GB2145545A - Voltage regulator for aircraft generators - Google Patents

Voltage regulator for aircraft generators Download PDF

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Publication number
GB2145545A
GB2145545A GB8322652A GB8322652A GB2145545A GB 2145545 A GB2145545 A GB 2145545A GB 8322652 A GB8322652 A GB 8322652A GB 8322652 A GB8322652 A GB 8322652A GB 2145545 A GB2145545 A GB 2145545A
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GB
United Kingdom
Prior art keywords
voltage
circuit
current
exciter field
exciter
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.)
Withdrawn
Application number
GB8322652A
Other versions
GB8322652D0 (en
Inventor
David Allen Fox
Lynn Lee Tipton
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.)
CBS Corp
Original Assignee
Westinghouse Electric Corp
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 Westinghouse Electric Corp filed Critical Westinghouse Electric Corp
Priority to GB8322652A priority Critical patent/GB2145545A/en
Publication of GB8322652D0 publication Critical patent/GB8322652D0/en
Publication of GB2145545A publication Critical patent/GB2145545A/en
Withdrawn legal-status Critical Current

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Classifications

    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02PCONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
    • H02P9/00Arrangements for controlling electric generators for the purpose of obtaining a desired output
    • H02P9/14Arrangements for controlling electric generators for the purpose of obtaining a desired output by variation of field
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02PCONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
    • H02P2101/00Special adaptation of control arrangements for generators
    • H02P2101/30Special adaptation of control arrangements for generators for aircraft

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  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Control Of Eletrric Generators (AREA)

Abstract

A voltage regulator controls generator output voltage by controlling exciter field current. Sensors 14, 20 produce control signals which are proportional to exciter field current and generator output voltage. These signals are combined 22 and compared with a reference voltage signal 24 by a comparator 26. A current controller 28 regulates exciter field current in response to the comparator output. The controller 28 may be a transistor in series with the field winding 12. The signal from the field current sensor 14 may also be supplied to overcurrent protection circuitry 30. <IMAGE>

