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TRANSFORMER     TECHNOLOGY




     Prof. Chandrabhan Sharma
TRANSFORMER TECHNOLOGY

WINDINGS
     Material →       * mainly Cu
                      * Al also used
Insulation: Most common      -       Paper
                             -       paper board (Press Board)

Some cases     - Wood (laminated varnish impregnated),
               - Synthetic enamel.

     Fluid insulant provides two (2) functions:

               -       inter-part insulation

               -       removal of heat
-   Oil mainly used

-   Air/SF6 for dry type. (H2 also used in the past)

-   Oil dielectric breakdown → 40 kV

            test using 2 kV/s voltage between 13mm spheres
            spaced 2.5mm apart.
DRY TYPE INSULATING MATERIALS




  Note :   Most Air transformer are type C

  Conductors are usually Cu or Al

       Form     :   Wire, strip, foil, sheets

               Choice of form f(current)
WINDING TYPE

                           •Helical (high ‘I’; low ‘V’)
      Construction         •Crossover (low ‘I’; high ‘V’)
                           •Mulitlayer HV (V ≥ 132 kV)
                           •Continuous Disc (Arc Furnaces)

  Note:
  Because of poor space factor, wire only found in coils of distribution
  and instrumentation transformers.




                                                           - No space problem
                                                           - Less wire needed
                                                           - More efficient
TAPPINGS

     Depending on MVA rating, tap position can be selected so as to
     offset out-of-balance conditions.

Losses:
          -    I2R

          -    Eddy current

          -    Losses in clamps (leakage flux)

          -    Tank Losses (due to tank being magnetic)
TRANSFORMER CORES
Materials : Iron-silicon alloys used for power transformers.

Produced by cold rolling process which causes crystals to
align along the direction of rolling.




                 a - silectron
                 b - unisil
Insulating Materials:

     Magnesia is added to the core surface during manufacture.

     Then given a coat of acid phosphates prior to annealing.

     This is sufficient for cores up to 30 MVA.


   Additional insulation can be:

           -       Paper

           -       Mixtures of china, clay and flour

           -       Varnishes
FORM
(1)Cross-section:

  Windings for core are cylindrical in shape → circular fill.

               ⇒ core section should be circular

(2)Pattern:
Clamping (of Laminations) :

Disadvantages:

  -    Bolts are potential source of core faults.

  -    Bolt must be well insulated, else cooling slots have to be
       provided.

       -         This causes increase in flux densities and iron losses.

       -         Complications of punching process.

       -         Eddy current losses.

  -    Difficult getting optimum cross-sectional areas. (Bolt heads,
       insulation and stiffening plates).
LOSSES

  Building factor ≅ actual losses
    (B.F.)          ideal losses

               Design is to get B.F. → 1
               Core joints cause B.F. >1

NOISE:

  Source is the core, caused by longitudinal mangnetostrictive
  vibrations of the iron.

Flatness and proper bending strain, when clamped, will reduce noise.
TRANSFORMER REPRESENTATION

Winding connections suppress 3rd harmonic voltages by providing path
for 3rd harmonic current to flow.

Equipment ckt: (Two winding)




                  xm >> Ƶp, Ƶs
           xm, magnetizing impedance neglected
THREE WINDING




Only earthed star connection and delta connection allow I0 currents
to flow by providing a path.

** Unearthed star connection does not allow I0 to flow.
STAR CONNCETION (Unearthed)




STAR CONNCETION (Earthed)
Y/DELTA CONNECTION (With Star point unearthed)
Let       Ƶoc = Ƶm                    ( xm >> Ƶp )


      ∴   Ƶsc = Ƶp + Ƶs               for 2 winding transformer


For 3 winding transformer

          Ƶsc can be either
                  (i)         Secondary (s) is grounded or

                  (ii)        Tertiary (t) is grounded

For (i)           →           Ƶsc = Ƶps = Ƶp + Ƶs


or (ii)           →           Ƶsc = Ƶpt = Ƶp + Ƶt
From which we can write:



               Ƶp=½[Ƶps + Ƶpt – Ƶst]


               Ƶs=½[Ƶps + Ƶst – Ƶpt]


And

               Ƶt=½[Ƶpt + Ƶst – Ƶps]


       where Ƶst = Ƶs + Ƶt


Ƶst → read as impedance seen from the secondary with the
tertiary short-circuited.
AUTO TRANSFORMERS

Consider YY∆ transformer earthed through Ƶe.
                          np 1               np
    Let ratios be :          =           and    =1
                          ns   n             nt

Then the unit current into primary is:
For the secondary:

                      ∴        VƵe = (1-n) Ƶe
                                Ƶe

                      ∴        Ƶsn = (1-n) Ƶe
                           Referring to primary

                            ⇒ Ƶsu = [(1-n)/n2 ]( Ƶe )

                     (where Vp is the base voltage)




                       Ƶtu = Ƶe/n


                      pu
Zero Sequence Equivalent circuit becomes
For a Generator solidly earthed with a 3 winding auto-transformer
we have, as seen from the secondary:




                                                 n - 1          3Z 
                                ( Zg + Z p ) + 3       Ze  Z t + e 
                 1 - n                          n               n 
i.e. Z 0 = Zs + 3       Ze + 
                   n                            n - 1            3Z
                                  (Zg + Z p ) + 3       Ze + Z t + e
                                                  n                 n
 (Zg + Z p )                       (Zg + Z p )         (Zg + Z p )                 2

                    Zs +
                           Z t Zs                                                    n -1 
                                + 3Zs + 
                                                       Z t + 3
                                                                      2
                                                                             + 3Z t       
            Ze              Ze                  Ze                   n               n 
 Z0 =                                                
                                     (Zg + Z p ) Z t
                                                 +      +3
                                         Ze        Ze

        but Z e >> Zg , Z p , Zs , Z t

                                         (Zg + Z p )         n −1 
                                                                       2

                      ⇒ Z 0 ≅ Zs +                     + Zt       
                                             n2               n 


   Or in terms of short circuit impedances
                                                                           2
     1                       1                             1  n −1
Z 0 = [Z ps + Zst − Z pt ] + 2 [2Zg + Z ps + Z pt − Zst ] −        [ Z pt + Zst − Z ps ]
     2                      2n                             2 n 

                               Z ps  n -1          1 - n  Zg
   OR                  Z0 =   + Zst        + Z pt  2  + 2
                            n        n             n  n
POWER TRANSFORMERS

RATING:

       Flux Density in core limited for 3 reasons

   (i) Heating of core

   (ii) Introduction of current or voltage harmonics

   (iii) Excessive magnetizing current in one or more windings

⇒ Limit on number of volts/turn

     Maximum voltage which may be applied is limited to 105%
     of rating!!
**     The current carrying capacity of a winding is limited by
       heating due to resistive losses.


