\[ \begin{align*} \frac{\underline{U}_1}{\underline{U}_2}=\frac{N_1}{N_2}=n, \qquad \frac{\underline{I}_1}{\underline{I}_2}=-\frac{1}{n} \end{align*} \] with a clear sign convention.
Well, again
For checking your understanding please do the quick checks in the exercise section.
\[ \begin{align*} \text{higher voltage} \quad \Longleftrightarrow \quad \text{lower current} \end{align*} \]
In EEE1 we considered magnetic flux \(\Phi\), flux linkage \(\Psi\), and induction. For one coil with \(N\) turns the flux linkage is
\[ \begin{align*} \Psi = N\Phi . \end{align*} \]
Faraday's law gives
\[ \begin{align*} u(t)=\frac{{\rm d}\Psi}{{\rm d}t}=N\frac{{\rm d}\Phi}{{\rm d}t}. \end{align*} \]
In sinusoidal steady state this becomes the phasor equation
\[ \begin{align*} \underline{U}=j\omega\underline{\Psi}=j\omega N\underline{\Phi}. \end{align*} \]
This is the starting point for the transformer.
\[ \begin{align*} \underline{U}=j\omega N\underline{\Phi} \end{align*} \]
with
\[ \begin{align*} [\omega\Phi]={\rm s}^{-1}\cdot {\rm Wb} ={\rm s}^{-1}\cdot {\rm V\,s} ={\rm V}. \end{align*} \]
The number of turns \(N\) is dimensionless.
Before we look at the transformer, we need one important idea:
The flux created by coil \(1\) can be split into
\[ \begin{align*} \Phi_{11} = \Phi_{21} + \Phi_{\rm S1}. \end{align*} \]
The voltage induced in coil \(2\) is
\[ \begin{align*} u_{{\rm ind},2}(t) = -N_2\frac{{\rm d}\Phi_{21}}{{\rm d}t}. \end{align*} \]
Imagine two pistons connected by an air duct.
For coupled coils:
The analogy is not perfect, but it helps to remember: coupling is strong when much of the field of one coil also passes through the other coil.
For a single coil we already know
\[ \begin{align*} \Psi=L i . \end{align*} \]
For two coupled coils, each flux linkage can depend on both currents:
\[ \begin{align*} \Psi_1 &= L_{11}i_1 + M_{12}i_2, \\ \Psi_2 &= M_{21}i_1 + L_{22}i_2. \end{align*} \]
For most transformer calculations we use the symmetric case
\[ \begin{align*} M_{12}=M_{21}=M. \end{align*} \]
Then
\[ \begin{align*} \boxed{ \begin{pmatrix} \Psi_1\\ \Psi_2 \end{pmatrix} = \begin{pmatrix} L_{11} & M\\ M & L_{22} \end{pmatrix} \begin{pmatrix} i_1\\ i_2 \end{pmatrix} } \end{align*} \]
and
\[ \begin{align*} M=k\sqrt{L_{11}L_{22}}. \end{align*} \]
Here \(k\) is the coupling coefficient.
<tabcaption tab_coupling_coefficient|Meaning of the coupling coefficient \(k\)>
| Coupling coefficient | Interpretation | Typical example |
|---|---|---|
| \(k=0\) | no useful flux from one coil links the other coil | coils far apart |
| \(0<k<1\) | partial coupling | wireless charger with air gap or misalignment |
| \(k\approx 1\) | almost all useful flux links both coils | transformer with iron core |
| sign of \(k\) | depends on winding direction and reference arrows | dot convention |
The sign of the mutual term depends on the winding direction and on the chosen current reference arrows.
For positive coupling:
\[ \begin{align*} u_1 &= L_{11}\frac{{\rm d}i_1}{{\rm d}t} + M\frac{{\rm d}i_2}{{\rm d}t}, \\ u_2 &= M\frac{{\rm d}i_1}{{\rm d}t} + L_{22}\frac{{\rm d}i_2}{{\rm d}t}. \end{align*} \]
For negative coupling, the sign of \(M\) is negative in the chosen equation system.
In wireless charging, the transmitter coil and receiver coil are separated by an air gap. The coupling coefficient \(k\) is much smaller than in a transformer with an iron core.
