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equa105-1J.png
equa105-2J.png

    This value is valid for a single loop. As the armature winding has N turns, then the voltage value induced in the entire winding is given by:

    εind  =  Φmax N ω cos ω t

    After these considerations and assuming a three-phase synchronous machine, we can find the peak value of the induced voltage at any of the phases simply using the above equation for its maximum value, that is, when ω t = 0. So:

    EAmax  =  Φmax N ω

    However, as we know, ω = 2 π f. So you can write:

equa105-2K.png
    eq. 105-2a

    Therefore, it is possible to determine the effective value or RMS of the voltage induced in any of the phases of the machine, dividing the value found by √2, obtaining the eq. 105-03, or:

equa105-3J.png
    eq. 105-03

    In the technical literature the eq. 105-03 is best known for the format of the eq. 105-3a where the product was made √2 π.

equa105-3K.png
    eq. 105-3a

    The effective voltage at the machine terminals will depend on whether the stator is connected in Y or in delta. If the machine is connected in Y, the voltage at the terminals will be √3 EA. If the machine is connected in delta, the voltage at the terminals will simply be equal to EA.

    From eq. 105-03 it is possible to take the following conclusions:
  • The effective value of voltages at the machine terminals is proportional to the number of turns, the intensity of the magnetic induction field and the speed of rotation of the machine.

  • For the frequency to be constant, the rotor speed must be constant.

  • Keeping the speed constant, the effective value of the voltages can be modified through of the variation of the inductor field.


    5.   Electrical Model of the Synchronous Machine

    We will develop an equivalent electrical circuit model that we will use to study the behavior synchronous machine performance with sufficient accuracy.

    The current IF flowing through the field winding produces a flow ΦF in the air gap. On the other hand, the armature current Ia flowing through the stator winding produces a flux Φa. Part of this flux interacts only with the stator winding and is called leakage flux, which we will call Φal. This flow does not interact with the flow due to to the field winding. Therefore, most of the flux due to armature current is confined in the air gap and strongly interacts with the flux field. This flow is called armature reaction flow and is represented by Φar. Soon, the resulting flux in the air gap, called Φr, is due to the components of the two flows ΦF and Φar.   Every flows of these induce a voltage component in the stator winding. So, EA is induced by ΦF, Ea is induced by Φar and the resulting voltage Er is induced by Φr. The voltage EA can be calculated from the machine's open circuit curves.

    It should be noted that the voltage Eair, known as armature reaction voltage depends on Φar and therefore this depends on Ia. From what has been exposed so far, we can write that:

    Er = Ear + EA

    Algebraically working this equation, we can write:

    EA = - Ear + Er

    Thus, we can draw a diagram showing the phasors involved in this analysis.

fasor105-1J.png
Figure 105-01

    From the diagram shown in Figure 105-01, we see that the flow Φar, as well as the current Ia that generates it, are ahead of 90° in relation to the voltage Ear. And in turn, the voltage - Ear is ahead of 90° in relation to Ia. Remembering that an inductive reactance delays the current at 90° with respect to the voltage, so this suggests that - Eair is the voltage drop over an inductive reactance, which we will call Xar, due to the current Ia. Using this fact, we can rewrite the last equation as follows:

    EA = j Xar Ia + Er

    The Xar reactance is known as the armature reaction reactance or magnetizing reactance and is shown in Figure 105-02.

reatancia105-2J.png
Figure 105-02

    If the stator winding resistance Ra and the leakage reactance Xal (which takes into account the dispersion flux Φal) are included, the circuit equivalent per phase is represented in Figure 105-03.

reatancia105-3J.png
Figure 105-03

    The resistance Ra is the effective resistance and is approximately 1.6 times the dc resistance of the stator winding. The effective resistance includes the effects of operating temperature and the surface effect caused by switching the current flowing through the armature winding.

    For simplicity, it is common to define a new reactance called the synchronous reactance and represented by XS, which is the sum of the reactances Xar and Xal. So, using this new reactance, we can represent the synchronous machine model by the circuit shown in Figure 105-04.

reatancia105-4J.png
Figure 105-04

    Thus, we can define the following equations:

    XS = Xar + Xal
    ZS = Ra + j XS

    It should be noted that the synchronous reactance XS takes into account all fluxes, the magnetizing, as well as the dispersion, produced by the armature current.