 Windings normally capable of carrying up to 105 % of rated current



Example:
               For a winding rated ± 10 %
               rating on –10 % of tap ≃ 110% plus 5 % over-rating.


∴ Current carrying capacity = 115 %
For the + 10% tap -:

        Voltage rating/capability = 110 % V

        Also current rating/capability = 110 % I
                ∴Capability of transformer = 121% rating

N.B.
  This rating cannot be utilised because the untapped winding is
  limited to 100 % i.e. rated MVA.

   Present practice is to specify transformer ratio/turns ratio/voltage
   ratio at no load.

   Similarly tapping range is in terms of turns ratio at no load.
CAPACITIVE VOLTAGE TRANSFORMERS

As system voltage rise, insulation cost of wound transformers
become prohibitive.

→       C.V.T used in these cases where

                        V ≥ 132 kV

The capacitor divider can also be used as the coupler for PLC
(Power Line Carrier) signal; hence costs reduced.

Accuracies of better than 1 % for operating frequency range (for 50
Hz system can be 47≤ f ≤ 51)
To achieve this performance in a capacitor divider very large
capacitance would be required.

Problem simplified if source capacitance tuned to the mid- frequency
by a series reactor.

Further alleviation obtained if divider reduces voltage to an
intermediate value (10 ∼ 22 kV) and then a standard wire wound
transformer is used to step this down to 110 V.
Circuit Arrangement




Performance controlled by
   (1) C1


  (2) Magnitude of intermediate voltage (VI)
Equivalent circuit referred to primary becomes:




  Where:
                 Vp = system phase voltage
                 k = C1/(C1+C2)
           C1 + C2 = effective source capacitance
               Req = equivalent resistance referred to primary
kVp R eq
Output voltage = Vout =                                     ........................(1)
                                              1        
                           R eq + j ωL1 −
                                          ω(C1 + C 2 ) 
                                                        

  For resonance :
                          1                                 1
             ω0 L1 =                        or   ω L1 =
                                                  2
                                                  0
                     ω0 (C1 + C 2 )                     (C1 + C 2 )

      Sub into (1)
                                    kVp R eq
             ⇒ Vout =
                                           ω ω0 
                           R eq + j ω0 L1 
                                          ω − ω 
                                                 
                                            0   

                                      kVp
                       =
                                  ω0 L1  ω ω0 
                           1+ j         
                                        ω − ω 
                                               
                                  R eq  0     
- Vout + Vin kVp − Vo
But error =             =
                Vin        kVp
              Vo
         =1-
             kVp




                                 Vo    1
  ∴maximum error = f(D) ⇒           =
                                kVp 1 + jD
Vo      1       1
           or          =        =
                   kVp   1 + jD   1 + D2

or 1 + D 2 ≅    1 + error       (as error gets small)

Where D governs the maximum acceptable error.
                               ω   ω0 
Let this frequency deviation =  ω − ω 
                                      
                                0     

This has a maximum value (δ) at ω0


       Req is determined by maximum load Wmax
                                      (kVp ) 2
                 i.e.        Wmax =
                                       R eq
     δ       Wmax 
  ⇒D=                      
      ω (C + C )  (kV ) 2 
                                                                     2
                                 or Wmax = Dω0 (C1 + C 2 ) k 2 Vp
      0 1     2      p    




Since D, ω0, Vp and δ are fixed


        ⇒       maximum burden            ∝     C1 and k


Since, due to cost, necessary to keep C1 and k as small as possible.
Example:
Vphase = 275 kV ; k = 1/25


        error = 0.5 % ; frequency range = 51.5 – 47.5
Soln:

For frequency range
                       51.5 + 47.5
              ⇒ ω0 =               = 49.5
                            2

                      51.5 49.5 
                ∴δ =      −      = 0.08
                      49.5 51.5 

                  Wmax = 200 VA (given)
magnitude of error = 1 + D 2

              = 1 + 0.005


∴          1 +D2 ≑1.01

           D2 = 0.01           ⇒   D = 0.1




                                         ≑ 500pf
C.V.T. Transient Response
C3 – stray capacitance of E.M. unit


R1- loss of tuning cct.


Req – includes loss in magnetizing inductance L2


This is a band-pass network with an upper and lower resonant
frequency.

(a)     For the higher frequency, Ceq is low compared to L1 and L2
        and high compared to C3.


                 For lower frequency reverse is true.
HIGH FREQUENCY c.c.t.




    for p = j 2 πfu = jωu − Complex frequency

                                           
                                           
       kVp              1                       R eq      
       p 
 Vo =                                  
                                                       '     
                             R eq            1 + pC 2 R eq 
                                                              
              R 1 + pL1 +
             
                                          
                            1 + pC 2 R eq  
                                    '
                    
                                         
 kVp             
                                  
                                              R eq             
                                                               
        ⇒ Vo = 
                p               
                                  R + (R + pL )(1 + pC ' R ) 
                                 eq    1    1        2   eq 

Looking at denominator →
                             '                 '            '
R eq + (R 1 + pL1 )(1 + pC 2 R eq ) = p 2 L1C 2 R eq + p[C 2 R 1R eq + L1 ] + R 1 + R eq

                             '            2       2
                      = L1C 2 R eq  p 2 +  p + ω h 
                                                     
                                          T        
                                2     R 1 + R eq
                      where ω h =           '
                                                 and
                                      L1C 2 R eq
                                   2 R1      1
                                    =   +    '
                                   T L1   C 2 R eq
                                                   2
                            1   1      2
          roots are : α1 = −  +   −ω h
                            T   T 
                                                   2
                               1   1      2
                        α 2 = −  −   −ω h
                               T   T 
2
                               2    1
       For oscillation : ω h       > 
                                    T
                                     R eq +  1 
                                              R
                                             2                R1
                                                                   2
                                                                             1
       ⇒                                                 >         +
                                              '                    2        2
                                       L1C 2 R eq               L1        '
                                                                       C 2 R eq
                                                                                2


                           True for high R eq


(i)     R eq = 0
                ⇒ transfer function is pL1 + R 1
                                                  Simple exponential transient

(ii)    R eq = ∞
                                                1
                                                      and T = ( L1 R 1 )
                                      2                                  2
                   ⇒                ωh =            '
                                              L1C 2
LOW FREQUENCY c.c.t




