1 Single and Three Phase Transformers and Power Flow Caution: In these experiments high voltages are involved, which could be harmful or fatal if one is exposed to them. Adhere to electrical safety rule at all times. Make sure that all of your connections are correct before turning on the power. A transformer is an electrical device that is used to raise or lower the voltage (or current) level. A single-phase transformer has two electrically isolated windings. The winding that is connected to the electrical power source is called the “primary” winding and the winding that is used to draw electrical power is called the “secondary” winding. Fig. 1 shows a schematic diagram of a singlephase transformer. Φm Figure 1: Schematic diagram of a single phase transformer. Let us examine the ideal transformer shown in Fig. 1 where, EP = induced voltage on the primary side (RMS) ES = induced voltage on the secondary side (RMS) NP = Number of turns on the primary windings NS = Number of turns on the secondary windings Syed A. Rizvi Summer’12-Revised Spring’16 ENS 441/ELT 437 2 Φm = magnetic flux created by the source voltage E When the primary winding is connected to an AC power source it produces an instantaneous magnetic flux “Φm (t)” linking the primary as well as secondary windings of the transformer. The flux linkage induces an instantaneous voltage “Ep (t)” in the primary winding in accordance with the Faraday’s law of electromagnetic induction. That is, πΈπ (π‘) = ππ π∅π (π‘) ππ‘ (1) Since the voltage applied at the primary is sinusoidal, therefore, the magnetic flux Φm (t) is also sinusoidal and mathematically it can be expressed as ∅π (π‘) = ∅πππ₯ sin ππ‘ (2) π∅π (π‘) π(sin ππ‘) = ππ × ∅πππ₯ ππ‘ ππ‘ (3) therefore, πΈπ (π‘) = ππ or πΈπ (π‘) = ππ × ∅πππ₯ × π cos ππ‘. (4) Substituting cos ππ‘ = sin(ππ‘ + 90π ) and π = 2ππ in Eq. 3 we get πΈπ (π‘) = 2ππ × ππ × ∅πππ₯ sin(ππ‘ + 90π ). (5) Eq. 4 shows that the induced voltage Ep (t) leads the magnetic flux Φm (t) by 90o. The RMS value of Ep (t), denoted by Ep is given by πΈπ = π ππ[πΈπ (π‘)] = |πΈπ (π‘)|πππ₯ √2 = 2ππ × ππ × ∅πππ₯ (6) √2 or πΈπ = 4.44 π × ππ × ∅πππ₯ . (7) Since the magnetic flux Φm (t) also links the secondary winding that has Ns turns, the RMS value of the induced voltage at the secondary side of the transformer, denoted by Es is given by πΈπ = 4.44 π × ππ × ∅πππ₯ . Syed A. Rizvi Summer’12-Revised Spring’16 (8) ENS 441/ELT 437 3 Comparing Eqs. (7) and (8) yields πΈπ πΈπ = 4.44 π × ππ 4.44 π × ππ (9) πΈπ πΈπ = ππ ππ (10) πΈπ ππ = =π πΈπ ππ (11) πΈπ = π × πΈπ (12) or or where, “a” is called the turn ratio of the transformer. Figure 2: An ideal transformer with a load on the secondary side. When secondary side is open (no load condition) under ideal conditions no current flows through the primary winding and the primary current “IP” is zero. When a load is connected to the secondary side (see Fig. 2), a current, Is, flows out of the secondary windings. The secondary current, Is, creates a magnetic flux “Φs” in the transformer’s core. Note that the source voltage, E, is unchanged, which mean the flux, Φm, must remain the same as it was before the load was connected. Therefore, the new flux (Φs) due to the secondary the current, Is, must be countered by an equal and opposite flux. The counter flux “Φp” is produced by causing a current, Ip, to flow into the primary windings. Under ideal conditions, the fluxes Φs and Φp cancel each other and the total flux through the core remains Φm. Therefore, the primary and secondary induced voltages (Ep and Es) remain unchanged. Syed A. Rizvi Summer’12-Revised Spring’16 ENS 441/ELT 437 4 The flow of the primary current, Ip, represents the power transfer from primary side to the secondary side of the transformer to support the load Zs. Under ideal conditions there is no loss of power during the power transfer from the primary side to the secondary side of the transformer. Therefore, the total power, Sp, on the primary side of the transformer must be equal to the total power, Ss, on the secondary side of the transformer, where ππ = πΈπ × πΌπ (13) ππ = πΈπ × πΌπ (14) πΈπ × πΌπ = πΈπ × πΌπ . (15) π × πΈπ × πΌπ = πΈπ × πΌπ (16) and but Sp = Ss, therefore, Combining Eqs. 12 and 14 yeilds or πΌπ = 1 × πΌπ . π (17) The load impedance as seen by the primary side, denoted by Zp, can be given by ππ = πΈπ π × πΈπ πΈπ = = π2 × 1 πΌπ πΌπ π × πΌπ (18) πΈπ πΌπ (19) but ππ = therefore, ππ = π2 × ππ . (20) Equation 20 shows an important property of the transformer; that is, it can be used to change the effective impedance of any load and thus can also act as an impedance transformer. Equation 20 is used to express impedances on the secondary side as the equivalent impedances on the primary side to greatly simplify the circuit analysis involving transformers (see Fig. 3). Syed A. Rizvi Summer’12-Revised Spring’16 ENS 441/ELT 437 5 Figure 3: An ideal transformer with the load shifted to the primary side. So far we have considered an ideal transformer with no primary current when there was no load attached to the secondary side. That is, the ideal transformer is lossless. In a real transformer, however, the primary current is not zero under no-load condition due to the “iron losses” and “magnetizing reactance” of the transformer. The iron losses are due to eddy currents and hysteresis losses (described below). Eddy Current Losses: When time-varying magnetic flux passes through a solid metal core, the solid metallic core acts like a bundle of concentric conductors and a voltage is induced in each of these sections of the metallic core. Note that in a solid metal plate each of these sections would behave like a shortcircuited conductor and, therefore, the induce voltages would cause a strong currents which swirl back and forth in the core. These currents are called eddy currents. Fig. 4 shows a cross-section of a solid metal core with circulating eddy currents. Eddy currents are a major source of generating heat in transformers. In a solid metal core these currents can be so strong that they render the core red hot. To minimize eddy current, cores are designed with thin laminated stripes instead of using a solid piece of metal. The lamination insulates the strips from each other, thus greatly reducing the length of the conducting path, which in turn, significantly reduces the magnitudes of the induced voltages in the core thereby diminishing eddy current losses. In general, eddy current losses are reduced proportional to the square of the number of strips used in the core. Figure 4: Eddy currents in a solid metallic core. Syed A. Rizvi Summer’12-Revised Spring’16 ENS 441/ELT 437 6 Hysteresis Losses The magnetic flux is caused by magnetic field strength, H. The resulting flux density, B, in any material is related to the magnetic field strength (H) by the following equation: π΅ = ππ × ππ × π» (21) where, B = magnetic flux density (weber/m2 or tesla) H = magnetic field strength (A-turns/m) µo = permeability of free space = 4π × 10−7 µr = relative permeability of the material Note that the value of µr changes with flux and, therefore, the relationship between B and H is expressed in terms of a B-H curve. Under an AC current the iron core is continuously magnetized in one direction, demagnetized, and then magnetized again in the opposite direction. However, the relationship between B and H is not linear. Fig. 5 shows the change in flux density with the magnetic field intensity for one complete cycle of AC current. Initially, B reaches its peak (let’s assume the positive peak) as H reaches the maximum field strength (at maximum current in the positive direction). After that H decrease with the decreasing current and so does B; however, B decreases at a slower rate than H following the path a-b. The result is that as the current reduces to zero bringing H to zero, there still remains some residual flux density in the core (“+Br” in Fig. 5). As the current starts increasing in the negative direction, producing a negative magnetic field strength, B continue to decrease following the path b-c and eventually reduces to zero at a field strength of “-Hc.” As the current continue to decrease in negative direction B starts to decrease in negative direction following the path c-d and eventually reach its maximum value in the negative direction (-Bmax) as H reaches its negative peak. As the current starts decreasing again reducing H, B decreases as well, but with a slower rate following the path d-e. Consequently, when the current and H reduce to zero, B still maintains a negative flux of – Br in the core. B eventually reduces to zero at when H = +Hc following the path e-f. B then increases to