    The machine parameter values ​​depend on the machine size. Table 105-01 shows its order of magnitude. The units are in p.u.. An impedance of 0.1 pu means that if rated current flows, the impedance will produce a voltage drop of 0.1 (or 10%) of the face value. In general, as machine size increases, the resistance per unit decreases but the synchronous reactance per unit increases.


Table 105-01
Small Machines (dozens of KVA) Big Machines (dozens of MVA)
  Ra 0.05 - 0.02 0.01 - 0.005
  Xal 0.05 - 0.08 0.1 - 0.15
  XS 0.5 - 0.8 1.0 - 1.5

    An alternative way of showing the synchronous machine equivalent circuit is to use the Norton equivalent of the excitation voltage Ef and the synchronous reactance XS, as shown in Figure 105-05.

reatancia105-5J.png
Figure 105-05

    Transforming to the Norton equivalent, we get:

    I'a = EA / XS

    Doing some algebraic transformations it is possible to demonstrate that we can obtain the following relation:

equa105-4J.png
    eq. 105-04

    Where we define m as:

equa105-5J.png
    eq. 105-05

    Where the variables are defined as:

  • Nre - is the number of effective turns of the field winding.
  • Nse - is the number of effective turns of the stator winding per phase.

    6.   Phasor Diagram of a Synchronous Generator

    Since the voltages of a synchronous generator are AC voltages, they are usually expressed as phasors, which have magnitude and angle. Therefore, the relationships between them can be expressed by a graph two-dimensional. When the voltages on one phase (EA, Vg, j XS Ia and Ra Ia ) and the current Ia of this phase are plotted, resulting in a graph called phasor diagram showing the relationships between these quantities.

modelo105-6J.png
Figure 105-06

    In Figure 105-06 we see the model of the equivalent electrical circuit per phase of the synchronous generator. Note that the internal resistance of the field loop and the variable external resistance have been combined on a single resistor RF. Let's use this template to make the phasor diagram shown in Figure 105-07, when we use a resistive load and therefore have a factor of unit power.

fasorial105-7J.png
Figure 105-07

    From the circuit shown in Figure 105-06 we see that the difference between the total voltage EA and the phase terminal voltage, Vg, is given by the resistive and inductive voltage drops. All voltages and currents are referred to Vg, whose angle is arbitrarily assumed to be . So, we can write the equation that defines the terminal voltage Vg, and is given by eq. 105-06, or:

equa105-6J.png
    eq. 105-06

    It should be noted that the circuit shown in Figure 105-06 presents a voltage source of direct current VF, which feeds the rotor field circuit, which is modeled by inductance and series resistance of the field coil. In series with resistor RF there is an adjustable resistor (not shown in the circuit) that controls the flow of the field current. To represent the three-phase system there are three circuits similar to the one shown, one for each phase. The voltages and currents generated by them are identical in magnitude, but they are out of phase with each other of 120°.

    These three phases can be connected in delta or star configuration. When the per-phase equivalent circuit is used, it must be taken into account keep in mind an important fact: the three phases have the same voltages and currents only when the loads connected to them are balanced (or balanced). if generator loads are not balanced, so more sophisticated analysis techniques will be needed. These techniques are beyond the scope of this website.

    This phasor diagram can be compared with the phasor diagrams of generators that work with leading and lagging power factors. In this case, we must note that:

    "For a given voltage phase and a given armature current, an internal generated voltage EA is required higher for lagging loads than for leads loads."
    This statement is quite evident by looking at the phasor diagrams shown in Figure 105-08 and Figure 105-09. Therefore, when you want obtain the same terminal voltage, a larger field current will be required to lagging loads.
fasorial105-8J.png
Figure 105-08
fasorial105-9J.png
Figure 105-09
    Alternatively, we can state that:
    "For a given field current and load current strength, the terminal voltage will be smaller with lagging loads and major with lead loads."