If the receiver is misaligned, less flux from the transmitter passes through it. Then \(M\) decreases, the induced voltage decreases, and the transmitted power decreases.
We now use the magnetic circuit model from EEE1, but only with magnetic reluctance \(R_{\rm m}\). No inverse magnetic quantity is needed here.
The magnetic voltage, also called magnetomotive force, is
\[ \begin{align*} \Theta=N i . \end{align*} \]
For a magnetic path with reluctance \(R_{\rm m}\), Hopkinson's law is
\[ \begin{align*} \Theta=R_{\rm m}\Phi \qquad \Longleftrightarrow \qquad \Phi=\frac{\Theta}{R_{\rm m}}. \end{align*} \]
\[ \begin{align*} \text{electric:}\quad U=R I \qquad \text{magnetic:}\quad \Theta=R_{\rm m}\Phi \end{align*} \]
For two windings on the same main magnetic path, the total magnetic voltage is
\[ \begin{align*} \Theta = N_1\underline{I}_1 + N_2\underline{I}_2. \end{align*} \]
The main flux is
\[ \begin{align*} \underline{\Phi} = \frac{\Theta}{R_{\rm mH}} = \frac{N_1\underline{I}_1+N_2\underline{I}_2}{R_{\rm mH}}. \end{align*} \]
The flux linkages are
\[ \begin{align*} \underline{\Psi}_1 &= N_1\underline{\Phi} = \frac{N_1^2}{R_{\rm mH}}\underline{I}_1 + \frac{N_1N_2}{R_{\rm mH}}\underline{I}_2, \\ \underline{\Psi}_2 &= N_2\underline{\Phi} = \frac{N_1N_2}{R_{\rm mH}}\underline{I}_1 + \frac{N_2^2}{R_{\rm mH}}\underline{I}_2. \end{align*} \]
Therefore
\[ \begin{align*} \boxed{ L_{1{\rm H}}=\frac{N_1^2}{R_{\rm mH}} } \qquad \boxed{ L_{2{\rm H}}=\frac{N_2^2}{R_{\rm mH}} } \qquad \boxed{ M=\frac{N_1N_2}{R_{\rm mH}} } \end{align*} \]
for an ideal common magnetic path.
\[ \begin{align*} M=\frac{N_1N_2}{R_{\rm mH}} \end{align*} \]
with
\[ \begin{align*} [R_{\rm mH}] = \frac{{\rm A}}{{\rm Vs}} = \frac{1}{{\rm H}}. \end{align*} \]
Thus
\[ \begin{align*} [M]=\frac{1}{1/{\rm H}}={\rm H}. \end{align*} \]
For an ideal transformer we assume:
Let \(N_1\) be the number of turns of the primary winding and \(N_2\) the number of turns of the secondary winding.
\[ \begin{align*} \underline{\Psi}_1 &= N_1\underline{\Phi}, & \underline{U}_1 &= j\omega\underline{\Psi}_1 = j\omega N_1\underline{\Phi}, \\ \underline{\Psi}_2 &= N_2\underline{\Phi}, & \underline{U}_2 &= j\omega\underline{\Psi}_2 = j\omega N_2\underline{\Phi}. \end{align*} \]
Dividing the two voltage equations gives the turns ratio
\[ \begin{align*} \boxed{ \frac{\underline{U}_1}{\underline{U}_2} = \frac{N_1}{N_2} = n } \end{align*} \]
with
\[ \begin{align*} n=\frac{N_1}{N_2}. \end{align*} \]
With the indicated reference arrows and a lossless transformer:
\[ \begin{align*} \underline{U}_1\underline{I}_1+\underline{U}_2\underline{I}_2=0 \end{align*} \]
and therefore
\[ \begin{align*} \boxed{ \frac{\underline{I}_1}{\underline{I}_2} = -\frac{\underline{U}_2}{\underline{U}_1} = -\frac{N_2}{N_1} = -\frac{1}{n} } \end{align*} \]
The minus sign is not a “loss”. It is caused by the chosen current arrows. The primary side absorbs power while the secondary side delivers power to the load.
