Physical Description
Mathematical Model
Park's "dqo" transportation
Steady-state Analysis
phasor representation in d-q coordinates
link with network equations
Definition of "rotor angle"
Representation of Synchronous Machines in Stability Studies
neglect of stator transients
magnetic saturation
Simplified Models
Synchronous Machine Parameters
Reactive Capability Limits
Consists of two sets of windings:
3 phase armature winding on the stator distributed with centres 120° apart in space
field winding on the rotor supplied by DC
Two basic rotor structures used:
salient or projecting pole structure for hydraulic units (low speed)
round rotor structure for thermal units (high speed)
Salient poles have concentrated field windings; usually also carry damper windings on the pole face.Round rotors have solid steel rotors with distributed windings
Nearly sinusoidal space distribution of flux wave shape obtained by:
distributing stator windings and field windings in many slots (round rotor);
shaping pole faces (salient pole)
Physical Description
Mathematical Model
Park's "dqo" transportation
Steady-state Analysis
phasor representation in d-q coordinates
link with network equations
Definition of "rotor angle"
Representation of Synchronous Machines in Stability Studies
neglect of stator transients
magnetic saturation
Simplified Models
Synchronous Machine Parameters
Reactive Capability Limits
Consists of two sets of windings:
3 phase armature winding on the stator distributed with centres 120° apart in space
field winding on the rotor supplied by DC
Two basic rotor structures used:
salient or projecting pole structure for hydraulic units (low speed)
round rotor structure for thermal units (high speed)
Salient poles have concentrated field windings; usually also carry damper windings on the pole face.Round rotors have solid steel rotors with distributed windings
Nearly sinusoidal space distribution of flux wave shape obtained by:
distributing stator windings and field windings in many slots (round rotor);
shaping pole faces (salient pole)
Unit I: Introduction to Protection System:
Introduction to protection system and its elements, functions of protective relaying, protective zones, primary and backup protection, desirable qualities of protective relaying, basic terminology.
Relays:
Electromagnetic, attracted and induction type relays, thermal relay, gas actuated relay, design considerations of electromagnetic relay.
Unit-II: Relay Application and Characteristics:
Amplitude and phase comparators, over current relays, directional relays, distance relays, differential relay.
Static Relays: Comparison with electromagnetic relay, classification and their description, over current relays, directional relay, distance relays, differential relay.
Unit-III Protection of Transmission Line:
Over current protection, distance protection, pilot wire protection, carrier current protection, protection of bus, auto re-closing,
Unit-IV: Circuit Breaking:
Properties of arc, arc extinction theories, re-striking voltage transient, current chopping, resistance switching, capacitive current interruption, short line interruption, circuit breaker ratings.
Testing Of Circuit Breaker: Classification, testing station and equipments, testing procedure, direct and indirect testing.
Unit-V Apparatus Protection:
Protection of Transformer, generator and motor.
Circuit Breaker: Operating modes, selection of circuit breakers, constructional features and operation of Bulk Oil, Minimum Oil, Air Blast, SF6, Vacuum and d. c. circuit breakers.
Application of Capacitors to Distribution System and Voltage RegulationAmeen San
Application of Capacitors to
Distribution System and Voltage
Regulation
POWER FACTOR IMPROVEMENT,
System Harmonics
Voltage Regulation
Methods of Voltage Control
Nowadays, it is very important to maintain voltage level. Controlling of that voltage is also important. This Presentation contains methods of voltage control.
Automatic generation control (AGC) is a system for adjusting the power output of multiple generators at different power plants, in response to changes in the load. Since a power grid requires that generation and load closely balance moment by moment, frequent adjustments to the output of generators are necessary. The balance can be judged by measuring the system frequency; if it is increasing, more power is being generated than used, which causes all the machines in the system to accelerate. If the system frequency is decreasing, more load is on the system than the instantaneous generation can provide, which causes all generators to slow down.
Unit I: Introduction to Protection System:
Introduction to protection system and its elements, functions of protective relaying, protective zones, primary and backup protection, desirable qualities of protective relaying, basic terminology.
Relays:
Electromagnetic, attracted and induction type relays, thermal relay, gas actuated relay, design considerations of electromagnetic relay.
Unit-II: Relay Application and Characteristics:
Amplitude and phase comparators, over current relays, directional relays, distance relays, differential relay.
Static Relays: Comparison with electromagnetic relay, classification and their description, over current relays, directional relay, distance relays, differential relay.
Unit-III Protection of Transmission Line:
Over current protection, distance protection, pilot wire protection, carrier current protection, protection of bus, auto re-closing,
Unit-IV: Circuit Breaking:
Properties of arc, arc extinction theories, re-striking voltage transient, current chopping, resistance switching, capacitive current interruption, short line interruption, circuit breaker ratings.
Testing Of Circuit Breaker: Classification, testing station and equipments, testing procedure, direct and indirect testing.
Unit-V Apparatus Protection:
Protection of Transformer, generator and motor.
Circuit Breaker: Operating modes, selection of circuit breakers, constructional features and operation of Bulk Oil, Minimum Oil, Air Blast, SF6, Vacuum and d. c. circuit breakers.
Application of Capacitors to Distribution System and Voltage RegulationAmeen San
Application of Capacitors to
Distribution System and Voltage
Regulation
POWER FACTOR IMPROVEMENT,
System Harmonics
Voltage Regulation
Methods of Voltage Control
Nowadays, it is very important to maintain voltage level. Controlling of that voltage is also important. This Presentation contains methods of voltage control.
