CA1293015C - Ac-excited generator/motor apparatus - Google Patents

Ac-excited generator/motor apparatus

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Publication number
CA1293015C
CA1293015C CA000592975A CA592975A CA1293015C CA 1293015 C CA1293015 C CA 1293015C CA 000592975 A CA000592975 A CA 000592975A CA 592975 A CA592975 A CA 592975A CA 1293015 C CA1293015 C CA 1293015C
Authority
CA
Canada
Prior art keywords
exciting
armature
active power
slip
winding
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
CA000592975A
Other languages
French (fr)
Inventor
Akira Bando
Osamu Nagura
Shigehiro Kayukawa
Junichi Shiozaki
Akira Momiyama
Hiroto Nakagawa
Yasuteru Oono
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Kansai Electric Power Co Inc
Hitachi Ltd
Original Assignee
Kansai Electric Power Co Inc
Hitachi Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Kansai Electric Power Co Inc, Hitachi Ltd filed Critical Kansai Electric Power Co Inc
Priority to CA000592975A priority Critical patent/CA1293015C/en
Application granted granted Critical
Publication of CA1293015C publication Critical patent/CA1293015C/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Abstract

ABSTRACT OF THE DISCLOSURE
An AC-excited generator/motor apparatus comprising an AC-excited generator/motor having an armature mounting thereon an armature winding connected to an AC power system and a rotor mounting thereon an exciting winding excited by an AC current; exciting means for supplying a controlled AC exciting current to the exciting winding; means for calculating a real slip frequency based on a difference between the phase of an armature voltage appearing on the armature winding and the rotational phase of the rotor; and means for con-trolling the exciting current supplied to the exciting winding from the exciting means in response to a devia-tion of the real slip frequency from a predetermined allowable range of slip frequencies so as to restore the real slip frequency within the allowable range of slip frequencies.

Description

3~

FIELD OF THE INVENTION
The present invention is relating to an AC-excited generator/motor apparatus and more particular to an apparatus suitable for improving the stability of an AC power system such as variable-speed pumping-up power system and fly-wheel generator/motor system.
DESCRIPTION OF THE RELATED ART
In a conventional AC-excited genertor/motor apparatus as disclosed in Japanese Patent Kokoku Sho Nos. 53-7628 and S7-60645, the exciting current is controlled for controlling active and reactive power for the AC-excited machine. Such an apparatus is useful as active power regulator or reactive power regulator having a characteristic of fast response without hunting or stepping out of synchronization.
A variable-speed pumping-up power generator system in which a cycloconverter is used as a frequency converter for AC excitation and a pump turbine is directly connected to an AC-excited synchronous machine is suitable for adjusting frequency of a power system as disclosed in Record of the 1988 Kansai-Section Joint Convention of Institutes of Electrical Engineers of Japan. A similar system is disclosed in National Convention of Institutes of Electrical Engineers of 3(:~5 1 Japan, No. 1026, 1986 and Japan Electric Association, Journal, Pages 34 - 39, March 1986.
Measures for establishing cooperation between an AC excitation control device and a pump turbine guide vane control device are disclosed in Japanese Patent Kokai Sho Nos. 62-71497, 62-72498 and 62-282169.
Control of such an AC-excited generator/motor apparatus useful when it is shut off from an AC power system is disclosed in Japanese Patent Kokai sho 63-43599.
In the AC-excited generator/motor apparatus as disclosed in any of the above references, the control of AC excitation is carried out by using as a reference signal the phase of voltage of the AC power system.
However, none of the references teaches or discloses the control of AC excitation which is still effective when the apparatus is shut off from the AC power system, resulting in disappearance of the reference signal for control.

