Study of The Inverse Magnetostriction Effect On Machine Deformation
Study of The Inverse Magnetostriction Effect On Machine Deformation
O. A. Mohammed, Fellow IEEE, S. Liu, Member IEEE, and N. Abed, Student Member
                                    Dept. of Electrical and Computer Engineering
                                           Florida International University
                                                Miami, Florida, USA
                                                mohammed@fiu.edu
                                INTRODUCTION                                                                                                                     Excitation
                                                                                                                                                                 winding
          The inverse magnetostriction effects have been                                                         Fig. 1 Sample and measure method
    recognized for many years. It means that the magnetic
    properties of the magnetic materials are influenced by the
    applied and internal mechanical stresses. It is described by                          COUPLED MAGNETOELASTIC FORMULAR INCLUDING THE
    magnetization curves at different stress levels [1]. The changes                                MAGNETOSTRICTION EFFECTS
    of the magnetization property will bring the changes of the
    magnetic force acting on the machine stator iron. They reflect                        Below is the equation for the coupled magnetoelastic
    in both the force magnitude and its distribution. For this reason,                 problem.
    magnetostriction effects are considered to be one of the main
    reasons for the machine noise and vibration.                                       [S ][A] = [J e ]                                                                         (1)
        In this paper, first, our method of measuring the inverse                      [K ][U ] = [F ]                                                                          (2)
    magnetostriction effects is presented. Then, the FE formula,
    used for the magneto-mechanical coupled analysis including                             Where, S and K are electromagnetic stiffness matrix and
    anisotropy reluctivity tensor and inverse magnetostriction                         mechanical stiffness matrix respectively. J e represents the
    effects, are reviewed and the implementation details are
    explained. Last, the measured magnetization curves at various                      excitation of the magnetic field. F is the force applied on the
    stress levels and the proposed formulas are applied to a surface                   stress field. A is vector potential; U is displacement.
    mounted PM motor to investigate the effects of                                         The magnetostriction effects should be considered both in
    magnetostriction on the stator deformation. Both results                           the computation of S and F . When calculate S , the
    obtained with and without magnetostriction effects                                 permeability determination of the ferromagnetic materials
    consideration are provided for comparison purpose.                                 depends not only on the field strength H but also on the stress
                                                                                       level they are suffering.
    MEASUREMENT OF THE INVERSE MAGNETOSTRICTION EFFECTS                                    If the virtual work principle is adopted for the magnetic
                OF ELECTRICAL STEEL SHEETS                                             force calculation, an additional term of force needs to be added.
                                                                                       This is due to magnetostriction effects. The first reference of
       According to the definition of the inverse magnetostriction                     this paper gives the detailed deduction of the force calculation.
    effects mentioned in the introduction part, the measurement                        For convenience, the deduced element force formulation is
    method is proposed by the authors, as shown in Fig. 1.                             rewritten below [2,3]:
       A steel sheet sample is inserted at the center of the
    excitation winding. Pulling forces are applied at the two ends                                          B                  B                  (det(G ))
                                                                                                
                                                                                       F e =  [( H T         ) det(G ) + (   0 H
                                                                                                                                      T
                                                                                                                                            dB)
    of the sample so as to produce the required stress level                                                U                                        U                      (3)
                                                                                               Re
    everywhere of the sample. The measurement is performed
                                                                                                     B                   
    according to ASTM standard V3.04A341. B-coil is used for
    flux density measurement. Hall probes are put next to the
                                                                                              +(    0   
                                                                                                            ( H T )  dB)
                                                                                                                          U
                                                                                                                             det(G )]dudv
   Equation (4) and (5) are the expansion of equation (3) for                                                                 i +1
the diagonal reluctivity tensor case and the full reluctivity
                                                                                                                                                                                      B
tensor case respectively [4,5].                                                                                                        Be
                                                                                                                   Fig. 3 Derivative of element permeability to stress
            R
 e                       '
Fms    =            (( xx ( )B x2   +   '        2
                                            yy ( ) BY )
                 e
                                                                                     (4)                 Lets assume that the element equivalent stress and the
                E
                          det (G ))dudv                                                              element flux density obtained after performing one magneto-
        (1 +  )(1  2 )                                                                            mechanical coupled FEM analysis is  e (  i <  e <  i +1 ) and
                                                                                                      Be .  i and  i +1 are the permeability corresponding to Be at
                                                                                                     stress level  i and  i +1 respectively. They can be evaluated
         
 e                   '
Fms =           (( xx ( )Bx2 +  xy
                                    '
                                       ( ) Bx B y
            Re                                                                                       using any kind of nonlinear interpolation method. Linear
                                                                                           (5)
         +  'yx ( ) Bx B y +  'yy ( ) BY2 )
                                                          E
                                                                    det (G )) dudv
                                                                                                     interpolation is used to calculate the element permeability  e .