Automatic generation control (AGC) is a system for adjusting the power output of multiple generators at different power plants, in response to changes in the load. Since a power grid requires that generation and load closely balance moment by moment, frequent adjustments to the output of generators are necessary. The balance can be judged by measuring the system frequency; if it is increasing, more power is being generated than used, which causes all the machines in the system to accelerate. If the system frequency is decreasing, more load is on the system than the instantaneous generation can provide, which causes all generators to slow down.
Welcome to WIPAC Monthly the magazine brought to you by the LinkedIn Group Water Industry Process Automation & Control.
In this month's edition, along with this month's industry news to celebrate the 13 years since the group was created we have articles including
A case study of the used of Advanced Process Control at the Wastewater Treatment works at Lleida in Spain
A look back on an article on smart wastewater networks in order to see how the industry has measured up in the interim around the adoption of Digital Transformation in the Water Industry.
Overview of the fundamental roles in Hydropower generation and the components involved in wider Electrical Engineering.
This paper presents the design and construction of hydroelectric dams from the hydrologist’s survey of the valley before construction, all aspects and involved disciplines, fluid dynamics, structural engineering, generation and mains frequency regulation to the very transmission of power through the network in the United Kingdom.
Author: Robbie Edward Sayers
Collaborators and co editors: Charlie Sims and Connor Healey.
(C) 2024 Robbie E. Sayers
Immunizing Image Classifiers Against Localized Adversary Attacksgerogepatton
This paper addresses the vulnerability of deep learning models, particularly convolutional neural networks
(CNN)s, to adversarial attacks and presents a proactive training technique designed to counter them. We
introduce a novel volumization algorithm, which transforms 2D images into 3D volumetric representations.
When combined with 3D convolution and deep curriculum learning optimization (CLO), itsignificantly improves
the immunity of models against localized universal attacks by up to 40%. We evaluate our proposed approach
using contemporary CNN architectures and the modified Canadian Institute for Advanced Research (CIFAR-10
and CIFAR-100) and ImageNet Large Scale Visual Recognition Challenge (ILSVRC12) datasets, showcasing
accuracy improvements over previous techniques. The results indicate that the combination of the volumetric
input and curriculum learning holds significant promise for mitigating adversarial attacks without necessitating
adversary training.
CFD Simulation of By-pass Flow in a HRSG module by R&R Consult.pptxR&R Consult
CFD analysis is incredibly effective at solving mysteries and improving the performance of complex systems!
Here's a great example: At a large natural gas-fired power plant, where they use waste heat to generate steam and energy, they were puzzled that their boiler wasn't producing as much steam as expected.
R&R and Tetra Engineering Group Inc. were asked to solve the issue with reduced steam production.
An inspection had shown that a significant amount of hot flue gas was bypassing the boiler tubes, where the heat was supposed to be transferred.
R&R Consult conducted a CFD analysis, which revealed that 6.3% of the flue gas was bypassing the boiler tubes without transferring heat. The analysis also showed that the flue gas was instead being directed along the sides of the boiler and between the modules that were supposed to capture the heat. This was the cause of the reduced performance.
Based on our results, Tetra Engineering installed covering plates to reduce the bypass flow. This improved the boiler's performance and increased electricity production.
It is always satisfying when we can help solve complex challenges like this. Do your systems also need a check-up or optimization? Give us a call!
Work done in cooperation with James Malloy and David Moelling from Tetra Engineering.
More examples of our work https://www.r-r-consult.dk/en/cases-en/
About
Indigenized remote control interface card suitable for MAFI system CCR equipment. Compatible for IDM8000 CCR. Backplane mounted serial and TCP/Ethernet communication module for CCR remote access. IDM 8000 CCR remote control on serial and TCP protocol.
• Remote control: Parallel or serial interface.
• Compatible with MAFI CCR system.
• Compatible with IDM8000 CCR.
• Compatible with Backplane mount serial communication.
• Compatible with commercial and Defence aviation CCR system.
• Remote control system for accessing CCR and allied system over serial or TCP.
• Indigenized local Support/presence in India.
• Easy in configuration using DIP switches.
Technical Specifications
Indigenized remote control interface card suitable for MAFI system CCR equipment. Compatible for IDM8000 CCR. Backplane mounted serial and TCP/Ethernet communication module for CCR remote access. IDM 8000 CCR remote control on serial and TCP protocol.
Key Features
Indigenized remote control interface card suitable for MAFI system CCR equipment. Compatible for IDM8000 CCR. Backplane mounted serial and TCP/Ethernet communication module for CCR remote access. IDM 8000 CCR remote control on serial and TCP protocol.
• Remote control: Parallel or serial interface
• Compatible with MAFI CCR system
• Copatiable with IDM8000 CCR
• Compatible with Backplane mount serial communication.
• Compatible with commercial and Defence aviation CCR system.
• Remote control system for accessing CCR and allied system over serial or TCP.
• Indigenized local Support/presence in India.
Application
• Remote control: Parallel or serial interface.
• Compatible with MAFI CCR system.
• Compatible with IDM8000 CCR.
• Compatible with Backplane mount serial communication.
• Compatible with commercial and Defence aviation CCR system.
• Remote control system for accessing CCR and allied system over serial or TCP.
• Indigenized local Support/presence in India.
• Easy in configuration using DIP switches.
Courier management system project report.pdfKamal Acharya
It is now-a-days very important for the people to send or receive articles like imported furniture, electronic items, gifts, business goods and the like. People depend vastly on different transport systems which mostly use the manual way of receiving and delivering the articles. There is no way to track the articles till they are received and there is no way to let the customer know what happened in transit, once he booked some articles. In such a situation, we need a system which completely computerizes the cargo activities including time to time tracking of the articles sent. This need is fulfilled by Courier Management System software which is online software for the cargo management people that enables them to receive the goods from a source and send them to a required destination and track their status from time to time.
COLLEGE BUS MANAGEMENT SYSTEM PROJECT REPORT.pdfKamal Acharya
The College Bus Management system is completely developed by Visual Basic .NET Version. The application is connect with most secured database language MS SQL Server. The application is develop by using best combination of front-end and back-end languages. The application is totally design like flat user interface. This flat user interface is more attractive user interface in 2017. The application is gives more important to the system functionality. The application is to manage the student’s details, driver’s details, bus details, bus route details, bus fees details and more. The application has only one unit for admin. The admin can manage the entire application. The admin can login into the application by using username and password of the admin. The application is develop for big and small colleges. It is more user friendly for non-computer person. Even they can easily learn how to manage the application within hours. The application is more secure by the admin. The system will give an effective output for the VB.Net and SQL Server given as input to the system. The compiled java program given as input to the system, after scanning the program will generate different reports. The application generates the report for users. The admin can view and download the report of the data. The application deliver the excel format reports. Because, excel formatted reports is very easy to understand the income and expense of the college bus. This application is mainly develop for windows operating system users. In 2017, 73% of people enterprises are using windows operating system. So the application will easily install for all the windows operating system users. The application-developed size is very low. The application consumes very low space in disk. Therefore, the user can allocate very minimum local disk space for this application.
Event Management System Vb Net Project Report.pdfKamal Acharya
In present era, the scopes of information technology growing with a very fast .We do not see any are untouched from this industry. The scope of information technology has become wider includes: Business and industry. Household Business, Communication, Education, Entertainment, Science, Medicine, Engineering, Distance Learning, Weather Forecasting. Carrier Searching and so on.
My project named “Event Management System” is software that store and maintained all events coordinated in college. It also helpful to print related reports. My project will help to record the events coordinated by faculties with their Name, Event subject, date & details in an efficient & effective ways.
In my system we have to make a system by which a user can record all events coordinated by a particular faculty. In our proposed system some more featured are added which differs it from the existing system such as security.
Forklift Classes Overview by Intella PartsIntella Parts
Discover the different forklift classes and their specific applications. Learn how to choose the right forklift for your needs to ensure safety, efficiency, and compliance in your operations.
For more technical information, visit our website https://intellaparts.com
TECHNICAL TRAINING MANUAL GENERAL FAMILIARIZATION COURSEDuvanRamosGarzon1
AIRCRAFT GENERAL
The Single Aisle is the most advanced family aircraft in service today, with fly-by-wire flight controls.
The A318, A319, A320 and A321 are twin-engine subsonic medium range aircraft.
The family offers a choice of engines
TECHNICAL TRAINING MANUAL GENERAL FAMILIARIZATION COURSE
Lecture notes 2(Electrical machine-1)
1. MODULE-II DC MOTOR
Machine that converts electricalenergy into mechanical energy iscalled an electric motor.
2.1TYPESOFELECTRICMOTORS
Depending upon the source of electrical energy,there are two types of electric motors:
A.C. Motors : Motor that converts alternating current energyinto mechanical energy is called A.C.
motor.
D.C. Motors : Motor that converts direct current energy intomechanical energy is called D.C. motor.
2.2 CONSTRUCTIONOFADCMOTOR
DC Motor Consists of Four Main Parts
1 . F i e l d M a g n e t s
2 . A r m a t u r e
3 . C o m m u t a t o r
4 . B r u s h a n d B r u s h G e a r s
2.3WORKINGPRINCIPLE:
The principle upon which a dc motor works is -If a current carrying conductor is placed in a magnetic
field, mechanical force is experienced on the conductor, the direction of which is given by Fleming’s left
hand rule (also called motor rule)and hence the conductor moves in the direction of force
The magnitude of the mechanical force experienced on the conductor is given by
F = B.I.L newtons
Where, B is the flux density in tesla ( Wb/m2
) I is the current flowing through conductor in amperesL is
the is length of conductor in meters.In general if the conductor lies at an angle θ with a magnetic field of
flux density B webers/meter 2
, the mechanical force experienced on a conductor is given by
F = B.I.L. sin θ newtons
FLEMING’S LEFT HAND RULE:
This rule states that if the thumb, forefinger and middle finger of the left hand are stretched in such a
way that they are at right angle to each other mutually and forefinger points towards the direction
of magnetic field, the middle finger towards the direction of flow of current then the thumb will point
the direction of force acting on the conductor.
2.4 BACK EMF IN A DC MOTOR AND ITS IMPORTANCE
When the armature of motor continues to rotate due to motoring action, the armature conductors cut
the magnetic flux and therefore e.m.f are induced in them. The direction of this induced emf, known as
back emf,is such that it opposes the applied voltage.
Since the back emf is induced due to the generator action, the magnitude of it is, therefore, given by the
expression,
Back emf, Eb = ØZNP/60A
2. Where, Ø is flux per pole in webers, Z is the total number of armature conductors or coil sides on
thearmature, P is the number of poles, A is the number of parallel paths in the armature, N is the
rotational speed of the armature in rpm
The equivalent circuit of a dc motor is shown in fig below. The armature circuit is equivalent to a source
of emf, Eb in series with a resistance, Ra put across a dc supply mains of V volts. It is evident from fig
thatthe applied voltage V must be large enough to balance both the voltage drop in armature resistance
and the back emf at all times
i.e. = Eb + Ia Ra
or
Ia = (V-Eb)/Ra
Depends among other factors upon the armature speed and the armature current depends upon
the back emf Eb for a constant applied voltage and armature resistance.If the armature speed is high,
back emf will be large and therefore, armature current small. If thespeed of the armature is low, then
back emf will be less and armature current Ia will be more resulting in development of large torque.