SUMMARY OF THE INVENTION
It is an object of the present invention to provide an AC-excited generator/motor apparatus having an armature mounting thereon an armature winding connected to an AC power system and a rotor mounting thereon an AC-excited exciting winding wherein the AC
excitation of the exciting winding is controlled, when a slip frequency corresponding to the difference between ~ 3~1S

1 the rotational phase of the rotor and the phase of the output voltage of the armature winding goes beyond a predetermined allowable range of slip frequencies, so as to restore the slip frequency within the allowable range.
It is another object of the present invention to provide an excitation system used with an AC-excited generator/motor apparatus having an armature mounting thereon an armature winding connected to an AC power system and a rotor mounting thereon an AC-excited excit-ing winding wherein if a slip frequency corresponding to the difference between the rotational phase of the rotor and the phase of an armature voltage appearing on the armature winding goes beyond a predetermined allowable range of slip frequencies, the AC excitation is controlled so as to restore the slip frequency within - the allowable range.
In order to achieve the above objects, an AC-excited generator/motor apparatus according to the present invention comprises an AC-excited generator/
motor having an armature mounting thereon an armature winding connected to an AC power system and a rotor mounting thereon an exciting winding; exciting means for supplying a controlled AC exciting current to the exciting winding; means for calculating a real slip frequency from a difference between the phase of an armature voltage appearing on the armature winding and the rotational phase of the rotor; and means for 1 controlling the exciting current supplied to the excit-ing winding from the exciting means in response to a deviation of the real slip frequency from a predeter-mined allowable range of slip frequencies so as to restore the real slip frequency within the allowable range.
According to another aspect of the present invention, an excitation control system for use with an AC-excited generator/motor apparatus having an armature mounted thereon an armature winding connected to an AC
power system and a rotor mounting thereon an exciting winding excited by an AC current comprises exciting means for supplying a controlled AC exciting current to the exciting winding; means for generating an active power control signal based on an active power command and an active power component transmitted between the AC
power system and the armature winding; means for gener-ating a voltage control signal based on an armature voltage appearing on the armature winding and a voltage command; means for generating an exciting current con-trol signal applied to the exciting means for control-ling the exciting current based on the active power control signal and the voltage control signal; means for calculating a real slip frequency based on a difference between the phase of the armature voltage and the rota-tional phase of the rotor of the generator/motor and means responsive to a deviation of the real slip frequency from a predetermined allowable range of slip ```` ~i2~3C lS

1 frequencies for controlling the active power control signal so as to restore the real slip frequency within the allowable range.

BRIEF DESCRIPTION OF THE DRAWINGS
Fig. 1 is a block diagram of an AC-excited generator/motor apparatus as a first embodiment of the present invention;
Fig. 2 is a block diagram of an AC-excited generator/motor apparatus as a second embodiment of the present invention;
Fig. 3 is a block diagram of an AC-excited generator/motor apparatus as a third embodiment of the present invention;
Fig. 4 is a block diagram of an AC-excited generator/motor apparatus as a fourth embodiment of the present invention;
Fig. 5 is a block diagram of a conventional AC-excited generator/motor apparatus; and Fig. 6 is a diagram showing the comparison in frequency changes after the shutting off of the load between the AC generator/motor apparatus of the present invention and that of the prior art.

DESCRIPTION OF THE PREFERRED EMBODIMENTS
An example of the conventional technique will be first described with reference to Fig. 5. An AC

power system 1 is connected via a main circuit breaker 2 1~3~iS

l to a main transformer 3, of which a low voltage side is connected via a synchronizing circuit breaker 4 to an armature winding Sa of the synchronous machine 5. A
frequency converter 6 is provided for converting the output voltage of the armature winding 5a or the low voltage of the main transformer 3 to an output having a voltage suitable for the AC excitation and a frequency controlled as mentioned hereinafter. The frequency converter 6 includes three units provided respectively to the three phases of the exciting winding 5b of the synchronous machine, each unit including an exciting transformer 7 connected to the low voltage side of the main transformer 3 for obtaining an AC voltage suitable for the AC excitation and thyristor power converter 8 which converts the output of the corresponding exciting transformer to a low-frequency AC power to be supplied to the exciting winding 5b. A phase detector 9 is provided for producing an AC excitation frequency signal and includes a potential transformer 10, a voltage phase calculator 11 which calculates a voltage phase Ov of the power system voltage based on an output of the potential transformer lO, a resolver 12 which is connected to the rotation axis of the rotor of the synchronous machine and detects an angular position of the rotor of the AC-exeited synchronous machine 5 or the rotational phase ~rexpressed by an electrieal angle displaeed from a predetermined referenee angular position of the rotor and a slip phase calculator 13 for ealeulating a slip 1~3~1~

