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Innovative Systems Design and Engineering                                                www.iiste.org
ISSN 2222-1727 (Paper) ISSN 2222-2871 (Online)
Vol 2, No 4, 2011

    Analysis of bending strength of helical gear by
                        FEM
                                 Kailash C. Bhosale (Corresponding author)

                                 SRES College of Engineering, Kopargaon.

                              Dist- Ahmadnagar (Maharashtra) India.-423603.

                                    Email: bhosale_kailash@yahoo.co.in

Abstract:

Lewis equation is used for finding out the bending strength of a helical gear. This equation is based on
certain assumptions. Various FEM are also based on this equation. Bending stress can also be found out by
modified Lewis formula, AGMA standards etc. In this paper a comparison between Lewis equation and
Ansys workbench is done.

Keywords: helical gear, bending strength, FEM

1. Introduction:

         Lewis equation is used for finding out the bending strength of a helical gear. Various FEM are
also based on this equation.

        In this work bending strength of helical gear is found out with the help of three dimensional
photoelasticity. A helical gearbox with 2.2 kW power transmitting at 760 rpm and

Number of Teeth = 30mm, Pitch circle Diameter = 60mm, Module = 2mm, Pressure Angle =20°, Helix
Angle = 12054’, Addendum = 64mm, Base circle Diameter = 56.38mm, Dedendum = 55mm

2. Theoretical analysis

          The finite element method is a numerical analysis technique for obtaining approximate solutions
to a wide variety of engineering problems. The method originated in the aerospace industry as a tool to
study stresses in complex airframe structures. It grew out of what was called the matrix analysis method
used in aircraft design. The method has gained increased popularity among both researchers and
practitioners.

2.1 Theoretical analysis By Lewis equation:

     The analysis of bending stress in gear tooth was done by Mr. Wilfred Lewis known as Lewis equation.
In the Lewis analysis, the gear tooth is treated as a cantilever beam as shown in fig. 4.1. The tangential
component (Pt) causes the bending moment about the base of tooth. The Lewis analysis is based on the
following assumptions:

The effect of radial component (Pr) is neglected.

The effect of stress concentration is neglected.

At any time only one pair of teeth is in contact and takes the total load.




                                                      125
Innovative Systems Design and Engineering                                                   www.iiste.org
ISSN 2222-1727 (Paper) ISSN 2222-2871 (Online)
Vol 2, No 4, 2011
      It is observed that the cross- section of tooth varies from free end to fixed end. Therefore, a parabola
is constructed with in the tooth profile. The advantage of parabolic outlines is that it is a beam of uniform
strength [6].

In fig.2.2 at section XX,                                    ………..… (Eq.2.1)


                ………….….(Eq. 2.2)



             …………..         .(Eq. 2.3)
Here,
        = Bending Moment,
   h = Height from root of tooth (dedendum circle to intersection of parabolas)
I = M.I of tooth about neutral axis and
t = thickness of tooth at root y = Distance of neutral axis from edge.




Figure 2.1 Gear Tooth As Cantilever Beam                 Figure.2.2 Gear Tooth As Parabolic Beam


 The bending stress (σb) is given by

                                         …………………..(Eq. 2.4)
Putting values of Mb, I, y and solving,
   We get,


                     …………..(Eq. 2.5)
 Here, Y is Lewis form factor


                    …………. (Eq. 2.6)
  m= Module of gear,                                 Pt = tangential component of load
Calculations:




                                                     126
Innovative Systems Design and Engineering                                                   www.iiste.org
ISSN 2222-1727 (Paper) ISSN 2222-2871 (Online)
Vol 2, No 4, 2011
The speed of helical gear (n) =760 rpm
Torque transmitted by helical pinion =M
Power transmitted by gear box (P) =2.2 KW



                              ……………                                                                   (Eq.2.7)



                                                                            …..                       (Eq.2.8)
   Mt = 27656.72 N-mm
Tangential component acts at pitch poin

Pt × ( ) = Mt ………………………………… (Eq. 2.9)