Description

SPECIFICATION Voltage regulator for aircraft generators This invention relates to voltage regulators and more particularly to voltage regulators for aircraft generators.
Aircraft generator voltage regulators which regulate generator output. voltage by controlling exciter field current are well known. These regulators generally utilize a feedback loop that includes a voltage sensor which produces a voltage signal proportional to generator output voltage, an amplifier which amplifies this signal, and a means for controlling exciter field current in response to the amplified voltage signal.
Aircraft generators (e.g., synchronous AC machines with brushless excitation) have requirements in common with generators for other applications but also have requirements for high reliability and performance in a compact and cost effective arrangement. The generator control unit, including the voltage regulator, is part of the generator system that must meet a high level of performance. While the subject matter of the present invention has particular advantage in aircraft generator systems, it is not limited to such applications.
Early regulators utilized series compensation techniques to improve transient performance. In these systems, a filter circuit was inserted in the feedback loop to compensate for the exciter time constant. However, circuit time constants vary with changing environmental conditions, such as temperature changes. This limited the effectiveness of series compensation circuits.
Minor loop feedback techniques were developed to achieve improved stability and transient response. In these systems, a signal proportional to the voltage regulator output voltage is fed back to the input of the amplifier in the major feedack loop. Although this results in improved performance, the circuit does not provide adequate performance for wide speed range systems, such as DC link systems with a converter in the closed loop.
Negative exciter field forcing is used to improve transient response time. This is accomplished by inserting an active current limiter, such as a transistor, in series with the exciter field coil. By turning off the transistor, a rapid reduction in field current is achieved.
If negative exciter field forcing is used in combination with a minor loop feedback circuit, the feedback signal which is derived from the voltage regulator output voltage cannot respond to the negative field forcing. The regulator then treats the negative field forcing as a disturbance, rather than a correction. Therefore transient response is degraded considerably.
It is the principal object of the present invention to provide improved voltage regulation.
The invention resides broadly in a voltage regulator circuit for a generator with an exciter field coil, said circuit comprising: a current sensing circuit connected to sense current in said exciter field coil; a voltage sensing circuit for sensing the generator output voltage; combining circuitry connected to the exciter current and generator voltage sensing circuits; for combining the signals therefrom; a comparator for comparing the combined signal with a reference voltage; a control circuit for controlling current in said exciter field coil, responsive to the output of said comparator.
The present invention incorporates an improved feedback technique which utilizes the exciter field current rather than voltage. The exciter field current accurately reflects the exciter output voltage and is therefore more useful in representing a state variable of the machine.
Components of previous feedback circuits which attempted to model the exciter time constant have been eliminated since the time constant is accurately represented by the exciter field current.
A voltage regulator constructed in accordance with the present invention includes means for sensing exciter field current and for producing a signal proportional to the current. In addition, a voltage sensing means produces a second signal proportional to the output voltage of the generator. These two signals are combined to produce a third signal which goes to a comparator for comparison with a reference signal. The comparator produces a fourth signal in response to the difference between the reference signal and the third signal. A current controlling means responds to this fourth signal to control the exciter field current.
The invention is illustrated in exemplary fashion with the aid of the accompanying drawings, in which: Figure 1 is a block diagram of a voltage regulator system employing a voltage regulator in accordance with the present invention.
Figure 2 is a schematic diagram of one embodiment of a circuit employing a voltage regulator in accordance with the present invention.
Referring to the drawings, Fig. 1 is a block diagram of a voltage regulator system employing a voltage regulator in accordance with the present invention. A source of power such as D.C.
power supply 10 provides power to exciter field coil 1 2. Current sensor 14, which includes sensing means such as a shunt resistor or current transformer, provides a first signal which is proportional to exciter field current. Negative field forcing circuit 1 6 is connected in series with current sensor 14 and exciter field coil 1 2. Shunt diode 1 8 provides a path for current produced by the collapsing magnetic field of exciter field coil when exciter field coil current is interrupted.
Terminal VS is connected to a point in the generator circuit which is at a voltage level that is proportional to the generator output voltage. In a variable speed constant frequency system, terminal VS may be connected to the converter output. The voltage at terminal VS is sensed by voltage sensor 20 which produces a second signal proportional to the generator output voltage.
Voltage divider 22 serves as a means for combining the first and second signal and for producing a third signal.
Voltage reference source 24 supplies a reference voltage which is compared with the third signal by comparator 26. A fourth signal, proportional to the difference between the third signal and the reference voltage is produced by comparator 26. Current controller 28 provides means for controlling exciter field coil current in response to the fourth signal.
Overcurrent sensor 30 is connected to the output of current sensor 1 4 to detect an overcurrent condition in the exciter field coil 1 2. An excessive current sensed by overcurrent sensor 30 will cause protective devices in the voltage regulator, not shown, to operate and remove the overcurrent condition.
Fig. 2 is a schematic diagram of one embodiment of a circuit employing a voltage regulator in accordance with the present invention. A D.C. power supply, item 10 in Fig. 1, is connected to terminal PS to supply power to exciter field coil 12. Shunt R1 is connected in series with exciter field coil 12 and acts as a current sensing element in current sensor 14. Capacitor C1 in parallel with shunt R1 minimizes noise interference.
Capacitor C2, zener diode CR1, and resistor R2 are connected as shown to form a power supply referenced to terminal PS. The voltage developed across R1 is fed to operational amplifier IC1 which is connected to transistor Q1 and resistor R3 to form a current source in which the current in the collector of transistor Ol is proportional to the exciter field current.
Capacitor C3 stabilizes operational amplifier IC1.
Resistors R4 and R5 are connected in series between the collector of transistor Ol and ground. Consequently, a first ground referenced voltage signal which is proportional to exciter field current, is developed at the junction between R4 and the collector of Q1.
Resistors R4 and R5 also serve as an overcurrent sensor 30 with the voltage at the junction between resistors R4 and R5 being proportional to exciter field current. This voltage is connected to conventional overcurrent protective circuitry, not shown, by way of terminal OC.
A second voltage signal from voltage sensor 20 in Fig. 1 is connected to terminal S1. Voltage divider 22 serves as a means for combining the first and second voltage signals and comprises the series connection of capacitor C4 and resistors R6 and R7. Capacitor C4 blocks D.C. voltage which would produce an error in the steady state regulated voltage. The combination of resistor R6 and capacitor C4 may be tuned to improve circuit response. The voltage appearing at the junction of resistor R7 and capacitor C4 represents a third signal which closely reflects the state of the exciter and thus provides stabilitiy compensation.
This third signal is fed to operational amplifier IC2 of comparator 26 where it is compared with a reference voltage supplied to terminal VR from voltage reference source 24 in Fig. 1.
Comparator 26 produces a fourth signal which is fed to drive circuit 32 of current controller 28.
Conventional circuitry of drive circuit 32 controls transistor Q2 in response to the fourth signal from comparator 26.
Negative field forcing circuit 1 6 includes transistor Q3 and zener diode CR2. Transistor Q3 is driven by known circuitry via terminal NFF. Shunt diode 18 provides a path for current generated by the collapsing magnetic field of exciter field coil 1 2 when exciter field coil current is decreased as a result of transistor Q2 or Q3 being turned off. Since the cathode of shunt diode 1 8 is connected between terminal PS and current sensor 14, shunt resistor R1 remains in the current loop and continues to sense the actual exciter field coil current.
A voltage regulator circuit in accordance with this invention has been constructed and its performance has been evaluated on a DC link system. Significant improvement in transient response has been seen upon the removal of 42 KW and 60 KW loads. Recovery from load removals has been shown to be up to two times faster than with a prior art minor loop feedback circuit.
By way of further example, the following table identifies specific components which may be used in a voltage regulator in accordance with one embodiment of this invention as shown in Fig. 2. It will be apparent to those skilled in the art that other components may be used within the scope of this invention. For example, the level of feedback may be adjusted by changing the value of resistor R4.
RESISTORS R1 0.1S2 shunt R2 10K R3 125# R4 800s2 R5 1.1K R6 3.9K R7 10K CAPACITORS C1 1 f C2 1yf C3 100pf C4 0.33,uf DIODES CR1 15v zener CR2 168v zener CR3 200v/9 amp TRANSISTORS Q1 2N5416 Q2 2N6546 Q3 2N6546 OPERATIONAL AMPLI FIERS IC1 lOlA IC2 LM 124 Identification of reference numerals used in the drawings Legend Ref. No. Figure D.C. POWER SUPPLY 10 1 EXCITER FIELD COIL 12 1 CURRENT SENSOR 14 1 NEGATIVE FIELD FORCING 16 1 SHUNT DIODE 18 1 VOLTAGE SENSOR 20 1 VOLTAGE DIVIDER 22 1 VOLTAGE REFERENCE SOURCE 24 1 COMPARATOR 26 1 CURRENT CONTROLLER 28 1 OVERCURRENTSENSOR 30 1 DRIVE CIRCUIT 32 2