1 phase signal ~s = ~v - ~r from the voltage phase ~v and the rotational phase ~r. An exciting current control unit 14 generates a firing angle signal 15 for each phase from the slip phase signal ~s, a quadrature current command Iq (active power control signal) obtained in a manner as will be described later, and an ordinate current command Id (voltage control signal) obtained also in a manner as will be described later.
Each of three automatic pulse phase units 16 generates a firing pulse signal from the corresponding phase firing angle signal 15 and an AC reference signal having the same phase as that of the AC output of the synchronous machine 5 and supplied from a potential transformer 60 and provides the firing signal to the corresponding thyristor power converter 8. In the exciting current control unit 14, the quadrature current command Iq is at the same phase as the slip phase Os and controls the active power of the AC synchronous machine 5, while the ordinate current command ~d is at a phase angle of 90 with the slip phase Os and controls the reactive power component, and also the output voltage of the AC
synchronous machine is controlled by the current commands Iq and Id, as disclosed in Japanese Patent Kokoku Sho Nos. 53-7628 and 57-6045.
The formation of the quadrature and ordinate current commands Iq and Id will now be described. A PV
sensor 19 produces direct current (DC) output signals P
and V indicative of the active power and output voltage, 31~ 15 1 respectively, of the AC power system 1 from the output signals of a current transformer 18 and a potential transformer 10 and provides these signals P and V to an automatic active power regulator (APR) 20 and an auto-matic voltage regulator (AVR) 21, respectively. The AVR21 generates the ordinate current command Id from a voltage command VO externally supplied thereto and the DC signal V indicative of the voltage of the AC power system. Generally, a prime mover (not shown) such as a water wheel is directly coupled to the synchronous machine 5 and controls the rotational speed of the synchronous machine within an allowable range by adjust-ing the output thereof. However, if the output of the synchronous machine increases or decreases excessively, the rotational speed may go beyond the set range. In order to cope with this situation, there are provided a dead zone calculator 28 which generates, when the rotational speed of the synchronous machine indicated by a rotational speed signal outputted from a tachometer 22, a signal proportional to the deviation of the rotational speed from an upper or lower predetermined set limit a speed correction control unit 24 which generates a correction signal ~PO from the output signal of the blind zone calculator and an adder 30 which adds the correction signal ~PO to the active power output command PO to produce an active power correction command P'O. Usually, the APR 20 generates the quadrature current command Iq from the active power 1~3~715 1 correction command P'O and the output signal P of the PV
sensor 19.
If the main circuit breaker 2 is opened so that the synchronous machine 5 is shut off from the AC
power system, the actual active power output value P
becomes 0 regardless of the active power command PO~ so that the APR 20 may be out of order such as occurrence of saturation of an integrator provided therein. In order to prevent such situation, an over-speed relay 25 is provided such that if the relay is operated, it is determined that the synchronous machine is shut off from the AC system and thus a changeover unit 26 is operated so as to forcibly change the active power command PO to zero, and this zero command is applied to the APR 20.
15 . The above prior art is not constituted so as to cope with changes in the frequency in the armature winding of the AC-excited synchronous machine caused if the synchronous machine is shut off from the AC power system. For example, there is a problem such that it is difficult to continue reliably the self-excited opera-tion of the AC-excited generator/motor apparatus which may occur when the generator/motor apparatus is directly coupled to a water turbine and a load is shut off from the generator/motor. That is, when the generator/motor is shut off from the AC power system or a load, the active power output of the generator/motor is reduced to zero, and will not change even if the quadrature current command Iq from the automatic active power regulator 1~3~P15 1 APR is corrected, while the rotational frequency fn will rapidly increase as shown by a solid line 61 in Fig.
6(a) in response to the shutting off of the load, and the output frequency fO of the generator/motor will increase more rapidly than the rotational frequency En of its rotor as shown by a solid line 62, so that slip frequency fs will also increase. Thus, the speed cor-rection control unit 24 corrects the quadrature current command Iq so as to suppress the increase in the rotational frequency after the shutting off of the load.
Therefore, as shown by a two-dot chain line 63 in Fig.
6(b), the slip frequency f5 increases acceleratively to go beyond an operable slip frequency range to thereby disable the continuation of a stabilized operation by self-excitation.
Embodiments of the present invention will now be described with reference to Figs. 1 - 4 in which components similar to those in Fig. 5 are designated by the same reference numerals as those in Fig. 5.
Fig. 1 illustrates a first embodiment of the present invention, and portions of the embodiment dif-ferent from those of the conventional apparatus shown in Fig. 5 will be mainly described.
In Fig. 1, a slip frequency control unit 40 includes a frequency-to-voltage converter 27 which receives a slip phase signal from a phase sensor 9 and converts it to a frequency signal f~, a dead zone calculator 28 which receives the slip frequency signal l~3r., l5 1 f5 and provides an output signal only when the slip frequency is deviated from a predetermined slip frequency range defined by upper and lower limits +fm and ~fml i.e. when f5 ~ +fm or fs < ~fm, a first-order time-lag calculator 29 which multiplies the output of the calculator 28 by a first-order time-lag function , where K is an amplification factor and Ts is l+T5 a first-order time-lag factor, thereby producing a correction signal ~PO obtained by performing a first-order time-lag operation on the received output, and an adder 30 which adds the correction signal ~PO to an active power output command PO externally applied thereto thereby producing a corrected active power command PO~PO/ which is supplied to an automatic active power regulator 20 where ~PO and PO take a positive sign when it effects to accelerate the generator/motor.
When the armature winding of the AC-excited synchronous machine 5 is electrically connected to the AC power system 1, the armature voltage frequency fO is equal to the frequency of the AC power system, and the relationship between the rotational frequency fr and the slip frequency fs is given always by fO = fr + fs Generally, the frequency of the AC power system is almost constant, so that if the rotational frequency fr increases excessively, the slip frequency f5 decreases excessively while if the rotational frequency fr decreases excessively, the slip frequency f5 increases excessively. Therefore, the present embodiment which 3~1S