                                                  (1 +  )(1  2 )                                  Thus the permeability of this element  e and the derivative of
                                                                                                     the permeability component to the element stress can be
     Where, xx , xy , yx and                yy'
                     '     '      '                                                                  calculated as follows:
                                                      are the derivatives of the
corresponding components of the reluctivity to the element                                                                                              i +1   e
stress, which is obtained from the coupled solution.                                                                                              i +1 +           i
                                                                                                       i  e      e                                e i
                                                                                                                 = i                  , e =                                                     (8)
                                                                                                      e   i +1  e   i +1                          e
A.    e  Calculation                                                                                                                            1 + i +1
                                                                                                                                                        e i
  Fig. 2 shows the magnetostriction effects on the
magnetization property of ferromagnetic materials.                                                   For diagonal reluctivity tensor,
                                                                                                                                                                       e
                 B                    Highest stress                                                                                                   e
                                                                                                                                                     xx            yy         e  0
                                                                                                     If  e   0   e   1 , then                        e
                                                                                                                                                                =        e
                                                                                                                                                                             =              ;
                                                                                                                                                                              e  0
                                                        Stress level (i+1)                                                                                             e
                                                                                                                                                      e
                                                                                                                                                    xx             yy         1  e
                                                            Stress level (i)                         If  e   0 >  e   1 , then                            =            =
                                                                                                                                                     e             e         1  e
                                                                                                                                                                                                 (6)
                                             Without stress
                                             Initial magnetic property                                  Since the full tensor magnetization property of the steel
                                                                                                     sheet is not available, the following formula is used as a
                                                                                                     replacement for the full tensor reluctivity case [4,5].
                                                                        H
                                                                                                 4
   e
 yy                           e + 0                                                     (x4, y4) (fx4,fy4)                             (x3, y3) (fx3, fy3)
      e
          = sin( B +  ph )                                         (14)
                              e 0
If  e   0 >  e   1 , then                                                                                            (xc, yc)
                                                                                                                  C4                       C3
   e
 xx                         e  1
          = cos( B +  ph )                                         (15)
  e                        1   e
   e
                                                                                                                         (fxe,fye)
 xy                         e  1                                                                           C1
          = sin( B +  ph )                                         (16)                                                                  C2
  e                        1   e
                                                                                          (x1, y1) (fx3, fy3)
   e
 yx                        + e
          = sin( B +  ph ) 1                                       (17)                                                                  (x2, y2) (fx2 fy2)
  e                       1   e
   e
 yy                           1 + e                                                                     Fig. 4 Nodal force calculation
      e
          = cos( B +  ph )                                         (18)
                             1   e
                                                                                                             c1
                                                                                  ( fx1 , fy1 ) =                        ( fxe , fy e )                          (22)
                                                                                                    c1 + c 2 + c3 + c 4
     Where  B are the inclination angle of the flux density,  ph
                                                                                                              c2
are the phase angle between the flux density B and the field                      ( fx 2 , fy 2 ) =                       ( fxe , fy e )                         (23)
                                                                                                     c1 + c 2 + c3 + c 4
strength H .                                                                                                 c3
                                                                                  ( fx3 , fy3 ) =                         ( fxe , fy e )                         (24)
                                                                                                     c1 + c 2 + c3 + c 4
B.      det (G ) Calculation
                                                                                                              c4
    The local Jacobian derivatives matrix G and its determinate                   ( fx 4 , fy 4 ) =                       ( fxe , fy e )                         (25)
                                                                                                     c1 + c 2 + c3 + c 4
used for the triangular element can be found in the published
literatures [2]. The authors of this paper deduce the formula for
calculating G and its determinate of quadrilateral elements.                           Where, ( x c , y c ) and        ( fxe , fye )   represent the coordinate
They are given below.                                                             and the element magnetostrictive force value at the element
                                                                                  physical center of one quadrilateral element, shown in Fig. 4.
                   x     y                                                       ( fx1 , fy1 ) , ( fx 2 , fy 2 ) , ( fx3 , fy3 ) , and ( fx 4 , fy 4 ) are the nodal
     det[G ] = G = u
                         u = x y  y x                         (19)         magnetostrictive force contributed by one element. c1, c2, c3,
                   x     y   u v u v                                        and c4 are the distances between each node and the physical
                   v     v                                                      center.