    7.   Power and Torque in a Synchronous Generator

    A synchronous generator converts mechanical power into three-phase electrical power. The power source mechanical, the prime mover, can be a diesel engine, a steam turbine, a hydraulic turbine or any similar device. Whatever the source, it must have the property basic assumption that its speed is almost constant regardless of the power demanded. Otherwise, the frequency of the resulting power system would vary.

    Not all the mechanical power that enters a synchronous generator becomes electrical power at the output of the machine. The difference between the input power and the output represents the machine losses. The input mechanical power is the power on the generator shaft given by the product between the torque applied by the driving machine and the rotational speed of the machine, that is:

equa105-7J.png
    eq. 105-07

    On the other hand, the power internally converted by the synchronous generator from the mechanical form to the electrical form is given by the product of the induced torque and the machine rotational speed, or it is:

equa105-8J.png
    eq. 105-08

    An alternative way of writing this equation is as eq. 105-09.

equa105-9J.png
    eq. 105-09

    In this equation the angle α is the angle between the induced voltage EA and the armature current Ia. The difference between the input power of the generator and the power converted into it represents the mechanical, core and supplementary losses of the machine.

    In Figure 105-10 we present a schematic showing the power flow in a synchronous machine.

fluxo105J.png
Figure 105-10

    The effective electrical power that appears at the output of the synchronous machine can be expressed in line quantities by eq. 105-10.

equa105-10J.png
    eq. 105-10

    And in phase quantities by eq. 105-11, where we made Vg = VF to emphasize the phase greatness.

equa105-11J.png
    eq. 105-11

    We emphasize that, in this case, the angle θ is the angle between the phase or line voltage and the armature current, Ia, as shown in Figure 105-11 (below).

    It is also possible to express the reactive power in line magnitudes, according to eq. 105-12.

equa105-12J.png
    eq. 105-12

    And in phase magnitudes, according to eq. 105-13, where we made Vg = VF to emphasize the phase greatness.

equa105-13J.png
    eq. 105-13

    If the armature resistance RA is ignored, considering XS >> RA, then we can deduce a very useful equation to give an approximate value of the power of generator output. To deduce this equation, let's examine the phasor diagram in Figure 105-11. This figure shows a simplified phasor diagram of a generator with the stator resistance RA ignored.

fasorial105-11J.png
Figure 105-11

    Note that the vertical segment b-c can be expressed by eq. 105-14.

equa105-14J.png
    eq. 105-14

    We can substitute in eq. 105-11 the value of Ia cos θ by the algebraic transformation of the above relation. Thus, we will get:

equa105-15J.png
    eq. 105-15

    This equation stipulates an approximation because we have assumed that the generator resistances are equal to zero, that is, there are no electrical losses in the machine. So, we can state that Pout = Pconv.

    It is also possible to calculate the δ angle by algebraically working eq. 105-15 and obtaining the eq. 105-16 below.

equa105-16J.png
    eq. 105-16

    We should point out that the eq. 105-14 shows that the power produced by a synchronous generator depends directly on the δ angle. The angle δ is known as internal angle or torque angle of the machine. For the eq. 105-14 it is evident that the maximum power that the generator can supply is when δ = 90°, because sin δ = 1.

    The maximum power indicated by this equation is called the static stability limit from the generator. Normally, the real generators never arrive nor close to that limit. Real machines have typical torque angles at full load from 20 to 30 degrees.

    Examining the equations eq. 105-11, eq. 105-13 and eq. 105-15 carefully and, assuming that VF is constant, the effective output power will be directly proportional to Ia cos θ and EA sin δ and the reactive power output will be directly proportional to Ia sin θ.

    These observations are useful when plotting phasor diagrams of synchronous generators with variable payload.

    Taking into account eq.105-08 and eq. 105-15 we can easily write the equation that defines the induced torque on the generator rotor through eq. 105-17.

equa105-17J.png
    eq. 105-17

    8.   Determining the Parameters of a Generator

        Synchronous

    In the same way as we studied in the chapter referring to transformers, in synchronous machines we also use short-circuit and no-load tests to determine the parameters of synchronous machines.