                          pL 2 R eq         
                                            
               kVp        pL + R 
                           2        eq       
          Vo =
                p          1      pL 2 R eq   
                    R1 +       +              
                           pC1 pL 2 + R eq
                              '
                                              
                                              
kVp pL 2 R eq
  Vo =
                1 
          pR 1 + '  (pL 2 + R eq ) + p 2 L 2 R eq
                C1 
                   

Looking at the denominator it can be re-written as:
                                       L2  
                           p R 1R eq + '  
                             
                      p 2 +            C1  
                                               +         R eq
 (R 1L 2 + R eq L 2 )
                            L 2 (R 1 + R eq )         '
                                                  L 2 C1 (R 1 + R eq )
                                              
                      
                                              
                                               
                                L2
                     R 1R eq + '
      2                       C1             R 11       1
  Let   =                               =         + '
      T            L 2 (R 1 + R eq )         L 2 C1 (R 1 + R eq )
                                                      R 1R eq
                            where R 11 =
                                                  (R 1 + R eq )
2                    R eq
       and ω L =                    '
                         L1C1 (R 1 + R eq )

       Roots are :

                                                   2
                               1   1      2
                         α1 = −  +   −ω L
                               T   T 

                                                   2
                               1   1      2
                        α 2 = −  −   −ω L
                               T   T 

For oscillation:
                                               2
                                         1
                       ( ωL )   2
                                        > 
                                         T 
This yields:

                                                                 1                       
                               2       2
         R eq               R 1 R eq                 1                      R 1R eq
                     >                      +                  +                         
                                              4C1 (R 1 + R eq ) 2  L 2 C1 (R 1 + R eq ) 
     '                     2                      2                       '             2 
L1C1 (R 1 + R eq )     4L 2 (R 1 + R eq ) 2     '
                                                                  


                                                      2       2
              1                  1               R 1 R eq            1
or                          R eq − R 11  >                    +
     L 2 C1 (R 1 + R eq ) 
           '                                  2                    '2
                                         4L 2 (R 1 + R eq )
                                                             2
                                 2                              4C1 (R 1 + R eq )


     Again, oscillation occurs for large Req.

     Compromise in design between Ceq i.e. (C1+C2) and accuracy of
     response required.

     Generally, a large as possible value of C1 and k is used.
SURGES ON TRANSFORMER WINDING
Initial Voltage Distribution




                Assuming that the capacitance is uniformly
                distributed along the winding
                Define: l = length of winding

                        Cg = total capacitance to ground

                         Cs = total series capacitance
Cg
 ∇                ground capacitance/unit length =
                                                      l
and               series capacitance/unit length = Cs l

     Let:           E = voltage to ground at any point in the winding

                    Ig = total current in the ground capacitance

                    Is = total currents in the series capacitance

     Consider an elementary length of winding ∆x
                                            Cg 
       ∴              Capacitance/ground =  ∆x
                                            l 
                                            
      ∴              Current through this capacitance :
                                     C g ∆xωE
                              ∆I g =          ..................................(1)
                                          l
dI s
But                        ∆I g =        ∆x..................................(2)
                                    dx
Combining (1) and (2)


                            dI s C g ωE
              ⇒                 =       ..................................(3)
                            dx      l
                                                    l Cs
But the series capacitance of unit winding is
                                                     ∆x

                                         dE
and the voltage across the element =        ∆x............................(4)
                                         dx

                                                  dE
  and current in the series capacitance = C          = ............................(5)
                                                  dt
dE
Sub. into (3)   ⇒         Is = l Cs ω       ..................................(6)
                                         dx
                                      dI s         d 2E
Differentiating equation (6)        ⇒      = l Cs ω 2 ..................................(7)
                                      dx           dx
                           C g ωE           d 2E
From (3) and (7)     ⇒              = l Cs ω 2 ..................................(8)
                              l             dx

                          d 2E   1 Cg
or                           2
                               − 2    E = 0..................................(9)
                          dx     l Cs
Equation (9) is independent of ω and has a solution in the form


                E = A1e bx + A 2 e -bx .........................................(10)

                                                        1
                                       1  Cg          2
                              where b =  
                                       l  Cs 
Solving for A1 and A2 using the boundary conditions:

                   x=0      ⇒       E=0       Grounded
                                              neutral
And                x=l      ⇒       E=V
           where V is the amplitude of the step function surge

   Sub. Into (10) ⇒             A1 + A2 = 0


                                A1e bl + A 2 e -bl = V

                                                 V
      or                         A1 = - A 2 = bl
                                             e − e -bl
1
                  Cg 
                      2
Let         bl =   = α
                  Cs 

                              V
           A1 = - A 2 =            ...............................(11)
                           2 sinh α

                                          V
      Sub. (11) into (10) ⇒ E =                 [e bx - e -bx ]
                                       2 sinh α


                          ∴ E=V
                                         sinh α x( l)
                                           sinh α
      For isolated neutral the boundary conditions are :

                      x=l          ;            E=V
                                                                       dE
      and             x=0          ;            Is = 0            or      =0
                                                                       dx
⇒             b(A1 - A 2 ) = 0


                      A1e bl + A 2 e -bl = V.............................(12)

From which we get :
                            V         V
             A1 = A 2 =           =         .........................(13)
                        2 cosh(bl) 2 cosh α


                                               V
         Sub. (13) into (10) ⇒ E =                   [e bx + e -bx ]
                                            2 cosh α


                                        =V
                                             cosh α x ( l)
                                                cosh α
(a) Grounded Neutral :
                                    ( )
                                     x
                         dE α cosh α l
                           = V
                         dx l   sinh α

                            dE αV
for x = l      ⇒               =   cothα
                            dx   l
(b) Isolated Neutral :
                                    ( )
                                     x
                         dE α sinh α l
                           = V
                         dx l   cosh α

                            dE αV
for x = l        ⇒             =   tanhα
                            dx   l
WINDING OSCILLATIONS




                                         Cg
Let the capacitance/unit length = C1 =
                                         l

Looking at a length ∆x ⇒ the capacitance to ground = C1.∆x

       Let the interturn capacitance = C 2 /length
                           or         = bC 2 [for length of turn = b]

       Let                 L1 = self inductance/unit - length
                                = L1.∆x [for elementary unit]


       And for one turn with length ' b' = bL1
∴ within the limits, the induced voltage is

                 ∂I                ∂E    ∂I                                    Where I is the
        ∂E = L      ∂x     or         = L .......................(1)
                 ∂t                ∂x    ∂t                                    current flowing