2.5 POWE RELATION OF DC MOTOR:--
Voltage equation for a motor is:
V = Eb + Ia Ra
Multiplying each term of the voltage equation by Ia we get
VIa = Eb Ia + IaRa
The equation is known as power equation of the dc motor The term VIa represents the power supplied
to the motor armature, IaRa represents the power lost in the armature, Eb Ia represents developed in the
armature causing rotation of the armature.
The power developed ‘Eb Ia’ is not all available at the shaft since some it is used to overcome the
mechanical power losses of the motor As mentioned above the mechanical power developed in the
motor is given by
Pm= Eb Ia watt
2.6 TYPESOFDCMOTORS
Differenttypesofdcmotorsare:
1. Permanent magnet dc motors
2. Separately excited dc motors
3. Series wound dc motors
4. Shunt wound dc motors
5. Compound wound dc motors
2.6.1. Permanent magnet dc motors:
It consists of an armature and one or several permanent magnets encircling the armature. Field coils are
not usually required. However, some of these motors do have coils wound on the poles. If they exist,
these coils are Intended only for recharging the magnets in the even that they loose their strength.
2.6. 2. Separately excited dc motors:
These motors have field coils similar to those of a shunt wound dc motor, but the field coils and
armature are fed from different supply source. In a separately excited dc motor, Armature current, Ia =
Line current, IL
3. Back e.m.f developed, Eb = V – I Ra
Powerdrawnfromthemains,
P=VIMechanicalpowerdeveloped,
Pm=Powerinputtoarmature-
powerlostinarmature=VI–I2
Ra=I(V–IRa)=EbI watt
2.6. 3. Series wound dc motors:
As the name implies, the field coils, consisting of a few turns of thick wires, are connected in series with
the armature as shown in the fig. The cross-sectional of the wire for the coils has to be fairly to carry the
armature current, but owing to large current, the number of turns of wire in them need not be large.
In a dc series motor,Armature current, Ia = series field current, Ise= Line current,
IL= I (say)
Armature current,Ia = series field current, Ise = Linecurrent, IL= I (say)
Back emf developed,
Eb = V – I (Ra + Rse )
Power drawn from the mains, P = VI
Mechanical power developed,
Pm = Power input to armature- power lost in armature= VI – I2
(Ra + Rse)
= I [V – I (Ra + Rse) ]
= Eb I watts
2.6.4. Shunt wound dc motors:
The word “ shunt ’’ means “ parallel ’’ . In these motors , the field coils are connected in parallel with the
armature. The field winding consists of a large number of turns of thin wire so as to provide large
resistance. The field current is much less than the armature current, sometimes as low as 5%.
The current supplied to the motor is divided into two paths, one from the field winding and second
through the armature i.e.Input line current,
IL =Ia + Ish
Where Ia is the armature current and Ish is the shunt field current and is given by where V is the supply
voltage, Rsh is the shunt field resistance
Ish = V/Rsh
Back emf developed, Eb = V – I Ra Power drawn from the mains,
P = VIL
Mechanical power developed,
Pm = Power input to armature- power lost in armature
4. = VIL– V Ish - I2
aRa
= V( IL– Ish ) I2
aRa
= V Ia- I2
aRa
= Ia( V – Ia Ra )
= Eb Ia watt
2.6.5. Compound wound dc motors: Compound wound motors are of two types namely cumulative
compound motor wound and differential compound wound motor. In this motor field winding are
connected in such away that the direction of flow of current is same in both the field windings as shown
in fig. In the motor of this type the flux due to the series field winding strengthens the field due to the
shunt field winding.
Differential compound wound motor:
In this motor field winding are connected in such a way that the direction of flow of current is opposite
to each other in both the field windings as shown in fig. In the motor of this type the flux due to the
series field winding weakens the field due to the shunt field winding.
φtotal = φseries – φshunt
The net flux produced in this case is lesser than the original flux and hence does not find much of a
practical application.
Cumulative Compound DC Motor
When the shunt field flux assists the main field flux, produced by the main field connected in series to
the armature winding then its called cumulative compound dc motor.
φtotal = φseries + φshunt
Short Shunt DC Motor
If the shunt field winding is only parallel to the armature winding and not the series field winding then
its known as short shunt dc motor or more specifically short shunt type compound wound dc motor.
5. Long Shunt DC Motor
If the shunt field winding is parallel to both the armature winding and the series field winding then it’s
known as long shunt type compounded wound dc motor or simply long shunt dc motor.
Short shunt and long shunt type motors have been shown in the diagram below.
2.7 Performance calculations
In most applications, DC motors are used for driving mechanical loads. Some applications require that
the speed remain constant as the load on the motor changes. In some applications the speed is required
to be
Controlled over a wide range. It is therefore important to study the relationship between torque and
speed of the motor.
2.8 Speed Regulation
The performance measure of interest is the speed regulation, defined as the change in speed as full load
is
applied to the motor. It can be expressed as:
%Speed regulation= [ (N no load – N full load ) /N full load ] X 10
2.9DC MOTOR CHARACTERISTICS:-
Torque-current characteristics.
Torque- speed characteristics.
Speed- current characteristics.