its peak value following the path f-a, as H continues to increase and eventually peaks (point “a” in Fig. 5). The closed B-H curve shown in Fig. 5 is called a hysteresis loop and the area under this curve represents the energy that changes into heat during each cycle (joules per cubic meters). To minimize the hysteresis losses materials with relatively narrow hysteresis loop are used to build transformer cores. Since the iron losses (eddy current and hysteresis losses) only generate heat and do not affect the induced voltage they can be represented as resistance (Rm) in parallel to the primary terminals of the transformer. Furthermore, a current must flow through the primary windings to generate the magnetic flux Φm. This current is called magnetizing current and depends on the permeability of the material used to build the core. Higher permeability means lower magnetic current and vice versa. Permeability can be represented by a parallel inductance (Xm) to the primary terminal because magnetizing current does not affect the amount of induced voltage. This inductance is called magnetizing inductance. Syed A. Rizvi Summer’12-Revised Spring’16 ENS 441/ELT 437 7 Figure 5: Hysteresis loop. In a real transformer, the winding of the transformer has a finite resistance that must be taken into account while analyzing or modeling a practical transformer. Since these winding resistances result in a potential drop when current passes through the windings, they are represented as the series resistors (Rp and RS), both at the primary as well as at the secondary side of the transformer. In the analysis of the ideal transformer we assumed the flux due to the load current (Φs) and the counter flux (Φp) generated by the primary remain completely inside the core. However, in a real transformer some of the flux Φs and Φp does leak in the air. This flux leakage induces voltages both in the primary winding and secondary windings, which is counter to the voltages induced by the flux Φm. Consequently, it results in a voltage drop both at the primary as well as the secondary side. Accordingly, the effect of the leakage flux is represented as the series impedances (Xlp and Xls) at the primary as well as the secondary side of the transformer of the model of a practical transformer. Fig. 6 shows the complete model of practical transformer that incorporate the iron losses, magnetizing current, primary and secondary winding resistances, and the effect of the leakage flux under load conditions. Figure 6: Model of a practical transformer. Syed A. Rizvi Summer’12-Revised Spring’16 ENS 441/ELT 437 8 The model of the practical transformer shown in Fig. 6 becomes a lot easier to analyze if the elements on the secondary side are shifted to the primary side using equation (20). Figure 7 shows the model of the practical transformer when everything is viewed from the primary side. We will use the model in Fig. 7 in our analysis of practical transformers. Figure 7: Model of a practical transformer when the circuit is viewed from the primary side. Let’s now examine the model for the practical transformer shown in Fig. 7 for two special load conditions: (1) No-load condition and (2) full-load condition. No-load Condition: Under no-load condition the secondary is open and, therefore, no current flows through the secondary terminals. Consequently, I/p = 0, which means that Rs and Xls can be eliminated from the circuit. Also, Ip = Io, that is the branch containing Rp and Xlp now appear in series with the parallel combination of Rm and Xm. Note that both Rp and Xlp are significantly smaller than Rm and Xm that they can safely be ignored when compared to Rm and Xm. This simplifies the model of the practical transformer under no-load condition to the one given in Fig. 8. Full-load Condition: Note under the full-load condition πΌπ β« πΌπ and, therefore, we can ignore Rm and Xm and the model for the practical transformer reduces to the one shown in Fig. 9. The model of the practical transformer can further be simplified by adding the resistances and inductances as follows: π ππ = π π + π2 × π π Syed A. Rizvi Summer’12-Revised Spring’16 (22) ENS 441/ELT 437 9 Figure 8: Model for the practical transformer under no-load condition. Figure 9: Model of a practical transformer under full-load condition. and πππ = πππ + π2 × πππ . (23) Figure 10 shows the simplified circuit for the practical transformer with full load. Furthermore, Rlp and Xlp can be represented by the complex impedance Zp as follows: ππ = π ππ + ππππ Syed A. Rizvi Summer’12-Revised Spring’16 (24) ENS 441/ELT 437 10 Figure 10: Simplified circuit of the practical transformer under full-load condition. Zp is referred to as transformer impedance and is an important parameter that is used to compute the internal voltage drop of a transformer for varying load conditions (as long as Ip ≥ 10 Io). Example: Specifications of a power transformer are as follows: Sn Enp Ens Inp Ins Rp Rs (KVA) (V) (V) (A) (A) (β¦) (β¦) 1000 69000 6900 14.5 145 27.2 0.25 Xlp Xls Xm (β¦) 151 1.5 505000 432000 0.210 (β¦) (β¦) Rm (β¦) Io (A) Compute the full-load Vs, Is, as well as heat dissipation in the transformer using the simplified model of Fig. 10. Also, compute Iron losses using the model under no-load condition of Fig. 8. Solution: Let’s assume it’s a pure resistive load and full-load secondary voltage is the same as Vns and full-load secondary current is the same as Ins. Now we can calculate the load resistance, RL, as follows: π πΏ = πΈππ πΌππ = 6900 14.5 = 47.6 β¦ The turn ratio is given by π= πΈππ 69000 = = 10 πΈππ 6900 Now we can compute Rep and Xep π ππ = π π + π2 × π π = 27.2 + 102 × 0.25 = 52.2 β¦ πππ = ππ + π2 × ππ = 151 + 102 × 1.5 = 301 β¦ Syed A. Rizvi Summer’12-Revised Spring’16 ENS 441/ELT 437 11 The resistance shifted to primary, RLp, is given by π πΏπ = π2 × π πΏ = 102 × 47.6 = 4760 β¦. Now we can compute the total impedance of the model, ZTp, as follows πππ = π ππ + π πΏπ + ππππ = 52.2 + 4760 + π301 = 4812.2 + π301 = 4821.6 〈0.0186π β¦ Now we can compute primary current, Ip, primary voltage, Ep, secondary current, Is, and secondary voltage, Es as follows πΌπ = πΈππ 69000 = = 14.31 π΄ πππ 4821.6 πΈπ = πΌπ × πππ = 14.31 × 4821.6 = 68118.4 π πΈπ = πΈπ 68118.4 = = 6811.84 π π 10 πΌπ = πΈπ 6811.84 = = 143.1 π΄ π πΏ 47.6 Now we can compute the heat loss due to the load as follows π»πππ‘ πππ π = πΌπ2 × π ππ = 14.312 × 52.2 = 10689.3 π = 10.69 πΎπ Finally, we’ll compute iron losses at no load and at full load as follows 2 πΈππ 690002 πΌπππ πππ π ππ ππ‘ ππ ππππ = = = 11020.83 π = 11.02 πΎπ π π 432000 πΌπππ πππ π ππ ππ‘ ππ’ππ ππππ = πΈπ2 68118.42 = = 10741 π = 10.74 πΎπ π π 432000 Total power loss at full load = 10.69 + 10.74 = 21.43 KW. This power loss produces a significant amount of heat that must be removed from the transformer to avoid any damage to the transformer. There are a number of techniques that are used in the transformers to remove heat, such as through the natural circulation of air (type AA), through forced air circulation (type AFA), oil-immersed self-cooled (OA), and oil immersed selfcooled/forced air cooled (type OA/FA) to name a few. Figure 11 shows the front view of an OA/FA type power transformer and Fig. 12 shows the rear view of the same transformer where cooling fans can be seen, which remove heat from the transformer through forced air circulation. A transformer is called a “step-down” transformer if the secondary voltage, ES, is lower than the primary voltage, EP. On the hand, if the secondary voltage is higher than the primary voltage, it is called a “step-up” transformer. Syed A. Rizvi Summer’12-Revised Spring’16 ENS 441/ELT 437 12 Figure 11: Front view of an OA/FA type power transformer. Figure 12: Rear view of an OA/FA type power transformer. The cooling fans can be in, which are used for forced air circulation to remove heat from the power transformer. Syed A. Rizvi Summer’12-Revised Spring’16 ENS 441/ELT 437 13 Terminal Marking on Power Transformers: In power transformers, the high voltage (HV) terminals are marked by symbols H1 and H2; the low voltage (LV) terminals are marked by symbols X1 and X2. These terminals are mounted on the transformer tank in a way that they either have additive polarity or they have subtractive polarity. The transformer is said to have additive polarity when the terminal H1 is mounted diagonally opposite to the terminal X1. On the other hand, if the terminal H1 is mounted directly opposite to the terminal X1, it is said to have subtractive polarity (see Fig. 13). When you face the voltage side of a power transformer, the terminal at the extreme right is H1, and H2, and so on. The location