                                                              ∂E
   Also, the capacitance to ground for one turn = bC1            ............................(a)
                                                              ∂t


    Capacitance current to turn 2 from turn 1 is
                                           ∂     ∂E 
                                = b C2           ∂x  b ............................(2)
                                           ∂t    1,2


                                           ∂     ∂E 
   and from turn 3 is           = - b C2         ∂x  b ............................(3)
                                           ∂t     2,3
 ∂E     ∂E   ∂ E  b
                                                 2
     It is known that :      ∂x  =  ∂x  +  ∂x 2  . 2 ............................(4a)
                             1,2    2           2


                             ∂E     ∂E   ∂ E  b
                                                 2
    and                      ∂x  =  ∂x  −  ∂x 2  . 2 ............................(4b)
                              2,3   2           2


            ∂ 2E 
     where  2  = space rate of change of voltage gradient at conductor 2
            ∂x  2

Sub. (4a) and (4b) into (2) and (3) gives the net charging current from adjacent turns


                ∂      ∂E   ∂ 2 E  b     ∂   ∂E   ∂ 2 E  b 
    i.e.   bC 2         +  2  . .b - bC 2    −  2  . .b
                ∂t     ∂x  2  ∂x  2 2 
                                             ∂t   ∂x  2  ∂x  2 2 
                                                                       

                                        ∂ 3E
                                 = C2b   3
                                               ............................(5)
                                       ∂t ∂x 2
Subtract from this the capacitance current to ground (a), we have
     the net rate of change of the total current per turn length

                           ∂I       3 ∂ E
                                        3
                                                   ∂E
                        -b    = C2b          - C1b    ............................(6)
                           ∂x        ∂t ∂x 2
                                                   ∂t

               [-ve because ' x' is measured from the neutral]

        Differentiating (1) w.r.t. x
                                         ∂ 2I   1 ∂ 2E
                    ⇒                         =        ............................(7)
                                        ∂x∂t    L ∂x 2



Differentiating (6) w.r.t. ' t'
                              ∂ 2I             ∂ 4E       ∂ 2E
            ⇒                      = - C2b 2
                                                      + C1 2 ............................(8)
                             ∂x∂t            ∂t ∂x
                                               2    2
                                                          ∂t
Equating (7) and (8)
                        1 ∂ 2E              ∂ 4E ∂ 2E
                  ⇒            = - C 2 b 2 2 + C1 2
                                        2

                        L ∂x 2
                                          ∂t ∂x  ∂t

                           ∂ 2E      ∂ 2E          ∂ 4E
          or                    − LC1 2 + LC2 b 2 2 = 0................(9)
                                               2

                           ∂x 2
                                     ∂t          ∂t ∂x

Sub :             E = Vγ e jωt e j γ x


From which ⇒ - γ 2 + LC1ω 2 + LC2 b 2 γ 2 ω 2 = 0

                                                             1/ 2
                                            LC1ω      2
                or                       γ=                
                                           1 - LC2 b 2 ω 2 


                                                    γ
               and                       ω=
                                            (LC1 + LC2 b 2 γ 2 )1/ 2
From the denominator for ' γ'


             ⇒ if          LC2 b 2 ω 2 > 1   then γ is imaginary


        This corresponds to a critical frequency ω c such that
                                       1
                                ωc =
                                     b LC2



Therefore, the winding behaves like a filter blocking all frequencies > ωc
FLOW CHART FOR THE FIELD INSTALLATION OF TRANSFORMERS
FIELD DRYING OF TRANSFORMER INSULATION

Residual water content < 0.5 % of wt. of paper insulation

Method #1 :- CIRCULATING HOT OIL (Slow process)

Requirements:

        (a) Oil Filter → either vacuum drier type or blotter press.

        (b) Heater suitable of raising oil temp to 85oC
Procedure:

     - Fill transformer to top of core with oil.

     - Circulate oil through filter with heater on.

     - Reduce heat losses by:
          - Close off radiators
          - Blanket outside of transformer tank.

     - Continue circulation until dryness is achieved.

N.B. The rate of drying can be increased by application of a vacuum to
     the surface of the oil!
Method #2 :-    Short – Circuited Windings: Vacuum (Most Rapid
                Method)

Requirements:

       -        Power source to drive current thru transformer
                coil/winding → heating source [winding temperature <
                95oC

       -        Vacuum Pump

       -        Refrigerated condenser trap in vacuum line.(this serves
                to collect/condensed extracted moisture)

       -        Blanket the outside of transformer tank so as to
                minimise heat loss.
Procedure:-

      -       Transformer filled with oil above core and coil
              allowing room for expansion.

      -       Vacuum pump connected to suitable valve at top
              of tank.

      -       With one winding s/c, connect supply to other.
              Circulate current up to FLC. [Winding temperature not
              to exceed 95oC]

      -       For forced cooled transformer, oil pumps should
              be operating → however, radiators should be off.
Procedure:-(cont’d)

           -   After desired temperatures reached, disconnect supply
               and drain oil.

       -       Start vacuum pump and continue until water extraction
               ceases.

       -       Repeat procedure if necessary to achieve desired
               dryness.

N.B.
       Water extraction will stop WHEN the V.P. of water in the
       insulation equals the partial pressure of water vapour in the
       tank at the prevailing temperature and pressure.
Method #3 :- Using High Vacuum (Specially suited for EHV T/F)

Requirements:

       -        Vacuum pump capable of vacuum of <7 Pa absolute.

       -        Cold trap to collect moisture.

       -        Possibly additional heat may be required.

       -        Transformer must be designed to withstand full
                vacuum.
Procedure:-
       -       Drain oil while at same time fill with nitrogen (dry)

       -       Remove heat exchangers and external pipe connections

       -       Install cold trap as close to the transformer as possible

       -       Seal transformer and pressure test for leaks

N.B.
       Water extraction from the facilities start when the
       residual vapour pressure in tank is less than v.p. of
       water insulation.

       -       Vacuum maintained in the order of 1mm Hg (130 pa)

       -       End point is when the rate of water condensate in the
               cold trap is less than 3g/hr per 1000kg of insulation wt.
Method #4: -Using Hot Air (Hazardous)

Tank should first be blanketed in order to minimize heat required (loss)

Procedure:-

Volume of Hot Air Required
Area of Base (m2)              2.8  5.6     11.6      14.0
Volume of Air (m3/min)         28   56      114       140
_______________________________________________________________
i.e →   Volume Required (m3/min) =  10 (Area of tank base m3)
___________________________________________________________
         -       Clean dry hot air is blown through air opening at
                 base of tank, over coils exiting at top.