    The equivalent circuit that was deduced earlier for a synchronous generator contained three quantities that must be determined to fully describe the behavior of a real synchronous generator. Are they:

  • The relationship between field current and flux (that is, the field current IF and the induced voltage EA ).

  • The synchronous reactance XS.

  • The armature resistance RA.

        8.1   No-Load Test of a Synchronous Generator

    This is the first step to be performed to determine the parameters of the synchronous generator. Therefore, we must ensure that we do not there is any kind of load connected to the generator terminals. That is, we have the generator in the condition of "empty". Next, we run the generator at its nominal speed. Since we have no load, then we know that Ia = 0 and in this case we have EA = VF . Knowing this information, it is possible to construct a plot of EA versus IF. The curve constructed on the graph is called the empty characteristic. In some literature also known as open circuit characteristic.

    Using the characteristic curve we can find the generated internal voltage EA for any current of field IF given.

saturacao105-12J.png
Figure 105-12

    In Figure 105-12 we see the empty characteristic typical of a synchronous generator. Note that, at the beginning, the curve is almost perfectly straight until some saturation is observed with high field currents. The unsaturated iron of the synchronous machine has a reluctance that is several thousand times less than the reluctance of the air gap. Thus, in the beginning, almost all the magnetomotive force is in the air gap and the resulting flux increment is linear. When the iron finally saturates, the iron's reluctance increases dramatically and the flow increases a lot more slowly with increasing magnetomotive force. The linear portion of a empty characteristic is called the air gap line of the characteristic.


        8.2   Short-Circuit Test of a Generator

            Synchronous

    After carrying out the empty test and determining the graph EA versus IF, we are able to carry out the short circuit test and determine the various parameters of the generator synchronous. Like first step, we must short-circuit the output of the generator with a set of ammeters and adjust the field current IF for the value zero. Thus, the armature current Ia (or the line current IL) is measured while the field current is gradually increased. Making a table of measurements and placing these values ​​on a graph, we will get the so-called short circuit characteristic and we can see this graph in the Figure 105-13.

curvaCCC105-1J.png
Figura 105-13

    Notice that it's basically a straight line. To understand this, we can look at Figure 105-06 and considering that the generator terminals are short-circuited (that is, Vg = VF = 0 ), so we can write the value of Ia by eq. 105-18. In fact, the resulting magnetic induction field in the machine is very small, causing machine is not saturated, so short circuit characteristic is linear.

equa105-18J.png
    eq. 105-18

    Of course we can write the value of the module of Ia by eq. 105-19.

equa105-19J.png
    eq. 105-19

    On the other hand, when the machine is short-circuited, we have VF = 0, and this allows us to write the machine's internal impedance, represented by ZS and given by eq. 105-20.

equa105-20J.png
    eq. 105-20

    However, in general, we know that we can consider ZS >> RA and so, considering RA ≈ 0, we can rewrite the eq. 105-20 like:

equa105-21J.png
    eq. 105-21

    In this equation we are representing the voltage at the output of the no load generator as VF0. So, to determine the approximate value of the machine's synchronous reactance, XS, with a given field current, we can follow the guide below:

  • For a given field current IF and using the graph curves empty characterisitic determine the internal voltage generated EA.

  • Find the short-circuit armature current using the short circuit characteristic graph for field current specified.

  • Using the eq. 105-21 calculate the value of XS.

    If you are interested in determining the armature resistance, RA, you can use the following process:

  • With the machine at rest (inactive), a known DC voltage is applied to the machine terminals and the value of the current flowing is measured by winding. The quotient between these two magnitudes will be the value of RA. This value is approximate, as it was not considering the skin effect at high frequencies. The approximation can be improved by multiplying the value found by 1.6.

        8.3   Short Circuit Ratio

    Another parameter used to describe a synchronous generator is the so-called short circuit ratio. It can be set like:

    "It is the ratio between the field current required for the nominal voltage at no load and the field current required for the rated current of armature in short circuit condition."

    The short-circuit ratio allows characterizing the quality of the synchronous machine. For the same power and rated currents, a machine with lower short-circuit ratio has less volume and weight and, consequently, lower cost.