1 operates so as to restore the slip frequency f5 within the preset range gives the same effect as the prior art which applies a correction signal to the active power regulator 20 so as to restore the rotational frequency 5 fr within its the preset range.
If the synchronous machine 5 is shut off from the AC power system 1, the armature voltage frequency fO
is not restricted by the frequency of the AC power system. Also in this case, unless the relationship fO =
fr + fs is established, a stabilized self-excitation operation cannot be expected. Fig. 6 shows experimental results as to how the armature voltage frequency fO will change if the synchronous machine 5 is shut off from the AC power system.
The rotational frequency fr rapidly increases upon shutting off of the load from the synchronous machine 5 when operated in the power generation mode.
At this time, the armature voltage frequency fO in-creases, as shown in Fig. 6(a), more rapidly than the rotational frequency fr. Therefore, the slip frequency fs changes so as to increase immediately after shutting off of the load as shown by the solid line 64 in Fig.
6(b). Therefore, the change of the slip frequency f5 is similar to the situation where the rotational frequency fr decreases when the AC-excited synchronous machine 5 is electrically connected to the AC power system 1. The speed correction control unit 24 of the prior art shown in Fig. 5 acts to change the quadrature current command 1 Iq (active power control signal) so as to increase the slip frequency f5 as shown by the two-dot chain line 63 in Fig. 6(b) in order to suppress an increase in the rotational frequency fr after the shutting off of the load. Therefore, the increase in the slip frequency is accelerated and the slip frequency may go beyond its operable slip frequency range resulting in discontinua-tion of the self-excitation operation.
In the first embodiment of Fig. 1, the quadrature current command Iq is corrected, when the slip frequency exceeds a set point so as to restore the slip frequency to the set point as shown by the one-dot chain line in Fig. 6(b). As a result, the self-excita-tion operating condition fO = fr + fs is determined definitely by the set point of the slip frequency and the rotational frequency fr adjusted by the prime mover In the present embodiment, the tachometer 22 of Fig. 5 may be omitted.
Fig. 2 illustrates a second embodiment of the present invention in which the output of the dead zone calculator 28 is added by an adder 30A, after processed by the first-order time-lag calculator 29, to the quad-rature current command Iq produced by the automatic active power regulator 20. The output of a tachometer 22 is applied to an over-speed relay 25 such that when the rotational speed of the synchronous machine exceeds a predetermined value, the over-speed relay 25 actuates a changeover unit 26 to switch the active power output 1~3~ 1 5 1 command PO to zero. According to this embodiment, when the synchronous machine 5 is shut off from the AC power system 1, a rapid increase in the rotor speed is sensed and the active power output command PO is switched to zero. Therefore, the input to the automatic power regulator 20 is nullified and the output of the first-order time-lag calculator 29 is used as the quadrature current command Iq, so that the automatic active power regulator 20 is effectively shut off and the quadrature current command Iq is controlled with a control constant suitable for ~the self-excitation operation.