 Where               d = Pitch circle diameter
Pt = 921.89 N
In order to determine bending stress, the helical gear is considered to be equivalent to a formative spur
gear. The formative gear is an imaginary spur gear in a plane perpendicular to the tooth element.
   Therefore for helical gear,

 b’ =              = 24.58mm


 Z’ =              =33

 Y for Z’ = 0.367


                         ………..(Eq. 2.10)

b =         921.89                              b   = 51.08 N/ mm2 (theoretically)
        2  24.58  0.367


Therefore, theoretically bending strength of helical gear is = 51.08 N/ mm2



3. Solid Modeling And Modeling:

A solid modeling is done with Catia and then by using the hypermesh meshing is done. Analysis is done
with Ansys Workbench 12.1.




                                                       127
Innovative Systems Design and Engineering                                                        www.iiste.org
ISSN 2222-1727 (Paper) ISSN 2222-2871 (Online)
Vol 2, No 4, 2011




Figure 3.1. Meshing with Hypermesh                         Figure 3.2 : Maximum Principal Stress plot




Figure 3.2 : Maximum Principal Stress plot

4. Result And Conclusion:

1)In helical gear the engagement between driver gear and driven gear teeth begins with point contact and
gradually extends along the tooth surface. Due to initial point contact in helical gear the bending stresses
produced at critical section (root of tooth) are maximum as compared to spur gear, which has kinematic
line contact.

2)The calculation of maximum stresses in a helical gear at tooth root is three dimensional problems. The accurate
evaluation of stress state and distribution of stress is complex task. The stresses produced at any discontinuity are
different in magnitude from those calculated by elementary formulae.

3) In theory of helical gear we are considering that load is acting at one point and the stress is calculated.
But, in case of FEM a continuous load is considered. So a pressure will act along the teeth of helical gear.



REFERENCES

V. B. Bhandari, “Design of machine elements”, Tata McGraw hill publishing company limited, second
edition, pp. 703-720.

Design data book, PSG College of Technology, pp.8.1-8.64.

N.S. Gokhale, S.S.Deshpande, “Practical finite element analysis”, Finite to Infinite, pp.111-207.




