8 %  The fundamental natural frequency respectively, when the shaft is embedded increased by 10.38%, 6.59% and with viscoelastic polymer. 1.8% for Steel, Carbon Epoxy and b. The static deflection value of the E- Glass E- Glass Epoxy Shafts respectively. Epoxy Shaft is decreased by 5.96 % when  The deflection value decreased by the damping material is embedded. 17.84%, 12.48% and 5.69% for Steel , Carbon Epoxy and E- Glass CONCLUSIONS Epoxy Shafts respectively.  The damping factor has been found out for  The increase in damping factor Steel Shaft, Carbon Epoxy Shaft and E- results in further suppression of Glass Epoxy Shaft with and without vibrations and hence results in Viscoelastic polymer (Rubber). increased structural life.  The Static, Modal and Transient Dynamic  An optimal relation between design Analyses have been carried out using parameters such as the length, diameter, Finite Element Analysis. spacing, and Young’s modulus of fibers  The following observations were made by and the shear modulus of viscoelastic embedding the Viscoelastic polymer matrix has been derived for achieving (Rubber) into the structure. maximum damping performance. It has  Damping factor increased by been found that for maximum damping 14.69%, 7.57% and 4.93% for performance, the characteristic value of the composite should be set to 0.75. 709 | P a g e
  • 11. Davidclaude Gollapudi, P.Veera Raju / International Journal of Engineering Research and Applications (IJERA) ISSN: 2248-9622 www.ijera.com Vol. 3, Issue 2, March -April 2013, pp.700-710 Adhesively Bonded Joints for Composite BIBLIOGRAPHY Propeller shafts”, Journal of Composite [1] Autar K. Kaw, "Mechanics of Composite Materials, Vol.35, No.11, pp. 999-1021. Materials", CRC press, 1997. [7] T. E. Alberts and Houchun Xia, “Design [2] Ahid D. Nashif, David I. G. Jones and and Analysis of Fiber Enhanced John P. Henderson, “Vibration Damping”, Viscoelastic Damping Polymers”, Journal John Wiley & Sons Publication, 1985, of Vibration and Acoustics, Vol. 117, Newyork. October 1995, pp. 398-404. [3] C. T. Sun and Y. P. Lu, "Vibration [8] K. J. Buhariwala and J. S. Hansen, Damping of Structural Elements", "Dynamics of Viscoelastic Structures", Prentince Hall PTR, New Jeresy, 1995. AIAA Journal, Vol. 26, February [4] K. L. Napolitano, W. Grippo, J. B. 1988, pp 220-227. Kosmatka and C. D. Johnson, “A [9] J. B. Kosmatka and S. L. Liguore, comparison of two cocured damped “Review of Methods for Analyzing composite torsion shafts”, Composite Constrained Layer Damped Structures”, Structures, Vol. 43, 1998, pp. 115-125. Journal of Aerospace Engineering, Vol.6, [5] J. M. Biggerstaff and J. B. Kosmatka, No.3, July 1993, pp. 268-283. “Damping Performance of Cocured [10] T. C. Ramesh and N. Ganesan, “Vibration Composite Laminates with Embedded and Damping Analysis of Cylindrical Viscoelastic Layers”, Journal of Shells with Constrained Damping Composite Materials, Vol. 32, No.21/ Treatment- A Comparison of Three 1998. Theories”, Journal of Vibration and [6] Jin Kook Kim, Dai Gil Lee, and Durk Acoustics, Vol. 117, April 1995, pp. 213 – Hyun Cho, 2001, “Investigation of 219. 710 | P a g e