Fig. 3 illustrates a third embodiment of the present invention in which the slip frequency control unit 40 comprises a slip frequency setting unit 50 which includes a tachometer 22 which detects the rotational speed of the rotor and outputs a signal indicative of the sensed rotational speed, an over-speed relay 25 operated when the rotational speed exceeds a predeter-mined value, a changeover unit 26 which selects one of two frequency values fml and fmz predetermined as limits which defines a dead zone width of the dead zone calcu-lator 28 in response to the operation of the over-speed relay 25, and a first-order time-lag calculator 33 which performs a first-order time-lag operation on the selected slip frequency limit fml or fmz. The dead zone width is determined by an output fm from the slip frequency setting unit 50. The over-speed relay 25 is closed thereby causing the changeover unit 26 to output 1~293~1S
1 the value fm2 when the rotational frequency fr detected by the tachometer 22 exceeds a set point which is set at a value higher than a speed at which the synchronous machine is allowed to rotate in the state in which the synchronous machine is connected to the AC power system 1. On the other hand, the over-speed relay 25 is opened in response to the stoppage of the thyristor power converter 8 or the closing of the main circuit breaker 2 thereby causing the changeover unit 26 to output the value of fml. When the over-speed relay 25 is closed, the output of the changeover unit 26 changes from fml to fm2 where the frequencies fml and fm2 are set to satisfy fml > fm2 ~ 0, for example, fml = 5 Hz and fm2 = 3 Hz.
The output of the changeover unit 26 is applied to the first-order time-lag calculator 33 so that its change is moderated, and the resulting output of calculator 33 is applied, to set the dead zone width ~fm to +fm of the dead zone calculator 28.
According to this embodiment, since the slip frequency f5 is decreased to fm2 smoothly by the action of the first-order time-lag calculator 33 after the synchronous machine is shut off from the AC power system 1 and the slip frequency f5 reaches fml/ the output voltage of frequency converter 6 can be reduced while the control voltage margin can be increased, so that a stabilized self-excitation operation of the machine is maintained.
Fig. 4 illustrates a fourth embodiment of the 3~15 1 present invention which detects the frequency of the armature voltage instead of the rotational speed of the rotor in the third embodiment shown in Fig. 3.
In Fig. 4, a frequency relay 34 receives an output voltage of a frequency detector 35 indicative of the frequency of the armature voltage and operates when the frequency of the armature voltage exceeds a pre-determined set value to switch the changeover unit 26.
Other operations are similar to the third embodiment shown in Fig. 3. The frequency relay 34 may be closed when the armature frequency fO exceeds the set point for a time interval longer than a predetermined value. The set frequency value is selected so as to be higher than a maximum allowable value for the AC power system.
Frequency relay 34 is opened in response to the stoppage of thyristor power converter 8 or the closing of the main circuit breaker 2.
This embodiment has the effects that the change to the self-excitation mode in operation of the synchronous machine is determined by detecting that the armature frequency fO exceeds the set value when the synchronous machine is shut off from the AC power system 1, and then the slip frequency f5 is reduced by narrow-ing the allowable range of slip frequencies, i.e. the dead zone width of the dead zone calculator 28, so that the output voltage of frequency converter 6 can be reduced, the control voltage margin can be increased, and thus a stabilized self-excited machine operation is 3(~15 1 maintained.
According to the present invention, the AC-excited generator/motor apparatus includes the frequency control unit which delivers a correction signal to the active power regulator so as to suppress possible deviations of the slip frequency from an allowable range thereof when the generator/motor apparatus is shut off from its AC system, so that a rapid increase in the armature voltage frequency in the generator/motor is prevented and a stabilized self-excited apparatus operation is maintained.