                                                        128

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14 kailash fem-125-128

  • 1. Innovative Systems Design and Engineering www.iiste.org ISSN 2222-1727 (Paper) ISSN 2222-2871 (Online) Vol 2, No 4, 2011 Analysis of bending strength of helical gear by FEM Kailash C. Bhosale (Corresponding author) SRES College of Engineering, Kopargaon. Dist- Ahmadnagar (Maharashtra) India.-423603. Email: bhosale_kailash@yahoo.co.in Abstract: Lewis equation is used for finding out the bending strength of a helical gear. This equation is based on certain assumptions. Various FEM are also based on this equation. Bending stress can also be found out by modified Lewis formula, AGMA standards etc. In this paper a comparison between Lewis equation and Ansys workbench is done. Keywords: helical gear, bending strength, FEM 1. Introduction: Lewis equation is used for finding out the bending strength of a helical gear. Various FEM are also based on this equation. In this work bending strength of helical gear is found out with the help of three dimensional photoelasticity. A helical gearbox with 2.2 kW power transmitting at 760 rpm and Number of Teeth = 30mm, Pitch circle Diameter = 60mm, Module = 2mm, Pressure Angle =20°, Helix Angle = 12054’, Addendum = 64mm, Base circle Diameter = 56.38mm, Dedendum = 55mm 2. Theoretical analysis The finite element method is a numerical analysis technique for obtaining approximate solutions to a wide variety of engineering problems. The method originated in the aerospace industry as a tool to study stresses in complex airframe structures. It grew out of what was called the matrix analysis method used in aircraft design. The method has gained increased popularity among both researchers and practitioners. 2.1 Theoretical analysis By Lewis equation: The analysis of bending stress in gear tooth was done by Mr. Wilfred Lewis known as Lewis equation. In the Lewis analysis, the gear tooth is treated as a cantilever beam as shown in fig. 4.1. The tangential component (Pt) causes the bending moment about the base of tooth. The Lewis analysis is based on the following assumptions: The effect of radial component (Pr) is neglected. The effect of stress concentration is neglected. At any time only one pair of teeth is in contact and takes the total load. 125
  • 2. Innovative Systems Design and Engineering www.iiste.org ISSN 2222-1727 (Paper) ISSN 2222-2871 (Online) Vol 2, No 4, 2011 It is observed that the cross- section of tooth varies from free end to fixed end. Therefore, a parabola is constructed with in the tooth profile. The advantage of parabolic outlines is that it is a beam of uniform strength [6]. In fig.2.2 at section XX, ………..… (Eq.2.1) ………….….(Eq. 2.2) ………….. .(Eq. 2.3) Here, = Bending Moment, h = Height from root of tooth (dedendum circle to intersection of parabolas) I = M.I of tooth about neutral axis and t = thickness of tooth at root y = Distance of neutral axis from edge. Figure 2.1 Gear Tooth As Cantilever Beam Figure.2.2 Gear Tooth As Parabolic Beam The bending stress (σb) is given by …………………..(Eq. 2.4) Putting values of Mb, I, y and solving, We get, …………..(Eq. 2.5) Here, Y is Lewis form factor …………. (Eq. 2.6) m= Module of gear, Pt = tangential component of load Calculations: 126
  • 3. Innovative Systems Design and Engineering www.iiste.org ISSN 2222-1727 (Paper) ISSN 2222-2871 (Online) Vol 2, No 4, 2011 The speed of helical gear (n) =760 rpm Torque transmitted by helical pinion =M Power transmitted by gear box (P) =2.2 KW …………… (Eq.2.7) ….. (Eq.2.8) Mt = 27656.72 N-mm Tangential component acts at pitch poin Pt × ( ) = Mt ………………………………… (Eq. 2.9) Where d = Pitch circle diameter Pt = 921.89 N In order to determine bending stress, the helical gear is considered to be equivalent to a formative spur gear. The formative gear is an imaginary spur gear in a plane perpendicular to the tooth element. Therefore for helical gear, b’ = = 24.58mm Z’ = =33 Y for Z’ = 0.367 ………..(Eq. 2.10) b = 921.89 b = 51.08 N/ mm2 (theoretically) 2  24.58  0.367 Therefore, theoretically bending strength of helical gear is = 51.08 N/ mm2 3. Solid Modeling And Modeling: A solid modeling is done with Catia and then by using the hypermesh meshing is done. Analysis is done with Ansys Workbench 12.1. 127
  • 4. Innovative Systems Design and Engineering www.iiste.org ISSN 2222-1727 (Paper) ISSN 2222-2871 (Online) Vol 2, No 4, 2011 Figure 3.1. Meshing with Hypermesh Figure 3.2 : Maximum Principal Stress plot Figure 3.2 : Maximum Principal Stress plot 4. Result And Conclusion: 1)In helical gear the engagement between driver gear and driven gear teeth begins with point contact and gradually extends along the tooth surface. Due to initial point contact in helical gear the bending stresses produced at critical section (root of tooth) are maximum as compared to spur gear, which has kinematic line contact. 2)The calculation of maximum stresses in a helical gear at tooth root is three dimensional problems. The accurate evaluation of stress state and distribution of stress is complex task. The stresses produced at any discontinuity are different in magnitude from those calculated by elementary formulae. 3) In theory of helical gear we are considering that load is acting at one point and the stress is calculated. But, in case of FEM a continuous load is considered. So a pressure will act along the teeth of helical gear. REFERENCES V. B. Bhandari, “Design of machine elements”, Tata McGraw hill publishing company limited, second edition, pp. 703-720. Design data book, PSG College of Technology, pp.8.1-8.64. N.S. Gokhale, S.S.Deshpande, “Practical finite element analysis”, Finite to Infinite, pp.111-207. 128