         -       Temperature of inlet and outlet streams noted
                 (Temperature of inlet should be ≃ 100oC)

 Note: Fire hazard as flash point for transformer oil is 145oC.
Variation of winding (R & p.f.) with drying time (t)


N.B.: As soon as the transformer is considered dry, it should
be     immediately filled with oil to cover the core and
windings
Vacuum Treatment prior to oil filling


Principal function of vacuum treatment is to remove trapped
air/moisture from the insulation so that the insulation can achieve
full dielectric strength.


For     V ≤ 345 kv → Vacuum used ≈ 5mmHg
        V > 345 kv → Vacuum used ≃ 1mmHg


Vacuum should be held for 4 hours or more as per manufacturers
instruction.
PRE-ENERGIZATION TESTING:-

        -        Insulation resistance tests (megger)

        -        Power factor test → windings, bushings

        -        Ratio test

        -        Operation of attached auxiliary parts and sensors

        -        Dielectric strength, power factor of oil

        -        O2 content and total combustible gas content of
                 Nitrogen Gas Cushion

After energizing, the transformer should “soak” unloaded for 8 hours.
TESTING (BS 171)

Routine Test → All transformers are subjected to these:

        -       Voltage Ratio and polarity

        -       Winding resistance

        -       Impedance voltage, s/c impedance and load test

        -       Dielectric tests

        -       No-load losses

        -       On-load tap changer where installed.
TYPE TESTS

Test made on one transformer is representative of all.

        -       Temperature-rise test

        -       Lightning Impulse test
SPECIAL TESTS

   As agreed between vendor and purchaser

     -       Dielectric test

     -       Zero sequence Impedance (3-phase t/f only)

     -       s/c test

     -       Acoustic sound level

     -       Magnetizing on no load

     -       Power taken by auxiliaries ( fans, pumps etc.)

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TRANSFORMER TECHNOLOGY FUNDAMENTALS