Claims (19)

1. An AC-excited generator/motor apparatus comprising:
an AC-excited generator/motor having an armature mounting thereon an armature winding connected to an AC power system and a rotor mounting thereon an exciting winding excited by an AC current;
exciting means for supplying a controlled AC
exciting current to the exciting winding;
means for calculating a real slip frequency corresponding to a difference between a phase of an armature voltage appearing on the armature winding and a rotational phase of the rotor; and means for controlling the exciting current supplied to the exciting winding from the exciting means in response to a deviation of the real slip frequency from a predetermined allowable range of slip frequencies so as to restore the real slip frequency within the allowable range.
2. An AC-excited generator/motor apparatus ac-cording to claim 1, further including means responsive to a rotational speed of the rotor exceeding a predeter-mined set value for changing the allowable range of slip frequencies.
3. An AC-excited generator/motor apparatus according to claim 1, further including means responsive to a deviation of a frequency of the armature voltage from a predetermined set value for changing the allowable range of slip frequencies.
4. An AC-excited generator/motor apparatus according to claim 1, further including means for generating an active power control signal based on a given active power command and an active power component transmitted between the AC power system and the armature winding, means for generating a voltage control signal based on the armature voltage and a given voltage command, and means for generating an exciting current control signal to control the exciting current based on the active power control signal and the voltage control signal, and said exciting current controlling means including means responsive to the deviation of the slip frequency from the predetermined allowable range of slip frequencies for generating a correction signal to correct the active power command.
5. An AC-excited generator/motor apparatus according to claim 4, wherein the correction signal is determined in accordance with a degree of the deviation of the real slip frequency from the predetermined allowable range of slip frequencies.
6. An AC-excited generator/motor apparatus according to claim 4, further including means responsive to a rotational speed of the rotor exceeding a predeter-mined set value for changing the allowable range for the slip frequency.
7. An AC-excited generator/motor apparatus according to claim 4, further including means responsive to a deviation of a frequency of the armature voltage from a predetermined set value for changing the allow-able range of slip frequencies.
8. An AC-excited generator/motor apparatus according to claim 1, further including means for generating an active power control signal from a given active power command and an active power component transmitted between the alternating current power system and the armature winding, means for generating a voltage control signal from a given voltage command and an output voltage appearing on the armature winding, and means for generating an exciting current control signal to control the exciting current on the basis of the active power control signal and the voltage control signal, and said exciting current controlling means including means responsive to the deviation of the slip frequency from the predetermined allowable range of slip frequencies for generating a correction signal to correct the active power control signal.
9. An AC-excited generator/motor apparatus according to claim 8, wherein the correction signal is determined in accordance with a degree of the deviation of the real slip frequency from the predetermined allow-able range of slip frequencies.
10. An AC-excited generator/motor apparatus according to claim 8, further including means responsive to a rotational speed of the rotor exceeding a predeter-mined set value for changing the active power command.
11. An AC-excited generator/motor apparatus according to claim 10, wherein the active power command is changed to zero in response to the rotational speed of the rotor exceeding the predetermined set value.
12. An AC-excited generator/motor apparatus comprising:
an AC-excited generator/motor having an armature mounting thereon an armature winding connected to an AC power system and a rotor mounting thereon an exciting winding excited by an AC current;
exciting means for supplying a controlled AC
exciting current to the exciting winding;
means for calculating a real slip frequency corresponding to a difference between a phase of an armature voltage appearing on the armature winding and a rotational phase of the rotor; and means for controlling the exciting current supplied to the exciting winding from the exciting means in response to a deviation of the real slip frequency exceeding predetermined value of the slip frequency so as to reduce the real slip frequency.