A transformer has \(N_1=800\) turns and \(N_2=80\) turns. The primary RMS voltage is \(U_1=230~{\rm V}\).
\[ \begin{align*} n &= \frac{N_1}{N_2} = \frac{800}{80} =10, \\ U_2 &= \frac{U_1}{n} = \frac{230~{\rm V}}{10} =23~{\rm V}. \end{align*} \]
If the secondary side supplies \(I_2=4~{\rm A}\), the ideal primary current magnitude is
\[ \begin{align*} I_1 &= \frac{I_2}{n} = \frac{4~{\rm A}}{10} =0.4~{\rm A}. \end{align*} \]
The apparent power is equal on both sides:
\[ \begin{align*} S_1 &= U_1I_1=230~{\rm V}\cdot 0.4~{\rm A}=92~{\rm VA}, \\ S_2 &= U_2I_2=23~{\rm V}\cdot 4~{\rm A}=92~{\rm VA}. \end{align*} \]
In a real transformer, not all flux links both windings.
The real flux linkage equations become
\[ \begin{align*} \underline{\Psi}_1 &= L_1\underline{I}_1+M\underline{I}_2, & L_1&=L_{1{\rm H}}+L_{1\sigma}, \\ \underline{\Psi}_2 &= L_2\underline{I}_2+M\underline{I}_1, & L_2&=L_{2{\rm H}}+L_{2\sigma}. \end{align*} \]
The winding resistances \(R_1\) and \(R_2\) cause copper losses:
\[ \begin{align*} P_{\rm Cu,1}=R_1I_1^2, \qquad P_{\rm Cu,2}=R_2I_2^2. \end{align*} \]
In the following formulas:
\[ \begin{align*} \underline{U}_1 &= \underbrace{{\color{red}{R_1\underline{I}_1}}}_{\text{primary copper drop}} + \underbrace{{\color{orange}{j\omega L_{1\sigma}\underline{I}_1}}}_{\text{primary leakage drop}} + \underbrace{{\color{blue}{j\omega L_{1{\rm H}}\underline{I}_1+j\omega M\underline{I}_2}}}_{\text{main magnetic coupling}}, \\[6pt] \underline{U}_2 &= \underbrace{{\color{red}{R_2\underline{I}_2}}}_{\text{secondary copper drop}} + \underbrace{{\color{orange}{j\omega L_{2\sigma}\underline{I}_2}}}_{\text{secondary leakage drop}} + \underbrace{{\color{blue}{j\omega L_{2{\rm H}}\underline{I}_2+j\omega M\underline{I}_1}}}_{\text{main magnetic coupling}}. \end{align*} \]
With the leakage reactances
\[ \begin{align*} X_{1\sigma}=\omega L_{1\sigma}, \qquad X_{2\sigma}=\omega L_{2\sigma}, \qquad X_{\rm M}=\omega M \end{align*} \]
these equations can be represented by an equivalent circuit.
\[ \begin{align*} X_{1\sigma}=\omega L_{1\sigma} \end{align*} \]
with
\[ \begin{align*} [\omega L]={\rm s}^{-1}\cdot{\rm H} = {\rm s}^{-1}\cdot \frac{{\rm V\,s}}{{\rm A}} = \Omega . \end{align*} \]
So \(jX_{1\sigma}\) is an impedance.
A robot axis may draw a high current during acceleration. This high current produces a voltage drop at the leakage reactance and winding resistance of the transformer.
Possible effects:
So leakage is not only a “field theory detail”. It directly affects the electrical behavior of the machine.
For calculations it is convenient to move all secondary-side quantities to the primary side. This is called referring or transforming the secondary side to the primary side.
\[ \begin{align*} \boxed{ \underline{U}'_2=n\underline{U}_2 } \qquad \boxed{ \underline{I}'_2=\frac{1}{n}\underline{I}_2 } \end{align*} \]
The secondary resistance and leakage reactance are transformed by \(n^2\):
\[ \begin{align*} \boxed{ R'_2=n^2R_2 } \qquad \boxed{ X'_{2\sigma}=n^2X_{2\sigma} } \end{align*} \]
The turns ratio \(n\) is dimensionless. Therefore
\[ \begin{align*} [R'_2]=[n^2R_2]=\Omega . \end{align*} \]
The value changes, but the unit does not.