Claims (4)

1. A voltage regulator circuit for a generator with an exciter field coil, said circuit comprising: a current sensing circuit connected to sense current in said exciter field coil; a voltage sensing circuit for sensing the generator output voltage; combining circuitry connected to the exciter current and generator voltage sensing circuits; for combining the signals therefrom; a comparator for comparing the combined signal with a reference voltage; a control circuit for controlling current in said exciter field coil, responsive to the output of said comparator.
2. A circuit according to claim 1, further comprising: a field forcing circuit connected in series with said exciter field coil.
3. A circuit according to claim 1 or 2, wherein said combining circuit is a branch circuit comprising: the series connection of a first resistor, a capacitor, and a second resistor; said first and second voltage signals being impressed on opposite ends of said branch circuit.
4. A circuit according to claim 1, 2 or 3, further including an overcurrent circuit for sensing an overcurrent condition in said exciter field coil.
GB8322652A 1983-08-23 1983-08-23 Voltage regulator for aircraft generators Withdrawn GB2145545A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB8322652A GB2145545A (en) 1983-08-23 1983-08-23 Voltage regulator for aircraft generators

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8322652A GB2145545A (en) 1983-08-23 1983-08-23 Voltage regulator for aircraft generators

Publications (2)

Publication Number Publication Date
GB8322652D0 GB8322652D0 (en) 1983-09-28
GB2145545A true GB2145545A (en) 1985-03-27

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Family Applications (1)

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GB8322652A Withdrawn GB2145545A (en) 1983-08-23 1983-08-23 Voltage regulator for aircraft generators

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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2282469A (en) * 1993-10-01 1995-04-05 Lucas Aerospace Power Equip Microprocessor controller for starter generator
US5663632A (en) * 1995-07-17 1997-09-02 Lucas Aerospace Power Equipment Corp. Field current control for generator during build-up
US5903130A (en) * 1996-11-01 1999-05-11 Lucas Aerospace Power Equipment Corporation Fail-safe regulator biasing circuit
US6153942A (en) * 1995-07-17 2000-11-28 Lucas Aerospace Power Equipment Corp. Starter/generator speed sensing using field weakening
RU2510877C1 (en) * 2012-10-11 2014-04-10 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Южно-Уральский государственный университет" (национальный исследовательский университет) (ФГБОУ ВПО "ЮУрГУ" (НИУ)) Electric drive with synchronous reluctance machine
US11390161B2 (en) * 2010-08-03 2022-07-19 Polaris Industries Inc. Side-by-side vehicle

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2282469A (en) * 1993-10-01 1995-04-05 Lucas Aerospace Power Equip Microprocessor controller for starter generator
FR2713843A1 (en) * 1993-10-01 1995-06-16 Lucas Aerospace Power Equip Microprocessor control device and associated control and sensing circuits for a starter / generator.
US5583420A (en) * 1993-10-01 1996-12-10 Lucas Aerospace Power Equipment Corporation Microprocessor controller for starter/generator
GB2282469B (en) * 1993-10-01 1998-04-29 Lucas Aerospace Power Equip Microprocessor controller for starter/generator
US5801516A (en) * 1993-10-01 1998-09-01 Lucas Aerospace Power Equipment Corp. Drive overload protection circuit
US5663632A (en) * 1995-07-17 1997-09-02 Lucas Aerospace Power Equipment Corp. Field current control for generator during build-up
US6153942A (en) * 1995-07-17 2000-11-28 Lucas Aerospace Power Equipment Corp. Starter/generator speed sensing using field weakening
US5903130A (en) * 1996-11-01 1999-05-11 Lucas Aerospace Power Equipment Corporation Fail-safe regulator biasing circuit
US11390161B2 (en) * 2010-08-03 2022-07-19 Polaris Industries Inc. Side-by-side vehicle
US11840142B2 (en) 2010-08-03 2023-12-12 Polaris Industries Inc. Side-by-side vehicle
RU2510877C1 (en) * 2012-10-11 2014-04-10 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Южно-Уральский государственный университет" (национальный исследовательский университет) (ФГБОУ ВПО "ЮУрГУ" (НИУ)) Electric drive with synchronous reluctance machine

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Publication number Publication date
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