13. An AC-excited generator/motor apparatus comprising:
an AC-excited generator/motor having an armature mounting thereon an armature winding connected to an AC power system and a rotor mounting thereon an exciting winding excited by an AC current;
exciting means for supplying a controlled AC
exciting current to the exciting winding;
means for calculating a real slip frequency based on a difference between a phase of an armature voltage appearing on the armature winding and a rotational phase of the rotor; and means for controlling the exciting current supplied to the exciting winding from the exciting means in response to a deviation of the real slip frequency exceeding a predetermined value of the slip frequency.
14. An excitation control system for use with an AC-excited generator/motor apparatus having an armature mounted thereon an armature winding connected to an AC
power system and a rotor mounted thereon an exciting winding excited by an AC current, said control system comprising:
exciting means for supplying a controlled AC
exciting current to the exciting winding;
means for generating an active power control signal based on an active power command and an active power component transmitted between the AC power system and the armature winding;
means for generating a voltage control signal based on an armature voltage appearing on the armature winding and a given voltage command;
means for generating an exciting current control signal applied to the exciting means to control the exciting current based on the active power control signal and the voltage control signal;
means for calculating a real slip frequency corresponding to a difference between a phase of the armature voltage and a rotational phase of the rotor of the AC
generator motor;
means responsive to a deviation of the real slip frequency from a predetermined allowable range of slip frequencies for controlling the active power control signal so as to restore the real slip frequency within the allowable range of slip frequencies.
15. An excitation control system according to claim 14, wherein the controlling means includes means responsive to the deviation of the real slip frequency from the predetermined allowable range of slip frequen-cies for generating a correction signal and means for correcting the active power command by the correction signal.
16. An excitation control system according to claim 15, further including means responsive to a rotational speed of the rotor exceeding predetermined set value for changing the allowable range of slip frequencies.
17. An excitation control system according to claim 15, further including means responsive to a frequency of the armature voltage exceeding predeter-mined set value for changing the allowable range of slip frequencies.
18. An excitation control system according to claim 14, wherein the controlling means includes means responsive to the deviation of the real slip frequency from the predetermined allowable range of slip frequencies for generating a correction signal and means for correcting the active power control signal by the correction signal.
19. An excitation control system according to claim 18, further including means responsive to a rotational speed of the rotor exceeding a predetermined set value for changing the value of the active power command.
CA000592975A 1989-03-07 1989-03-07 Ac-excited generator/motor apparatus Expired - Lifetime CA1293015C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CA000592975A CA1293015C (en) 1989-03-07 1989-03-07 Ac-excited generator/motor apparatus

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA000592975A CA1293015C (en) 1989-03-07 1989-03-07 Ac-excited generator/motor apparatus

Publications (1)

Publication Number Publication Date
CA1293015C true CA1293015C (en) 1991-12-10

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Family Applications (1)

Application Number Title Priority Date Filing Date
CA000592975A Expired - Lifetime CA1293015C (en) 1989-03-07 1989-03-07 Ac-excited generator/motor apparatus

Country Status (1)

Country Link
CA (1) CA1293015C (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113839597A (en) * 2021-09-08 2021-12-24 西安陕鼓动力股份有限公司 Motor starting method, motor starting and synchronous operation method with different power supplies supplying power

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113839597A (en) * 2021-09-08 2021-12-24 西安陕鼓动力股份有限公司 Motor starting method, motor starting and synchronous operation method with different power supplies supplying power
CN113839597B (en) * 2021-09-08 2024-04-09 西安陕鼓动力股份有限公司 Motor starting and synchronous operation method powered by different power supplies

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