  • 1. TRANSFORMER TECHNOLOGY Prof. Chandrabhan Sharma
  • 2. TRANSFORMER TECHNOLOGY WINDINGS Material → * mainly Cu * Al also used Insulation: Most common - Paper - paper board (Press Board) Some cases - Wood (laminated varnish impregnated), - Synthetic enamel. Fluid insulant provides two (2) functions: - inter-part insulation - removal of heat
  • 3. - Oil mainly used - Air/SF6 for dry type. (H2 also used in the past) - Oil dielectric breakdown → 40 kV test using 2 kV/s voltage between 13mm spheres spaced 2.5mm apart.
  • 4. DRY TYPE INSULATING MATERIALS Note : Most Air transformer are type C Conductors are usually Cu or Al Form : Wire, strip, foil, sheets Choice of form f(current)
  • 5. WINDING TYPE •Helical (high ‘I’; low ‘V’) Construction •Crossover (low ‘I’; high ‘V’) •Mulitlayer HV (V ≥ 132 kV) •Continuous Disc (Arc Furnaces) Note: Because of poor space factor, wire only found in coils of distribution and instrumentation transformers. - No space problem - Less wire needed - More efficient
  • 6. TAPPINGS Depending on MVA rating, tap position can be selected so as to offset out-of-balance conditions. Losses: - I2R - Eddy current - Losses in clamps (leakage flux) - Tank Losses (due to tank being magnetic)
  • 7. TRANSFORMER CORES Materials : Iron-silicon alloys used for power transformers. Produced by cold rolling process which causes crystals to align along the direction of rolling. a - silectron b - unisil
  • 8. Insulating Materials: Magnesia is added to the core surface during manufacture. Then given a coat of acid phosphates prior to annealing. This is sufficient for cores up to 30 MVA. Additional insulation can be: - Paper - Mixtures of china, clay and flour - Varnishes
  • 9. FORM (1)Cross-section: Windings for core are cylindrical in shape → circular fill. ⇒ core section should be circular (2)Pattern:
  • 10.
  • 11. Clamping (of Laminations) : Disadvantages: - Bolts are potential source of core faults. - Bolt must be well insulated, else cooling slots have to be provided. - This causes increase in flux densities and iron losses. - Complications of punching process. - Eddy current losses. - Difficult getting optimum cross-sectional areas. (Bolt heads, insulation and stiffening plates).
  • 12. LOSSES Building factor ≅ actual losses (B.F.) ideal losses Design is to get B.F. → 1 Core joints cause B.F. >1 NOISE: Source is the core, caused by longitudinal mangnetostrictive vibrations of the iron. Flatness and proper bending strain, when clamped, will reduce noise.
  • 13. TRANSFORMER REPRESENTATION Winding connections suppress 3rd harmonic voltages by providing path for 3rd harmonic current to flow. Equipment ckt: (Two winding) xm >> Ƶp, Ƶs xm, magnetizing impedance neglected
  • 14. THREE WINDING Only earthed star connection and delta connection allow I0 currents to flow by providing a path. ** Unearthed star connection does not allow I0 to flow.
  • 15. STAR CONNCETION (Unearthed) STAR CONNCETION (Earthed)
  • 16. Y/DELTA CONNECTION (With Star point unearthed)
  • 17. Let Ƶoc = Ƶm ( xm >> Ƶp ) ∴ Ƶsc = Ƶp + Ƶs for 2 winding transformer For 3 winding transformer Ƶsc can be either (i) Secondary (s) is grounded or (ii) Tertiary (t) is grounded For (i) → Ƶsc = Ƶps = Ƶp + Ƶs or (ii) → Ƶsc = Ƶpt = Ƶp + Ƶt
  • 18. From which we can write: Ƶp=½[Ƶps + Ƶpt – Ƶst] Ƶs=½[Ƶps + Ƶst – Ƶpt] And Ƶt=½[Ƶpt + Ƶst – Ƶps] where Ƶst = Ƶs + Ƶt Ƶst → read as impedance seen from the secondary with the tertiary short-circuited.
  • 19. AUTO TRANSFORMERS Consider YY∆ transformer earthed through Ƶe. np 1 np Let ratios be : = and =1 ns n nt Then the unit current into primary is:
  • 20. For the secondary: ∴ VƵe = (1-n) Ƶe Ƶe ∴ Ƶsn = (1-n) Ƶe Referring to primary ⇒ Ƶsu = [(1-n)/n2 ]( Ƶe ) (where Vp is the base voltage) Ƶtu = Ƶe/n pu
  • 21. Zero Sequence Equivalent circuit becomes
  • 22. For a Generator solidly earthed with a 3 winding auto-transformer we have, as seen from the secondary:   n - 1   3Z   ( Zg + Z p ) + 3  Ze  Z t + e  1 - n   n    n  i.e. Z 0 = Zs + 3  Ze +   n   n - 1 3Z (Zg + Z p ) + 3  Ze + Z t + e  n  n
  • 23.  (Zg + Z p )   (Zg + Z p )  (Zg + Z p ) 2   Zs + Z t Zs  n -1    + 3Zs +   Z t + 3  2 + 3Z t   Ze Ze Ze n  n  Z0 =     (Zg + Z p ) Z t + +3 Ze Ze but Z e >> Zg , Z p , Zs , Z t (Zg + Z p )  n −1  2 ⇒ Z 0 ≅ Zs + + Zt   n2  n  Or in terms of short circuit impedances 2 1 1 1  n −1 Z 0 = [Z ps + Zst − Z pt ] + 2 [2Zg + Z ps + Z pt − Zst ] −   [ Z pt + Zst − Z ps ] 2 2n 2 n  Z ps  n -1   1 - n  Zg OR Z0 = + Zst   + Z pt  2  + 2 n  n   n  n
  • 24. POWER TRANSFORMERS RATING: Flux Density in core limited for 3 reasons (i) Heating of core (ii) Introduction of current or voltage harmonics (iii) Excessive magnetizing current in one or more windings ⇒ Limit on number of volts/turn Maximum voltage which may be applied is limited to 105% of rating!!
  • 25. ** The current carrying capacity of a winding is limited by heating due to resistive losses. Windings normally capable of carrying up to 105 % of rated current Example: For a winding rated ± 10 % rating on –10 % of tap ≃ 110% plus 5 % over-rating. ∴ Current carrying capacity = 115 %
  • 26. For the + 10% tap -: Voltage rating/capability = 110 % V Also current rating/capability = 110 % I ∴Capability of transformer = 121% rating N.B. This rating cannot be utilised because the untapped winding is limited to 100 % i.e. rated MVA. Present practice is to specify transformer ratio/turns ratio/voltage ratio at no load. Similarly tapping range is in terms of turns ratio at no load.
  • 27. CAPACITIVE VOLTAGE TRANSFORMERS As system voltage rise, insulation cost of wound transformers become prohibitive. → C.V.T used in these cases where V ≥ 132 kV The capacitor divider can also be used as the coupler for PLC (Power Line Carrier) signal; hence costs reduced. Accuracies of better than 1 % for operating frequency range (for 50 Hz system can be 47≤ f ≤ 51)
  • 28. To achieve this performance in a capacitor divider very large capacitance would be required. Problem simplified if source capacitance tuned to the mid- frequency by a series reactor. Further alleviation obtained if divider reduces voltage to an intermediate value (10 ∼ 22 kV) and then a standard wire wound transformer is used to step this down to 110 V.
  • 29. Circuit Arrangement Performance controlled by (1) C1 (2) Magnitude of intermediate voltage (VI)
  • 30. Equivalent circuit referred to primary becomes: Where: Vp = system phase voltage k = C1/(C1+C2) C1 + C2 = effective source capacitance Req = equivalent resistance referred to primary