2.9.1 Torque-current characteristics:-
11. 2.10 Speed Control of D.C. Motors
The speed of a d.c. motor is given by:
N ά Eb/
or
N= K (V --IaR a)/ ………………….(i)
where R = Ra for shunt motor
= Ra + Rse. for series motor
From exp. (i), it is clear that there are three main methods of controlling the
speed of a d.c. motor, namely:
(i) By varying the flux per pole (f). This is known as flux control method.
(ii) By varying the resistance in the armature circuit. This is known as
armature control method.
(iii) By varying the applied voltage V. This is known as voltage control
method.
2.11Speed Control of D.C. Shunt Motors
The speed of a shunt motor can be changed by (i) flux control method
(ii) armature control method (iii) voltage control method. The first method (i.e.
flux control method) is frequently used because it is simple and inexpensive
2.11.1. Flux control method
It is based on the fact that by varying the flux f, the motor speed (N ά 1/f) can
be changed and hence the name flux control method. In this method, a variable
resistance (known as shunt field rheostat) is placed in series with shunt field
winding as shown in fig.
12. The shunt field rheostat reduces the shunt field current Ish and hence the flux f.Therefore, we can only
raise the speed of the motor above the normal speed . Generally, this method permits to increase the
speed in the ratio 3:1. Wider speed ranges tend to produce instability and poor commutation.
Advantages
(i) This is an easy and convenient method.
(ii) It is an inexpensive method since very little power is wasted in the shunt field rheostat due to
relatively small value of Ish.
(iii) The speed control exercised by this method is independent of load on the
machine.
Disadvantages
(i) Only speeds higher than the normal speed can be obtained since the total field circuit resistance
cannot be reduced below Rsh—the shunt field winding resistance.
(ii) There is a limit to the maximum speed obtainable by this method. It is because if the flux is too much
weakened, commutation becomes poorer.
Note. The field of a shunt motor in operation should never be opened because its speed will increase to
an extremely high value.
2.11.2. Armature control method
This method is based on the fact that by varying the voltage available across the armature, the back
e.m.f and hence the speed of the motor can be changed. This is done by inserting a variable resistance
RC (known as controller resistance) in series with the armature as shown in Fig.
N ά V - Ia (Ra + RC )
where RC = controller resistance
Due to voltage drop in the controller resistance, the back e.m.f. (Eb) is decreased. Since N ά Eb, the speed
of the motor is reduced. The highest speed obtainable is lhat corresponding to RC = 0 i.e., normal speed.
Hence, this method can only provide speeds below the normal speed.
Disadvantages
(i) A large amount of power is wasted in the controller resistance since it carries full armature current Ia.
(ii) The speed varies widely with load since the speed depends upon the voltage drop in the controller
resistance and hence on the armature current demanded by the load.
(iii) The output and efficiency of the motor are reduced.
(iv) This method results in poor speed regulation. Due to above disadvantages, this method is seldom
used to control tie speed of shunt motors.
Note. The armature control method is a very common method for the speed control of d.c. series
motors. The disadvantage of poor speed regulation is not important in a series motor which is used only
where varying speed service is required.
13. 2.11.3. Voltage control method
In this method, the voltage source supplying the field current is different from that which supplies the
armature. This method avoids the disadvantages of poor speed regulation and low efficiency as in
armature control method. However, it is quite expensive. Therefore, this method of speed control is
employed for large size motors where efficiency is of great importance.
(i) Multiple voltage control. In this method, the shunt field of the motor is connected permanently
across a-fixed voltage source. The armature can be connected across several different voltages through
a suitable switchgear. In this way, voltage applied across the armature can be changed. The speed will
be approximately proportional to the voltage applied across the armature. Intermediate speeds can be
obtained by means of a shunt field regulator.
(ii) Ward-Leonard system. In this method, the adjustable voltage for the armature is obtained from an
adjustable-voltage generator while the field circuit is supplied from a separate source. This is illustrated
in Fig. The armature of the shunt motor M (whose speed is to be controlled) is connected directly to a
d.c. generator G driven by a constant-speed a.c. motor A. The field of the shunt motor is supplied from a
constant-voltage exciter E. The field of the generator G is also supplied from the exciter E. The voltage of
the generator G can be varied by means of its field regulator. By reversing the field current of generator
G by controller FC, the voltage applied to the motor may be reversed. Sometimes, a field regulator Is
included in the field circuit of shunt motor M for additional speed adjustment. With this method, the
motor may be operated at any speed up to its maximum speed.
Advantages
(a) The speed of the motor can be adjusted through a wide range without resistance losses which results
in high efficiency.
(b) The motor can be brought to a standstill quickly, simply by rapidly reducing the voltage of generator
G. When the generator voltage is reduced below the back e.m.f. of the motor, this back e.m.f. sends
current through the generator armature, establishing dynamic braking. While this takes place, the
generator G operates as a motor driving motor A which returns power to the line.
(c) This method is used for the speed control of large motors when a d.c. supply is not available. The
disadvantage of the method is that a special motor-generator set is required for each motor and the
losses in this set are high if the motor is operating under light loads for long periods.
2.12 Speed Control of D.C. Series Motors
The speed control of d.c. series motors can be obtained by (i) flux control
method (ii) armature-resistance control method. The latter method is mostly
used.