                                                                                       The total nodal magnetostriction force is obtained by adding
x y  N1      N        N        N                                          the elemental nodal magnetostriction force from all elements
     =  x1 + x2 2 + x3 3 + x4 4  
u v  u        u        u        u                                         around one node.
                                                                    (20)
       N1      N 2      N 3      N 4 
       y1  + y2      + y3      + y4                                             D.      Coupled analysis procedure
       v        v        v        v 
                                                                                      The element permeability is determined according to the
y x  N1       N     N    N                                                nonlinear magnetization properties as well as the stress level of
     =  y1  + y2 2 + y3 3 + y4 4  
u v  u         u     u    u                                               each element. Using the magnetization property without any
                                                                    (21)
       N1      N     N    N                                                 stress applied carries out the initial strong-coupled solution.
       x1  + x2 2 + x3 3 + x4 4                                                 Then the iteration for the proper element permeability and
       v        v     v    v 
                                                                                  stress determination is performed until the energy of the whole
                                                                                  system keeps unchanged. Usually several times coupled FE
   Where, N1 , N 2 , N 3 and N 4 are the interpolation functions
                                                                                  analyses are needed for the convergent iterations.
of quadrilateral element. (x1, y1 ) , (x2, y2 ) , (x3 , y3 ) and (x4 , y4 )
are the coordinates of the four nodes.                                                                   RESULTS AND CONCLUSION
C.    Nodal force summation                                                           A PM surface mounted motor is used for the application of
   The calculated Fmse
                        is the magnetostrictive force acted on                    the proposed method and the procedure. With our results, the
                                                                                  following conclusions can be obtained.
one element. In order to know its contribution to the force at
each node, it should be distributed. Below gives the
                                                                                  1.    If the virtual work principle is adopted for the magnetic
formulations used for this purpose.
                                                                                        force calculation and the magnetostriction effects are
                                                                                        considered, there are forces distributed inside the stator
                                                                                        iron. Fig. 5 and Fig. 6 show the force distribution along a
                                                                              5
                  round locus at the back iron with and without                                                             3.    If the full reluctivity tensor is considered, the magnetic
                  magnetostriction effects considered. No force appears in                                                        force profiles along any round locus of the stator iron will
                  the back iron in Fig. 6 is due to the application of the                                                        not be repeated. So are the displacements. This is already
                  virtual work principle. The result in Fig.5 shows that there                                                    shown in Fig. 5, 7 and can be further confirmed by the Fig.
                  exists force density in the back iron if the magnetostriction                                                   8 below.
                  effects are taken into account.
                                                                                                                                      9.E-07
                                                                                                                                      8.E-07
                   2.E+01
                                                                                                                                      7.E-07
                   2.E+01
                                                                                                                                      6.E-07
                   2.E+01                                                                                                             5.E-07
2.E+01 4.E-07
1.E+01 3.E-07
9.E+00 2.E-07
                                                                                                                                      1.E-07
                   6.E+00
                                                                                                                                      0.E+00
                   3.E+00
                                                                                                                                               0   25   50   75   105   130    155     180    205     230   255   280   305   330   355
0.E+00 A ngl e ( de gr e e )
3 27 53 78 102 127 153 177 203 227 253 277 303 327 353
A ngl e ( de gr e e )
                  Fig. 5         Magnetic force at the back iron at radius 0.100531m with                                    Fig. 8 Displacement at the teeth shank at radius 0.084624m with (unrepeated
                                            magnetostriction effects                                                                 curve) and without (repeated curve) magnetostriction effects
7.E-01
                  6.E-01
      Force (N)
5.E-01
4.E-01
3.E-01
2.E-01
1.E-01
                  0.E+00
                            3    27   53   78   102   127   153    177      203     227   253   277   303   327   353
                                                                Angle (degree)
                  0.E+00
                            2    28   52   78   102 128 152        178 202 228            252 278 302       328 352
                                                                Angle (degree)