In the reduced equivalent circuit:
Once all quantities are referred to one side, the transformer can be calculated like an AC network with impedances. This uses the same method as complex network calculation: replace components by impedances and apply Kirchhoff's laws.
No-load operation means that the secondary side is open:
\[ \begin{align*} \underline{I}_2=0. \end{align*} \]
The primary side still draws a small no-load current \(\underline{I}_{10}\). This current has two parts:
\[ \begin{align*} \underline{I}_{10} = \underline{I}_{\rm Fe} + \underline{I}_{\rm m}. \end{align*} \]
The technical voltage ratio is often defined from the no-load voltages. Here it is denoted by \(\ddot{u}\):
\[ \begin{align*} \ddot{u} = \frac{\text{higher voltage}}{\text{lower voltage}} \bigg|_{\rm no~load}. \end{align*} \]
For a step-down transformer:
\[ \begin{align*} \ddot{u} = \frac{U_{1{\rm N}}}{U_{20}}. \end{align*} \]
Here \(U_{1{\rm N}}\) is the rated primary voltage and \(U_{20}\) is the open-circuit secondary voltage.
\[ \begin{align*} \ddot{u}\neq n, \end{align*} \]
but for many practical transformers
\[ \begin{align*} \ddot{u}\approx n. \end{align*} \]
In the short-circuit test, the secondary side is shorted:
\[ \begin{align*} \underline{U}_2=0. \end{align*} \]
Because the required primary voltage is small, the magnetizing branch is often neglected:
\[ \begin{align*} X_{1{\rm H}},\;R_{\rm Fe} \gg X'_{2\sigma},\;R'_2. \end{align*} \]
This gives the short-circuit equivalent circuit with
\[ \begin{align*} \boxed{ R_{\rm k}=R_1+R'_2 } \qquad \boxed{ X_{\rm k}=X_{1\sigma}+X'_{2\sigma} } \end{align*} \]
and
\[ \begin{align*} \underline{Z}_{\rm k} = R_{\rm k}+jX_{\rm k}. \end{align*} \]
The rated short-circuit voltage \(U_{1{\rm k}}\) is the primary voltage that must be applied while the secondary side is shorted so that rated primary current \(I_{1{\rm N}}\) flows.
As a relative value:
\[ \begin{align*} \boxed{ u_{\rm k} = \frac{U_{1{\rm k}}}{U_{1{\rm N}}}\cdot 100~\% } \end{align*} \]
Small \(u_{\rm k}\) means: small internal impedance and high possible fault current. Large \(u_{\rm k}\) means: stronger current limitation and larger voltage drop under load.
The continuous short-circuit current for rated primary voltage is
\[ \begin{align*} \boxed{ I_{1{\rm k}} = \frac{U_{1{\rm N}}}{U_{1{\rm k}}}\cdot I_{1{\rm N}} = I_{1{\rm N}}\cdot \frac{100~\%}{u_{\rm k}} } \end{align*} \]
where \(u_{\rm k}\) is inserted as a percentage value.
\[ \begin{align*} u_{\rm k} = \frac{U_{1{\rm k}}}{U_{1{\rm N}}}\cdot 100~\% \end{align*} \]
is dimensionless. It is usually stated in percent.
The RMS short-circuit current \(I_{1{\rm k}}\) does not describe the highest instantaneous current.
When a short circuit starts, the current can contain
The worst case occurs when the fault starts at an unfavorable phase angle. Then the first current peak is larger than the normal sinusoidal peak \(\sqrt{2}I_{1{\rm k}}\).
A common engineering form is
\[ \begin{align*} i_{\rm p} = \kappa\sqrt{2}\,I''_{\rm k}. \end{align*} \]
Here
For a strongly inductive transformer short circuit, a practical approximation is
\[ \begin{align*} \kappa\approx 1.8. \end{align*} \]
Then
\[ \begin{align*} i_{\rm p} \approx 1.8\cdot\sqrt{2}\cdot I_{1{\rm k}} = 2.55\,I_{1{\rm k}} \approx 2.54\,I_{1{\rm k}}. \end{align*} \]
The factor \(2.54\) is an engineering approximation for the first peak current. It is not a universal transformer law.
For real protection design, use the applicable standard, manufacturer data, and the actual \(R/X\) ratio of the installation.