2.12.1. Flux control method
In this method, the flux produced by the series motor is varied and hence the speed. The variation of
flux can be achieved in the following ways:
14. (i) Field divertcrs. In this method, a variable resistance (called field diverter) is connected in parallel with
series field winding as shown in Fig. Its effect is to shunt some portion of the line current from the
series field winding, thus weakening the field and increasing the speed( N ά 1/f). The lowest speed
obtainable is that corresponding to zero current in the diverter (i.e., diverter is open). Obviously, the
lowest speed obtainable is the normal speed of the motor. Consequently, this method can only provide
speeds above the normal speed. The series field diverter method is often employed in traction work.
(ii) Armature diverter. In order to obtain speeds below the normal speed, a variable resistance (called
armature diverter) is connected in parallel with the armature as shown in Fig. The diverter shunts some
of the line current, thus reducing the armature current. Now for a given load, if Ia is decreased, the flux f
must increase ( T ά fIa). Since N ά 1/f, the motor speed is decreased. By adjusting the armature diverter,
any speed lower than the normal speed can be obtained.
(iii) Tapped field control. In this method, the flux is reduced (and hence speed is increased) by
decreasing the number of turns of the series field winding as shown in Fig. The switch S can short circuit
any part of the field winding, thus decreasing the flux and raising the speed. With full turns of the field
winding, the motor runs at normal speed and as the field turns are cut out; speeds higher than normal
speed are achieved.
(iv) Paralleling field coils. This method is usually employed in the case of fan motors. By regrouping the
field coils as shown in Fig. several fixed speeds can be obtained.
15. 2.12.2. Armature-resistance control
In this method, a variable resistance is directly connected in series with the supply to the complete
motor as shown in Fig. This reduces the voltage available across the armature and hence the speed falls.
By changing the value of variable resistance, any speed below the normal speed can be obtained. This
is the most common method employed to control the speed of d.c. series motors. Although this method
has poor speed regulation, this has no significance for series motors because they are used in varying
speed applications. The loss of power in the series resistance for many applications of series motors is
not too serious since in these applications, the control is utilized for a large portion of the time for
reducing the speed under light-load conditions and is only used intermittently when the motor is
carrying full-load.
5.4 Series-Parallel Control
Another method used for the speed control of d.c. series motors is the series parallel method. In this
system which is widely used in traction system, two (or more) similar d.c. series motors are mechanically
coupled to the same load.
When the motors are connected in series , each motor armature will receive one-half the normal
voltage. Therefore, the speed will be low. When the motors are connected in parallel, each motor
armature receives the normal voltage and the speed is high . Thus we can obtain two speeds. Note that
for the same load on the pair of motors, the system would run approximately four times the speed
when the machines are in parallel as when they are in series.
Series-parallel and resistance control
In electric traction, series-parallel method is usually combined with resistance method of control. In the
simplest case, two d.c. series motors are coupled mechanically and drive the same vehicle.
(i) At standstill, the motors are connected is series via a starting rheostat. The motors are started up in
series with each other and starting resistance is cut out step by step to increase the speed. When all the
16. resistance is cut out the voltage applied to each motor is about one-half of the line voltage. The speed is
then about one-half of what it would be if the full line voltage were applied to each motor
(ii) To increase the speed further, the two motors are connected in parallel and at the same time the
starting resistance is connected in series with the combination. The starting resistance is again cut out
step by step until full speed is attained. Then field control is introduced
2.13 NECESSITY OF STARTER:--
The stalling operation of a d.c. motor consists in the insertion of external resistance into the armature
circuit to limit the starting current taken by the motor and the removal of this resistance in steps as the
motor accelerates. When the motor attains the normal speed, this resistance is totally cut out of the
Armature circuit. It is very important and desirable to provide the starter with protective devices to
enable the starter arm to return to OFF position
(i) when the supply fails, thus preventing the armature being directly across the mains when this voltage
is restored. For this purpose, we use no-volt release coil.
(ii) when the motor becomes overloaded or develops a fault causing the motor to take an excessive
current. For this purpose, we use overload release coil.
TYPES OF DC MOTOR STARTER:--
There are two principal types of d.c. motor starters viz., three-point starter and four-point starter. As we
shall see, the two types of starters differ only in the manner in which the no-volt release coil is
connected
2.13.1THREE POINT STARTER:-
This type of starter is widely used for starting shunt and compound motors.
Fig shows the schematic diagram of a three-point starter for a shunt motor with protective devices. It is
so called because it has three terminals L, Z and A. The starter consists of starting resistance divided into
several sections and connected in series with the armature. The tapping points of the starting resistance
are brought out to a number of studs. The three terminals L, Z and A of the starter are connected
respectively to the positive line terminal, shunt field terminal and armature terminal. The other
terminals of the armature and shunt field windings are connected to the negative terminal of the supply.
The no-volt release coil is connected in the shunt field circuit. One end of the handle is connected to the
terminal L through the over-load release coil. The other end of the handle moves against a spiral spring
17. and makes contact with each stud during starting operation, cutting out more and more starting
resistance as it passes over each stud in clockwise direction.
Operation
(i) To start with, the d.c. supply is switched on with handle in the OFF position.
(ii) The handle is now moved clockwise to the first stud. As soon as it comes in contact with the first
stud, the shunt field winding is directly connected across the supply, while the whole starting resistance
is inserted in series with the armature circuit.
(iii) As the handle is gradually moved over to the final stud, the starting resistance is cut out of the
armature circuit in steps. The handle is now held magnetically by the no-volt release coil which is
energized by shunt field current.
(iv) If the supply voltage is suddenly interrupted or if the field excitation is accidentally cut, the no-volt
release coil is demagnetized and the handle goes back to the OFF position under the pull of the spring. If
no-volt release coil were not used, then in case of failure of supply, the handle would remain on the final
stud. If then supply is restored, the motor will be directly connected across the supply, resulting in an
excessive armature current.