of the low voltage side terminal would depend on whether the transformer has an additive or subtractive polarity. Subtractive polarity is standard on transformer above 200 KVA with HV rating of above 8660 V. Otherwise the transformer would have additive polarity. Note that it is imperative to know the correct polarity of the transformers if you are connecting them in parallel or configuring a 3-phase transformer bank using single phase transformers. Figure 13: Terminal marking and polarity of the power transformers. Voltage Regulation: Voltage regulation is a measure of variation in the secondary voltage from no-load to full-load condition when the primary voltage is kept constant. Voltage regulation is expressed in percent (%) and is defined by the following equation ππππ‘πππ ππππ’πππ‘πππ = πΈπ (ππ−ππππ) − πΈπ (ππ’ππ−ππππ) × 100 πΈπ (ππ’ππ−ππππ) (25) Power in AC Systems: In AC systems the power is divided into three different categories: Apparent Power: It is the product of the voltage and the complex conjugate of the current and is expressed in “volt-amperes” or VA. If the current I = IR + j IX then the conjugate of I, denoted by I*, is given by I*=IR – j IX. The apparent power, PA, is given by ππ΄ = π × πΌ ∗ Syed A. Rizvi Summer’12-Revised Spring’16 (26) ENS 441/ELT 437 14 Real Power: The real power (PR) is the power utilized by a user and is expressed in watts (W). When the apparent power is expressed in rectangular form, the real part of the apparent power is the real power. The real power always flows from the source to the user. Reactive Power: The reactive power (PX) is needed to establish a magnetic field in inductors. An electric field in a capacitor acts as a source of reactive power. Reactive power can be supplied as well as absorbed by an electric power source. It means that the reactive power can flow from the source to the circuit or from the circuit to the source. When the reactive power flows from the source to the circuit it is considered “positive” reactive power. However, it is considered “negative” reactive power when it flows from the circuit to the source. Mathematically, the apparent power (PA), the real power (PR), and the reactive power (PX) are related as follows: ππ΄ = ππ ± πππ Assignment 1.1: Compute Iron losses and magnetizing reactance of a single-phase transformer. Also, find the polarity of a single phase transformer and measure its voltage regulation. Components needed: Single phase transformer (N-6U): 1 Single phase transformer (VPS230-190): 1 Resistor 10 β¦: 1 Resistor 5 β¦: 1 Resistor 2 β¦: 1 1. Connect the transformer (N-6U) and meters as shown in Fig. 14. Make sure that all of your connections are correct before turning on the power. 2. Turn the power on and measure P through the power meter. Also measure the current Ip and Vp. Since there is no load connected to the secondary, P is solely due to the iron losses. 3. Compute apparent power as follows: π = ππ πΌπ 4. Compute the reactive power, Q, as follows: π = √π 2 − π 2 Syed A. Rizvi Summer’12-Revised Spring’16 ENS 441/ELT 437 15 5. Compute magnetizing reactance “Xm” as follows: ππ2 ππ = π Figure 14: Circuit diagram for measuring iron losses and magnetizing reactance Voltage Regulation: 1. Build the circuit shown in Fig. 15 using the transformer VPS230-190. Use 17 β¦ for the load. Note at full load Is must be less than 1.6 A. If this is not the case, add more resistance to the load until Is becomes 1.6 A or less. 2. Measure the voltage across the load. This is Es (full-load). 3. Now disconnect the load and measure the voltage across the secondary terminals. This is Es (no-load). Figure 15: Circuit diagram for measuring voltage regulation of a transformer. Syed A. Rizvi Summer’12-Revised Spring’16 ENS 441/ELT 437 16 4. Compute the voltage regulation as follows ππππ‘πππ ππππ’πππ‘πππ = πΈπ (ππ−ππππ) − πΈπ (ππ’ππ−ππππ) × 100. πΈπ (ππ’ππ−ππππ) Polarity of a transformer: 1. Connect the HV side of the transformer VPS230-190 to 50 V AC supply. 2. Connect any two adjacent HV and LV terminals using a jumper. 3. Measure the voltages Ep and Ex (see Fig. 16). 4. If Ex > Ep, the polarity of the transformer is additive. 5. However, if Ex < Ep, the polarity of the transformer is subtractive. Figure 16: Circuit for polarity test of a transformer. Syed A. Rizvi Summer’12-Revised Spring’16 ENS 441/ELT 437