  • 31. kVp R eq Output voltage = Vout = ........................(1)  1  R eq + j ωL1 −  ω(C1 + C 2 )   For resonance : 1 1 ω0 L1 = or ω L1 = 2 0 ω0 (C1 + C 2 ) (C1 + C 2 ) Sub into (1) kVp R eq ⇒ Vout =  ω ω0  R eq + j ω0 L1  ω − ω    0  kVp = ω0 L1  ω ω0  1+ j  ω − ω   R eq  0 
  • 32. - Vout + Vin kVp − Vo But error = = Vin kVp Vo =1- kVp Vo 1 ∴maximum error = f(D) ⇒ = kVp 1 + jD
  • 33. Vo 1 1 or = = kVp 1 + jD 1 + D2 or 1 + D 2 ≅ 1 + error (as error gets small) Where D governs the maximum acceptable error. ω ω0  Let this frequency deviation =  ω − ω     0  This has a maximum value (δ) at ω0 Req is determined by maximum load Wmax (kVp ) 2 i.e. Wmax = R eq
  • 34. δ  Wmax  ⇒D=    ω (C + C )  (kV ) 2  2  or Wmax = Dω0 (C1 + C 2 ) k 2 Vp  0 1 2  p  Since D, ω0, Vp and δ are fixed ⇒ maximum burden ∝ C1 and k Since, due to cost, necessary to keep C1 and k as small as possible.
  • 35. Example: Vphase = 275 kV ; k = 1/25 error = 0.5 % ; frequency range = 51.5 – 47.5 Soln: For frequency range 51.5 + 47.5 ⇒ ω0 = = 49.5 2  51.5 49.5  ∴δ =  −  = 0.08  49.5 51.5  Wmax = 200 VA (given)
  • 36. magnitude of error = 1 + D 2 = 1 + 0.005 ∴ 1 +D2 ≑1.01 D2 = 0.01 ⇒ D = 0.1 ≑ 500pf
  • 38. C3 – stray capacitance of E.M. unit R1- loss of tuning cct. Req – includes loss in magnetizing inductance L2 This is a band-pass network with an upper and lower resonant frequency. (a) For the higher frequency, Ceq is low compared to L1 and L2 and high compared to C3. For lower frequency reverse is true.
  • 39. HIGH FREQUENCY c.c.t. for p = j 2 πfu = jωu − Complex frequency      kVp  1   R eq   p  Vo =       '    R eq 1 + pC 2 R eq     R 1 + pL1 +   1 + pC 2 R eq   '    
  • 40.  kVp   R eq   ⇒ Vo =   p   R + (R + pL )(1 + pC ' R )    eq 1 1 2 eq  Looking at denominator → ' ' ' R eq + (R 1 + pL1 )(1 + pC 2 R eq ) = p 2 L1C 2 R eq + p[C 2 R 1R eq + L1 ] + R 1 + R eq '  2 2 = L1C 2 R eq  p 2 +  p + ω h     T   2 R 1 + R eq where ω h = ' and L1C 2 R eq 2 R1 1 = + ' T L1 C 2 R eq 2 1  1  2 roots are : α1 = −  +   −ω h T  T  2 1  1  2 α 2 = −  −   −ω h T  T 
  • 41. 2 2 1 For oscillation : ω h >  T R eq +  1  R  2 R1 2 1 ⇒   > + ' 2 2 L1C 2 R eq L1 ' C 2 R eq 2 True for high R eq (i) R eq = 0 ⇒ transfer function is pL1 + R 1 Simple exponential transient (ii) R eq = ∞ 1 and T = ( L1 R 1 ) 2 2 ⇒ ωh = ' L1C 2
  • 42. LOW FREQUENCY c.c.t   pL 2 R eq       kVp   pL + R   2 eq   Vo = p  1 pL 2 R eq   R1 + +  pC1 pL 2 + R eq '    
  • 43. kVp pL 2 R eq Vo =  1   pR 1 + '  (pL 2 + R eq ) + p 2 L 2 R eq  C1    Looking at the denominator it can be re-written as:   L2    p R 1R eq + '    p 2 +  C1    + R eq (R 1L 2 + R eq L 2 )  L 2 (R 1 + R eq )  ' L 2 C1 (R 1 + R eq )       L2 R 1R eq + ' 2 C1 R 11 1 Let   = = + ' T L 2 (R 1 + R eq ) L 2 C1 (R 1 + R eq ) R 1R eq where R 11 = (R 1 + R eq )
  • 44. 2 R eq and ω L = ' L1C1 (R 1 + R eq ) Roots are : 2 1  1  2 α1 = −  +   −ω L T  T  2 1  1  2 α 2 = −  −   −ω L T  T  For oscillation: 2 1 ( ωL ) 2 >  T 
  • 45. This yields: 1  2 2 R eq R 1 R eq 1 R 1R eq > + +   4C1 (R 1 + R eq ) 2  L 2 C1 (R 1 + R eq )  ' 2 2 ' 2  L1C1 (R 1 + R eq ) 4L 2 (R 1 + R eq ) 2 '  2 2 1  1  R 1 R eq 1 or R eq − R 11  > + L 2 C1 (R 1 + R eq )  ' 2 '2  4L 2 (R 1 + R eq ) 2  2 4C1 (R 1 + R eq ) Again, oscillation occurs for large Req. Compromise in design between Ceq i.e. (C1+C2) and accuracy of response required. Generally, a large as possible value of C1 and k is used.
  • 46. SURGES ON TRANSFORMER WINDING Initial Voltage Distribution Assuming that the capacitance is uniformly distributed along the winding Define: l = length of winding Cg = total capacitance to ground Cs = total series capacitance
  • 47. Cg ∇ ground capacitance/unit length = l and series capacitance/unit length = Cs l Let: E = voltage to ground at any point in the winding Ig = total current in the ground capacitance Is = total currents in the series capacitance Consider an elementary length of winding ∆x  Cg  ∴ Capacitance/ground =  ∆x  l    ∴ Current through this capacitance : C g ∆xωE ∆I g = ..................................(1) l
  • 48. dI s But ∆I g = ∆x..................................(2) dx Combining (1) and (2) dI s C g ωE ⇒ = ..................................(3) dx l l Cs But the series capacitance of unit winding is ∆x dE and the voltage across the element = ∆x............................(4) dx dE and current in the series capacitance = C = ............................(5) dt
  • 49. dE Sub. into (3) ⇒ Is = l Cs ω ..................................(6) dx dI s d 2E Differentiating equation (6) ⇒ = l Cs ω 2 ..................................(7) dx dx C g ωE d 2E From (3) and (7) ⇒ = l Cs ω 2 ..................................(8) l dx d 2E 1 Cg or 2 − 2 E = 0..................................(9) dx l Cs Equation (9) is independent of ω and has a solution in the form E = A1e bx + A 2 e -bx .........................................(10) 1 1  Cg  2 where b =   l  Cs 
  • 50. Solving for A1 and A2 using the boundary conditions: x=0 ⇒ E=0 Grounded neutral And x=l ⇒ E=V where V is the amplitude of the step function surge Sub. Into (10) ⇒ A1 + A2 = 0 A1e bl + A 2 e -bl = V V or A1 = - A 2 = bl e − e -bl
  • 51. 1  Cg  2 Let bl =   = α  Cs  V  A1 = - A 2 = ...............................(11) 2 sinh α V Sub. (11) into (10) ⇒ E = [e bx - e -bx ] 2 sinh α ∴ E=V sinh α x( l) sinh α For isolated neutral the boundary conditions are : x=l ; E=V dE and x=0 ; Is = 0 or =0 dx
  • 52. b(A1 - A 2 ) = 0 A1e bl + A 2 e -bl = V.............................(12) From which we get : V V A1 = A 2 = = .........................(13) 2 cosh(bl) 2 cosh α V Sub. (13) into (10) ⇒ E = [e bx + e -bx ] 2 cosh α =V cosh α x ( l) cosh α
  • 53. (a) Grounded Neutral : ( ) x dE α cosh α l = V dx l sinh α dE αV for x = l ⇒ = cothα dx l
  • 54. (b) Isolated Neutral : ( ) x dE α sinh α l = V dx l cosh α dE αV for x = l ⇒ = tanhα dx l
  • 55. WINDING OSCILLATIONS Cg Let the capacitance/unit length = C1 = l Looking at a length ∆x ⇒ the capacitance to ground = C1.∆x Let the interturn capacitance = C 2 /length or = bC 2 [for length of turn = b] Let L1 = self inductance/unit - length = L1.∆x [for elementary unit] And for one turn with length ' b' = bL1
  • 56. ∴ within the limits, the induced voltage is ∂I ∂E ∂I Where I is the ∂E = L ∂x or = L .......................(1) ∂t ∂x ∂t current flowing ∂E Also, the capacitance to ground for one turn = bC1 ............................(a) ∂t Capacitance current to turn 2 from turn 1 is ∂  ∂E  = b C2  ∂x  b ............................(2) ∂t  1,2 ∂  ∂E  and from turn 3 is = - b C2  ∂x  b ............................(3) ∂t   2,3
  • 57.  ∂E   ∂E   ∂ E  b 2 It is known that :  ∂x  =  ∂x  +  ∂x 2  . 2 ............................(4a)  1,2  2  2  ∂E   ∂E   ∂ E  b 2 and  ∂x  =  ∂x  −  ∂x 2  . 2 ............................(4b)   2,3  2  2  ∂ 2E  where  2  = space rate of change of voltage gradient at conductor 2  ∂x  2 Sub. (4a) and (4b) into (2) and (3) gives the net charging current from adjacent turns ∂   ∂E   ∂ 2 E  b  ∂   ∂E   ∂ 2 E  b  i.e. bC 2    +  2  . .b - bC 2    −  2  . .b ∂t   ∂x  2  ∂x  2 2    ∂t   ∂x  2  ∂x  2 2    ∂ 3E = C2b 3 ............................(5) ∂t ∂x 2
  • 58. Subtract from this the capacitance current to ground (a), we have the net rate of change of the total current per turn length ∂I 3 ∂ E 3 ∂E -b = C2b - C1b ............................(6) ∂x ∂t ∂x 2 ∂t [-ve because ' x' is measured from the neutral] Differentiating (1) w.r.t. x ∂ 2I 1 ∂ 2E ⇒ = ............................(7) ∂x∂t L ∂x 2 Differentiating (6) w.r.t. ' t' ∂ 2I ∂ 4E ∂ 2E ⇒ = - C2b 2 + C1 2 ............................(8) ∂x∂t ∂t ∂x 2 2 ∂t
  • 59. Equating (7) and (8) 1 ∂ 2E ∂ 4E ∂ 2E ⇒ = - C 2 b 2 2 + C1 2 2 L ∂x 2 ∂t ∂x ∂t ∂ 2E ∂ 2E ∂ 4E or − LC1 2 + LC2 b 2 2 = 0................(9) 2 ∂x 2 ∂t ∂t ∂x Sub : E = Vγ e jωt e j γ x From which ⇒ - γ 2 + LC1ω 2 + LC2 b 2 γ 2 ω 2 = 0 1/ 2  LC1ω  2 or γ=  1 - LC2 b 2 ω 2  γ and ω= (LC1 + LC2 b 2 γ 2 )1/ 2
  • 60. From the denominator for ' γ' ⇒ if LC2 b 2 ω 2 > 1 then γ is imaginary This corresponds to a critical frequency ω c such that 1 ωc = b LC2 Therefore, the winding behaves like a filter blocking all frequencies > ωc
  • 61. FLOW CHART FOR THE FIELD INSTALLATION OF TRANSFORMERS
  • 62. FIELD DRYING OF TRANSFORMER INSULATION Residual water content < 0.5 % of wt. of paper insulation Method #1 :- CIRCULATING HOT OIL (Slow process) Requirements: (a) Oil Filter → either vacuum drier type or blotter press. (b) Heater suitable of raising oil temp to 85oC
  • 63. Procedure: - Fill transformer to top of core with oil. - Circulate oil through filter with heater on. - Reduce heat losses by: - Close off radiators - Blanket outside of transformer tank. - Continue circulation until dryness is achieved. N.B. The rate of drying can be increased by application of a vacuum to the surface of the oil!
  • 64. Method #2 :- Short – Circuited Windings: Vacuum (Most Rapid Method) Requirements: - Power source to drive current thru transformer coil/winding → heating source [winding temperature < 95oC - Vacuum Pump - Refrigerated condenser trap in vacuum line.(this serves to collect/condensed extracted moisture) - Blanket the outside of transformer tank so as to minimise heat loss.
  • 65. Procedure:- - Transformer filled with oil above core and coil allowing room for expansion. - Vacuum pump connected to suitable valve at top of tank. - With one winding s/c, connect supply to other. Circulate current up to FLC. [Winding temperature not to exceed 95oC] - For forced cooled transformer, oil pumps should be operating → however, radiators should be off.
  • 66. Procedure:-(cont’d) - After desired temperatures reached, disconnect supply and drain oil. - Start vacuum pump and continue until water extraction ceases. - Repeat procedure if necessary to achieve desired dryness. N.B. Water extraction will stop WHEN the V.P. of water in the insulation equals the partial pressure of water vapour in the tank at the prevailing temperature and pressure.
  • 67. Method #3 :- Using High Vacuum (Specially suited for EHV T/F) Requirements: - Vacuum pump capable of vacuum of <7 Pa absolute. - Cold trap to collect moisture. - Possibly additional heat may be required. - Transformer must be designed to withstand full vacuum.
  • 68. Procedure:- - Drain oil while at same time fill with nitrogen (dry) - Remove heat exchangers and external pipe connections - Install cold trap as close to the transformer as possible - Seal transformer and pressure test for leaks N.B. Water extraction from the facilities start when the residual vapour pressure in tank is less than v.p. of water insulation. - Vacuum maintained in the order of 1mm Hg (130 pa) - End point is when the rate of water condensate in the cold trap is less than 3g/hr per 1000kg of insulation wt.
  • 69. Method #4: -Using Hot Air (Hazardous) Tank should first be blanketed in order to minimize heat required (loss) Procedure:- Volume of Hot Air Required Area of Base (m2) 2.8 5.6 11.6 14.0 Volume of Air (m3/min) 28 56 114 140 _______________________________________________________________ i.e → Volume Required (m3/min) = 10 (Area of tank base m3) ___________________________________________________________ - Clean dry hot air is blown through air opening at base of tank, over coils exiting at top. - Temperature of inlet and outlet streams noted (Temperature of inlet should be ≃ 100oC) Note: Fire hazard as flash point for transformer oil is 145oC.
  • 70. Variation of winding (R & p.f.) with drying time (t) N.B.: As soon as the transformer is considered dry, it should be immediately filled with oil to cover the core and windings
  • 71. Vacuum Treatment prior to oil filling Principal function of vacuum treatment is to remove trapped air/moisture from the insulation so that the insulation can achieve full dielectric strength. For V ≤ 345 kv → Vacuum used ≈ 5mmHg V > 345 kv → Vacuum used ≃ 1mmHg Vacuum should be held for 4 hours or more as per manufacturers instruction.
  • 72. PRE-ENERGIZATION TESTING:- - Insulation resistance tests (megger) - Power factor test → windings, bushings - Ratio test - Operation of attached auxiliary parts and sensors - Dielectric strength, power factor of oil - O2 content and total combustible gas content of Nitrogen Gas Cushion After energizing, the transformer should “soak” unloaded for 8 hours.
  • 73. TESTING (BS 171) Routine Test → All transformers are subjected to these: - Voltage Ratio and polarity - Winding resistance - Impedance voltage, s/c impedance and load test - Dielectric tests - No-load losses - On-load tap changer where installed.
  • 74. TYPE TESTS Test made on one transformer is representative of all. - Temperature-rise test - Lightning Impulse test
  • 75. SPECIAL TESTS As agreed between vendor and purchaser - Dielectric test - Zero sequence Impedance (3-phase t/f only) - s/c test - Acoustic sound level - Magnetizing on no load - Power taken by auxiliaries ( fans, pumps etc.)