(v) If the motor is over-loaded (or a fault occurs), it will draw excessive current from the supply. This
current will increase the ampere-turns of the over-load release coil and pull the armature C, thus short-
circuiting the no volt release coil. The no-volt coil is demagnetized and the handle is pulled to the OFF
position by the spring. Thus, the motor is automatically disconnected from the supply.
Drawback
In a three-point starter, the no-volt release coil is connected in series with the shunt field circuit so that
it carries the shunt field current. While exercising speed control through field regulator, the field current
may be weakened to such an extent that the no-volt release coil may not be able to keep the starter arm
in the ON position. This may disconnect the motor from the supply when it is not desired. This drawback
is overcome in the four point starter.
2.13.2 Four-Point Starter
In a four-point starter, the no-volt release coil is connected directly across the supply line through a
protective resistance R.Fig shows the schematic diagram of a 4-point starter for a shunt motor (over-
load release coil omitted for clarity of the figure). Now the no-volt release coil circuit is independent of
the shunt field circuit. Therefore, proper speed control can be exercised without affecting the operation
18. of no volt release coil. Note that the only difference between a three-point starter and a four-point
starter is the manner in which no-volt release coil is connected. However, the working of the two
starters is the same. It may be noted that the three point starter also provides protection against an
open field circuit. This protection is not provided by the four-point starter.
2.14 Grading of Starting Resistance—Shunt Motors
For starting the motor satisfactorily, the starting resistance is divided into a number of sections in such a
way that current fluctuates between maximum (Im) and minimum (I) values. The upper limit is that
value established as the maximum permissible for the motor; it is generally 1.5 times the full-load
current of the motor. The lower limit is the value set as a minimum for starting operation; it may be
equal to full-load current of the motor or some predetermined value. Fig. shows shunt-wound motor
with starting resistance divided into three sections between four studs. The resistances of these sections
should be so selected that current during starting remains between Im and I as shown in Fig.
(i) When arm A is moved from OFF position to stud 1, field and armature circuits are energized and
whole of the starting resistance is in series with the armature. The armature current jumps to maximum
value given by;
Im= V/R1
where R1 = Resistance of starter and armature
(ii) As the armature accelerates, the generated e.m.f. increases and the armature current decreases as
indicated by curve ab. When the current has fallen to I, arm A is moved over to stud 2, cutting out
sufficient resistance to allow the current to rise to Im again. This operation is repeated until the arm A is
on stud 4 and the whole of the starting resistance is cut out of the armature circuit.
(iii) Now the motor continues to accelerate and the current decreases until it settles down at some value
IL such that torque due to this current is just sufficient to meet the load requirement.
5.14.1 Starter Step Calculations for D.C. Shunt Motor
Fig shows a d.c. shunt motor starter with n resistance sections and (n + 1) studs.
Let R1 = Total resistance in the armature circuit when the starter arm is on stud no. 1
R2 = Total resistance in the armature circuit when the starter arm is on stud no.2 and so on
Im = Upper current limit
I = Lower current limit
n = Number of sections in the starter resistance
V = Applied voltage
Ra = Armature resistance
19. On stud 1. When the starter arm-moves to stud 1, the total resistance in the armature circuit is R1 and
the circuit current jumps to maximum values Im given by;
1
m R
Im=V/R …………………….. (i)
Since torque Ia, it follows that the maximum torque acts on the armature to
accelerate it. As the armature accelerates, the induced e.m.f. (back e.m.f.)
increases and the armature current decreases When the current has fallen to the
predetermined value I, the starter arm is moved over to stud 2. Let the value of
back e.m.f. be Eb1 at the instant the starter arm leaves the stud 1. Then I is given
by;
I = (V-Eb1 )/ R1 ………………………..(ii)
On stud 2. As the starter arm moves over to stud 2, sufficient resistance is cut
out (now total circuit resistance is R2) and current rises to maximum value Im
once again given by;
Im = (V- Eb1)/R2 ……………………….(iii)
The acceleration continues and the back e.m.f. increases and the armature
current decreases. When the current has fallen to the predetermined value I, the
starter arm is moved over to stud 3. Let Eb2 be the value of back e.m.f. at the
instant the starter arm leaves the stud 2. Then,
I = (V- Eb2)/R2 ………………………….(iv)
On stud 3.
As the starter arm moves to stud 3, I m = (V- Eb2)/R3 …………..(v)
As the starter arm leaves stud 3, I = (V- Eb3)/R3 ………………….(vi)
On nth stud.
As the starter arm leaves nth stud I = (V- Ebn)/Rn
On (n + 1)th stud. When the starter arm moves over to (n + 1)th stud, all the
external starting resistance is cut out, leaving only the armature resistance Ra.
Im = (V- Ebn)/Rn and I = (V- Eb)/Ra
20. Dividing Eq.(ii) by Eq.(iii), we get
I/Im = R2/R1
Dividing Eq.(iv) by Eq. (v), we get,
I/Im = R3/R2
Continuing these divisions, we Lave finally,
I/Im = Ra/Rn
Let I/Im = K then R2/R1= R3/R2=…..= Ra/Rn=K
If we multiply these n equal ratios together, then,
(R2/R1)X(R3/R2)X…….X(Ra/Rn) = Kn
Therefore Ra/R1 = Kn
Thus we can calculate the values of R2, R3, R4 etc. if the values of R1, Ra and n
are known.