Under load, the short-circuit equivalent circuit is often sufficient for engineering estimates.
\[ \begin{align*} \underline{U}_{\rm k} = \left(R_{\rm k}+jX_{\rm k}\right)\underline{I}_1. \end{align*} \]
This voltage drop is subtracted vectorially from the primary-side voltage relation. Therefore the secondary voltage depends on
In a robot with motors, the supply transformer may show a lower output voltage during high acceleration because the motor currents increase. The Kapp triangle helps estimate this voltage drop. This is important for:
Transformer behavior is influenced by construction.
Cooling types:
<tabcaption tab_transformer_types|Typical transformer types, short-circuit voltage, and secondary voltage>
| Name / use | Typical \(u_{\rm k}\) | Secondary voltage \(U_2\) | Important note |
|---|---|---|---|
| Power transformer | \(4\ldots 12~\%\) | application-dependent | low voltage drop, high fault currents possible |
| Isolating transformer | \(\approx 10~\%\) | max. \(250~{\rm V}\) | galvanic isolation for safety and measurement |
| Toy transformer | \(\approx 20~\%\) | max. \(24~{\rm V}\) | current limitation is desired |
| Doorbell transformer | \(\approx 40~\%\) | max. \(12~{\rm V}\), often several taps | simple robust low-voltage supply |
| Ignition transformer | \(\approx 100~\%\) | \(\leq 14~{\rm kV}\) | high voltage, limited current |
| Welding transformer | \(\approx 100~\%\) | max. \(70~{\rm V}\) | large current, strong current limitation |
| Voltage transformer | \(<1~\%\) | \(100~{\rm V}\) | operate with high load resistance, approximately no-load |
| Current transformer | \(100~\%\) | \(0~{\rm V}\) ideal secondary voltage | operate with low burden, approximately short-circuit |
A current transformer secondary must not be opened while primary current flows. If the secondary circuit is open, the transformer tries to maintain the magnetic balance and can generate dangerous high voltages.
A transformer has \(N_1=1200\) turns and \(N_2=300\) turns. The primary RMS voltage is \(U_1=230~{\rm V}\). The secondary side supplies a load current \(I_2=2.0~{\rm A}\).
\[ \begin{align*} n=\frac{N_1}{N_2} = \frac{1200}{300} = 4. \end{align*} \]
The secondary voltage is
\[ \begin{align*} U_2 = \frac{U_1}{n} = \frac{230~{\rm V}}{4} = 57.5~{\rm V}. \end{align*} \]
The primary current magnitude is
\[ \begin{align*} I_1 = \frac{I_2}{n} = \frac{2.0~{\rm A}}{4} = 0.50~{\rm A}. \end{align*} \]
Because \(U_2<U_1\), it is a step-down transformer.
Two coils are wound on the same ideal magnetic core. The main magnetic reluctance is
\[ \begin{align*} R_{\rm mH}=2.0\cdot 10^6~\frac{1}{\rm H}. \end{align*} \]
The number of turns is \(N_1=500\) and \(N_2=100\).
\[ \begin{align*} L_{1{\rm H}} = \frac{N_1^2}{R_{\rm mH}} = \frac{500^2}{2.0\cdot 10^6~1/{\rm H}} = 0.125~{\rm H}. \end{align*} \]
\[ \begin{align*} L_{2{\rm H}} = \frac{N_2^2}{R_{\rm mH}} = \frac{100^2}{2.0\cdot 10^6~1/{\rm H}} = 0.0050~{\rm H} = 5.0~{\rm mH}. \end{align*} \]
\[ \begin{align*} M = \frac{N_1N_2}{R_{\rm mH}} = \frac{500\cdot 100}{2.0\cdot 10^6~1/{\rm H}} = 0.025~{\rm H} = 25~{\rm mH}. \end{align*} \]
The unit is correct because \(1/(1/{\rm H})={\rm H}\).
A transformer has \(n=5\). The secondary winding resistance is \(R_2=0.20~\Omega\) and the secondary leakage reactance is \(X_{2\sigma}=0.35~\Omega\).