2.15 TESTING OF DC MOTOR:--
2.15.1 Swinburne's Test::--
It is a simple method in which losses are measured separately and from their knowledge, efficiency at
any desired load can be predetermined in advance. The only running test needed is no-load test.
However, this test is applicable to those machines in which flux is practically constant i.e. shunt and
compound-wound machines. The machine is running as a motor on no-load at its rated voltage. The
speed is adjusted to the rated speed with the help of shunt regulator. The noload current I is measured
by the ammeter A1 whereas shunt field current Ish is given by ammeter A2. The no-load armature
current is (I0-Ish) or Ia0. Let, supply voltage = V, No-load input power = VI0
Power input to armature=V(I0−Ish); Power input to shunt = VIsh
No-load power input to armature supplies the following losses :
(i) Iron losses in core (ii) friction loss (iii) windage loss and(iv) armature Cu
loss,(I0−Ish)2
Ra or Ia0
2
Ra
In calculating armature Cu loss, ‘hot’ resistance of armature should be
used. A stationary measurement of armature circuit resistance at the
room-temperature (15Co) is made by passing current through the armature
from a low voltage dc supply.
21. Then, the ‘hot’ resistance, allowing a temperature rise of 50Co is found thus:
R15 = Ro (1 + 15α0) ; R65 =Ro (1 + 65α0),
R65= R15 X [(1+65αo)/(1+15αo)]
If we subtract from the total input the no-load armature Cu loss, then we get constant losses.
Constant losses Wc= VI0−(I0−Ish)2Ra
Knowing the constant losses of the machine, its efficiency at any other load can be determined as given
below. Let I = load current at which efficiency is required. Then, armature current is
Ia= I − Ish ...if machine is motoring
= I + Ish ...if machine is generating
Efficiency when running as a motor
Input = VI,
Armature Cu loss = Ia
2
Ra=(I-Ish)2
Ra
Constant losses = Wc
Total losses = (I−Ish)2
Ra+Wc
Efficiency = (input-losses)/ Input
Efficiency when running as a generator
Output = VI ; Armature Cu loss = (I + Ish)2
Ra; constant loss=Wc
Total losses = (I+Ish)2
R+Wc
Efficiency = (output)/(output + losses)
Main Disadvantages
1. No account is taken of the change in iron losses from no-load to fullload. At full-load, due to armature
reaction, flux is distorted which increases the iron losses in some cases by as much as 50%.
2. As the test is on no-load, it is impossible to know whether commutation would be satisfactory at full-
load and whether the temperature rise would be within the specified limits.
2.15.2. Regenerative or Hopkinson's Test (Back to Back Test):
By this method, full-load test can be carried out on two shunt machines, preferably identical ones,
without wasting their outputs. The two machines are mechanically coupled and are so adjusted
electrically that one of them runs as a motor and the other as a generator. The mechanical output of the
motor drives the generator and the electrical output of generator is used in supplying the greater part of
input to the motor. If there were no losses in the machines, they would have run without any external
power supply. But due to these losses, generator output is not sufficient to drive the motor and vice-
versa. The losses are supplied either by an extra motor which is belt-connected to the motor-generator
set, or by electrically from the supply mains. The two shunt machines are connected in parallel. They
are, to begin with, started as unloaded motors. Then, the field of one is weakened and that of the other
is strengthened so that the former runs as a motor and the latter as a generator. The usual method of
procedure is as follows: Machine M is started up from the supply mains with the help of a starter (not
shown) whereas main switch S of the other machine is kept open. Its speed is adjusted to normal value
by means of its field regulator. Machine M drives machine G as a generator and its voltage is read on
voltmeter V. The voltage of G is adjusted by its field regulator until voltmeter V1 reads zero, thereby
showing that its voltage is the same, both in polarity and magnitude as that of the main supply.
Thereafter, S is closed to parallel the machines. By adjusting the respective field regulators, any load can
now be thrown on to the machines. Generator current I1 can be adjusted to any desired value by
increasing the excitation of G or by reducing the excitation of M and the corresponding values of
different ammeters are read. The electrical output of the generator plus the small power taken from the
supply, is taken by the motor and is given out as a mechanical power after supplying the motor losses. If
supply voltage is V, then
Motor input=V(I1+I2), where I2 is the current taken from the supply. Generator output = VI1
22. Assuming that both machines have the same efficiency η.
Output of motor = η × input = η V(I1+I2) = generator input
Output of generator=η×input=η×ηV(I1+I2)=η2V(I1 + I2)
η2V(I1 + I2)=VI1 or η=√
Let Ra= armature resistance of each machine
I3= exciting current of the generator
I4= exciting current of the motor
Armature Cu loss in generator = (I1+I3)2
Ra
Armature Cu loss in motor = (I1+I2-I4)2
Ra
Shunt Cu loss in generator = VI3
Shunt Cu loss in motor = VI4
But total motor and generator losses are equal to the power supplied by the mains. Power drawn from
supply = VI2If we subtract the armature and shunt Cu losses from this, we get the stray losses of both
machines.
Total stray losses for the set= VI2−[(I1+I3)2
Ra+(I1+I2−I4)2
Ra+VI3+VI4]=W
Making one assumption that stray losses are equally divided between the two machines, we have Stray
loss per machine = W/2
For Generator Total losses = (I1+I3)2
Ra+VI3+W/2=Wg
Output=VI1 ηg=VI1 /(VI1+Wg)
For Motor
Total losses = (I1+I2-I4)2
Ra+VI4+W/2=Wm
Input = V(I1+I2) ηm= [V(I1+I2)- Wm ] / V(I1+I2)