Calculate the values \(R'_2\) and \(X'_{2\sigma}\) referred to the primary side.
\[ \begin{align*} R'_2 = n^2R_2 = 5^2\cdot 0.20~\Omega = 25\cdot 0.20~\Omega = 5.0~\Omega. \end{align*} \]
\[ \begin{align*} X'_{2\sigma} = n^2X_{2\sigma} = 5^2\cdot 0.35~\Omega = 25\cdot 0.35~\Omega = 8.75~\Omega. \end{align*} \]
The unit remains \(\Omega\), because \(n\) is dimensionless.
A transformer has a rated primary current \(I_{1{\rm N}}=10~{\rm A}\) and a short-circuit voltage \(u_{\rm k}=5~\%\).
\[ \begin{align*} I_{1{\rm k}} = I_{1{\rm N}}\cdot \frac{100~\%}{u_{\rm k}} = 10~{\rm A}\cdot \frac{100~\%}{5~\%} = 200~{\rm A}. \end{align*} \]
\[ \begin{align*} i_{\rm p} \approx 2.54\cdot I_{1{\rm k}} = 2.54\cdot 200~{\rm A} = 508~{\rm A}. \end{align*} \]
The short-circuit current is much larger than the rated current. Protection devices must be selected accordingly.
A single-phase transformer supplies an actuator driver. Rated data and equivalent circuit data are:
\[ \begin{align*} U_{1{\rm N}}&=230~{\rm V}, & U_{2{\rm N}}&=23~{\rm V}, & I_{2{\rm N}}&=5.0~{\rm A}, \\ R_1&=1.2~\Omega, & X_{1\sigma}&=1.8~\Omega, \\ R_2&=0.012~\Omega, & X_{2\sigma}&=0.018~\Omega. \end{align*} \]
Assume \(n=\frac{U_{1{\rm N}}}{U_{2{\rm N}}}\). The magnetizing branch is neglected for the loaded operating point.
The turns ratio is
\[ \begin{align*} n = \frac{U_{1{\rm N}}}{U_{2{\rm N}}} = \frac{230~{\rm V}}{23~{\rm V}} = 10. \end{align*} \]
The secondary quantities referred to the primary side are
\[ \begin{align*} R'_2 &= n^2R_2 = 10^2\cdot 0.012~\Omega = 1.2~\Omega, \\ X'_{2\sigma} &= n^2X_{2\sigma} = 10^2\cdot 0.018~\Omega = 1.8~\Omega. \end{align*} \]
Therefore
\[ \begin{align*} R_{\rm k} &= R_1+R'_2 = 1.2~\Omega+1.2~\Omega = 2.4~\Omega, \\ X_{\rm k} &= X_{1\sigma}+X'_{2\sigma} = 1.8~\Omega+1.8~\Omega = 3.6~\Omega. \end{align*} \]
The primary current magnitude is
\[ \begin{align*} I_{1{\rm N}} = \frac{I_{2{\rm N}}}{n} = \frac{5.0~{\rm A}}{10} = 0.50~{\rm A}. \end{align*} \]
The magnitude of the short-circuit impedance is
\[ \begin{align*} |\underline{Z}_{\rm k}| = \sqrt{R_{\rm k}^2+X_{\rm k}^2} = \sqrt{(2.4~\Omega)^2+(3.6~\Omega)^2} = 4.33~\Omega. \end{align*} \]
Thus the internal voltage drop estimate is
\[ \begin{align*} U_{\rm k} \approx |\underline{Z}_{\rm k}|I_{1{\rm N}} = 4.33~\Omega\cdot 0.50~{\rm A} = 2.17~{\rm V}. \end{align*} \]
This is a primary-side voltage drop. On the secondary side it corresponds approximately to
\[ \begin{align*} \frac{2.17~{\rm V}}{10}=0.217~{\rm V}. \end{align*} \]
For a \(23~{\rm V}\) actuator supply this is small but not zero.
Use this simulation to revisit the EEE1 idea that a changing magnetic flux induces voltage. This is the physical basis of the transformer equations in this block.
Use CircuitJS for qualitative experiments with coupled inductors and transformer circuits. Suggested activity: search the example circuits for “transformer”, change the turns ratio, and observe voltage and current.
Suggested experiment:
This is especially useful for understanding the difference between an iron-core transformer and loosely coupled wireless charging coils.
Relevant continuity pages: