Excitation System of Alternator
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Transient Analysis of Three-Phase Wound Rotor (Slip-Ring) Induction Motor Under Operating Condition
International Journal of Recent Engineering Research and Development (IJRERD) ISSN: 2455-8761 www.ijrerd.com || Volume 02 – Issue 07 || July 2017 || PP. 19-32 Transient Analysis of Three-Phase Wound Rotor (Slip-Ring) Induction Motor under Operating Condition Obute K.C.1, Enemuoh F.O.1 1 – Department of Electrical Engineering Nnamdi Azikiwe University Awka, Anambra State Nigeria Corresponding Author - Obute Kingsley Chibueze Department of Electrical Engineering Nnamdi Azikiwe University Awka, Anambra State Nigeria Abstract: This work investigates the transient behaviours of a three phase wound rotor type induction motor, running on load. When starting a motor under load condition becomes paramount, obviously a wound rotor (slip ring) induction becomes the best choice of A.C. motor. This is because maximum torque at starting can be achieved by adding external resistance to the rotor circuit through slip-rings. Normally a face-plate type starter is used, and as the resistance is gradually reduced, the motor characteristics at each stage changes from the other (John Bird 2010). Hence, the three phase wound rotor (slip ring) induction motor competes favourably with the squirrel cage induction motor counterpart as the most widely used three-phase induction motor for industrial applications. The world-wide popularity and availability of this motor type has attracted a deep – look and in-depth research including its transient behavior under plugging (operating) condition. This paper unveils, through mathematical modeling, followed by dynamic simulation, the transient performance of this peculiar machine, analyzed based on Park’s transformation technique. That is with direct-quadrature-zero (d-q-o) axis based modeling in stationary reference frame. -
Electrical Machines
1 Electrical Machines 1. The left hand rule is applicable to (a) generator ( b) motor (c) transformer ( d) ( a) and ( b) both (e) ( a) or ( b) 2. The eddy current losses in the transformer will be reduced if (a) the laminations are thick (b) number of turns in the primary winding is reduced (c) the number of turns in the secondary winding is reduced (d) the laminations are thin 3. The speed of d.c. series motor at no load is (a) zero ( b) 1500 r.p.m. (c) infinity ( d) 3000 r.p.m. (e) none of the above 4. A sinusoidal voltage of frequency 1 Hz is applied to the field of d.c. generator. The armature voltage will be (a) 1 Hz square wave ( b) 1 Hz sinusoidal voltage (c) d.c. voltage ( d) none of the above 5. The function of the commutator in a d.c. machine is (a) to change alternating current to a direct current (b) to improve commutation (c) for easy control (d) to change alternating voltage to direct voltage 6. The phase sequence of voltage generated in the alternator can be reversed by reversing its field current. (a) true ( b) false 7. The rotation of three phase induction motor can be reversed by interchanging any two of the supply phases. (a) true ( b) false 2 ELECTRICAL ENGINEERING 8. The starting torque of the three phase induction motor can be increased by (a) increasing the rotor reactance (b) increasing the rotor resistance (c) increasing the stator resistance (d) none of the above 9. -
The Role of MHD Turbulence in Magnetic Self-Excitation in The
THE ROLE OF MHD TURBULENCE IN MAGNETIC SELF-EXCITATION: A STUDY OF THE MADISON DYNAMO EXPERIMENT by Mark D. Nornberg A dissertation submitted in partial fulfillment of the requirements for the degree of Doctor of Philosophy (Physics) at the UNIVERSITY OF WISCONSIN–MADISON 2006 °c Copyright by Mark D. Nornberg 2006 All Rights Reserved i For my parents who supported me throughout college and for my wife who supported me throughout graduate school. The rest of my life I dedicate to my daughter Margaret. ii ACKNOWLEDGMENTS I would like to thank my adviser Cary Forest for his guidance and support in the completion of this dissertation. His high expectations and persistence helped drive the work presented in this thesis. I am indebted to him for the many opportunities he provided me to connect with the world-wide dynamo community. I would also like to thank Roch Kendrick for leading the design, construction, and operation of the experiment. He taught me how to do science using nothing but duct tape, Sharpies, and Scotch-Brite. He also raised my appreciation for the artistry of engineer- ing. My thanks also go to the many undergraduate students who assisted in the construction of the experiment, especially Craig Jacobson who performed graduate-level work. My research partner, Erik Spence, deserves particular thanks for his tireless efforts in modeling the experiment. His persnickety emendations were especially appreciated as we entered the publi- cation stage of the experiment. The conversations during our morning commute to the lab will be sorely missed. I never imagined forging such a strong friendship with a colleague, and I hope our families remain close despite great distance. -
NNNNN May 19, 1970 A
May 19, 1970 A. D. APPLETON 3,513,340 HOMOPOLAR ELLCTRIC MACHINES Filed Jan. 6, 1967 2 Sheets-Sheet l -uo Lo NNNNN May 19, 1970 A. D. APPLETON HOMOPOLAR ELECTRIC MACHINES 3,513,340 Filed Jan. 6, 1967 2 Sheets-Sheet 2 222a1a1a2.1274.1444/4/14/a/ 244. A. ZZ 3,513,340 United States Patent Office Patented May 19, 1970 2 3,513,340 FIG. 1 shows diagrammatically a homopolar electrical HOMOPOLAR ELECTRIC MACHINES machine in accordance with the invention for use as a low Anthony Derek Appleton, Newcastle upon Tyne, Eng speed motor, land, assignor to International Research & Develop FIG. 2 is a longitudinal section of a typical machine of Company Limited, Newcastle upon Tyne, Eng the general form illustrated in FIG. 1, and FIG. 3 is a Filed Jan. 6, 1967, Ser. No. 607,784 detail of FIG. 2 on an enlarged scale. Claims priority, application Great Britain, Jan. 12, 1966, The homopolar machine shown in FIG. 1 comprises 1,530/66 two rotors 1 and 2. Int. Cl. H02k 31/00, 47/14 Each rotor is in the from of a disc of electrically con U.S. C. 310-13 10 Claims ducting material Such as copper. The copper discs may O each be mounted on a supporting disc of non-electrically conducting material. ABSTRACT OF THE DISCLOSURE Each rotor rotates within a magnetic field common to A homopolar machine is disclosed having two rotors both rotors and provided by a single superconducting coil in a common magnetic field, preferably provided by a 3, which surrounds the rotors. -
Excitation and Control of a High-Speed Induction Generator
Excitation and Control of a High-Speed Induction Generator by Steven Carl Englebretson S.B., Colorado School of Mines (Dec 2002) Submitted to the Department of Electrical Engineering and Computer Science in partial fulfillment of the requirements for the degree of Master of Science at the MASSACHUSETTS INSTITUTE OF TECHNOLOGY September 2005 @ Massachusetts Institute of Technology, MMV. All rights reserved. A uth or .............................. .. ....... I/.. .. ................. Department of Electrical Engineering and Computer Science August 26, 2005 Certified by ....... .... .............. /1 James L. Kirtley Jr. Professor of Electrical Engineering I Thesis Supervisor Accepted by....................... .............. ............ Arthur C. Smith Chairman, Department Committee on Graduate Students MASSACHUSETTS INSIT=EU OF TECHNOLOGY BARKER MAR 2 8"2006 LIBRARIES - 11 - I Excitation and Control of a High-Speed Induction Generator by Steven Carl Englebretson Submitted to the Department of Electrical Engineering and Computer Science on August 26, 2005, in partial fulfillment of the requirements for the degree of Master of Science Abstract This project investigates the use of a high speed, squirrel cage induction generator and power converter for producing DC electrical power onboard ships and submarines. Potential advantages of high speed induction generators include smaller size and weight, increased durability, and decreased cost and maintenance. Unfortunately, induction generators require a "supply of reactive power" to run and suffer from variation in output voltage and frequency with any changes to the input reactive power excitation, mechanical drive speed, and load. A power converter can resolve some of these issues by circulating the changing reactive power demanded by the generator while simultaneously controlling the stator frequency to adjust the machine slip and manage the real output power. -
Slip Ring Rotor - Vertical
Motors I Automation I Energy I Transmission & Distribution I Coatings Low and high voltage three phase induction motors M line - Slip ring rotor - Vertical Installation, Operation and Maintenance Manual Installation, Operation and Maintenance Manual Document Number: 11734748 Models: MAA, MAP, MAD, MAT, MAV, MAF, MAR, MAI, MAW and MAL Language: English Revision: 9 August 2018 Dear Customer, Thank you for purchasing a WEG motor. Our products are developed with the highest standards of quality and efficiency which ensures outstanding performance. Since electric motors play a major role in the comfort and well-being of mankind, it must be identified and treated as a driving machine with characteristics that involve specific care, such as proper storage, installation and maintenance All efforts have been made to ensure that the information contained in this manual is faithful to the configurations and applications of the motor. Therefore, we recommend that you read this manual carefully before proceeding with the installation, operation or maintenance of the motor in order to ensure safe and reliable operation of your equipment and facility. If you need any further information, please contact WEG. Always keep this manual close to the motor, so that it can be consulted whenever necessary. ATTENTION 1. It is imperative to follow the procedures contained in this manual for the warranty to be valid; 2. The motor installation, operation and maintenance procedures must be performed only by qualified personnel. NOTES 1. The total or partial reproduction of information supplied in this manual is authorized, provided that reference is made to its source. If this manual is lost, an electronic PDF file is available at www.weg.net or another printed copy may be requested. -
ALTERNATORS ➣ Armature Windings ➣ Wye and Delta Connections ➣ Distribution Or Breadth Factor Or Winding Factor Or Spread Factor ➣ Equation of Induced E.M.F
CHAPTER37 Learning Objectives ➣ Basic Principle ➣ Stationary Armature ➣ Rotor ALTERNATORS ➣ Armature Windings ➣ Wye and Delta Connections ➣ Distribution or Breadth Factor or Winding Factor or Spread Factor ➣ Equation of Induced E.M.F. ➣ Factors Affecting Alternator Size ➣ Alternator on Load ➣ Synchronous Reactance ➣ Vector Diagrams of Loaded Alternator ➣ Voltage Regulation ➣ Rothert's M.M.F. or Ampere-turn Method ➣ Zero Power Factor Method or Potier Method ➣ Operation of Salient Pole Synchronous Machine ➣ Power Developed by a Synchonous Generator ➣ Parallel Operation of Alternators ➣ Synchronizing of Alternators ➣ Alternators Connected to Infinite Bus-bars ➣ Synchronizing Torque Tsy ➣ Alternative Expression for Ç Alternator Synchronizing Power ➣ Effect of Unequal Voltages ➣ Distribution of Load ➣ Maximum Power Output ➣ Questions and Answers on Alternators 1402 Electrical Technology 37.1. Basic Principle A.C. generators or alternators (as they are DC generator usually called) operate on the same fundamental principles of electromagnetic induction as d.c. generators. They also consist of an armature winding and a magnetic field. But there is one important difference between the two. Whereas in d.c. generators, the armature rotates and the field system is stationary, the arrangement Single split ring commutator in alternators is just the reverse of it. In their case, standard construction consists of armature winding mounted on a stationary element called stator and field windings on a rotating element called rotor. The details of construction are shown in Fig. 37.1. Fig. 37.1 The stator consists of a cast-iron frame, which supports the armature core, having slots on its inner periphery for housing the armature conductors. The rotor is like a flywheel having alternate N and S poles fixed to its outer rim. -
ELECTRICAL SCIENCE Module 10 AC Generators
DOE Fundamentals ELECTRICAL SCIENCE Module 10 AC Generators Electrical Science AC Generators TABLE OF CONTENTS Table of Co nte nts TABLE OF CONTENTS ................................................................................................... i LIST OF FIGURES ...........................................................................................................ii LIST OF TABLES ............................................................................................................ iii REFERENCES ................................................................................................................iv OBJECTIVES .................................................................................................................. v AC GENERATOR COMPONENTS ................................................................................. 1 Field ............................................................................................................................. 1 Armature ...................................................................................................................... 1 Prime Mover ................................................................................................................ 1 Rotor ............................................................................................................................ 1 Stator ........................................................................................................................... 2 Slip Rings ................................................................................................................... -
Excitation Systems
Excitation Systems 10 kVA - 35 MVA alternators REGULATORS AND EXCITATION SYSTEMS ARE AT THE HEART OF INDUSTRIAL ALTERNATORS PERFORMANCE AND RELIABILITY. At Leroy-Somer, we design, test and qualify our electronic products to meet the challenges of power generation systems. Using our experience and field expertise, we provide regulation features that help protect installations from outage and failures, and our excitation systems are optimized to provide the best performance levels for any situation. EXCITATION SYSTEMS Leroy-Somer offers different excitation systems to match application requirements. An excitation system uses the alternator output to build an excitation current that is then used to power the rotating magnetic field of the rotor. This principle allows for the control of the output power. To build excitation current, a regulator needs both a supply voltage to provide power, and a measured reference voltage at output terminals to pilot the excitation. Alternator Alternator Main power outputMain power User input N Exciter output User input N Exciter U Sensing + U AVRSensing power supply + V AVR power supply AVR V AVR W W AVR outputAVR + - output + - Exciter current STATOR Exciter current STATOR Exciter Diode Exciter bridgeDiode stator bridge stator Prime Power Exciter Power systemPrime ROTOR supply system rotorExciter supply ROTOR rotor Voltage Voltage - sensing - Control sensing Comp. PID Control Exciter Comp. PID command Exciter Ref + command Main power External Ref + Main power referenceExternal reference Diagram of a complete excitation system SHUNT The SHUNT excitation system can also be completed by a booster system for larger installations to allow In SHUNT excitation systems, the AVR power supply for short circuit capability. -
Modeling Ward Leonard Speed Control System
UNIVERSITY OF NAIROBI DEPARTMENT OF ELECTRICAL AND ELECTRONICS ENGINEERING AUTHOR : SEBASTIAN M. MUTHUSI PROJECT CODE : J103 SUPERVISOR : DR. MANG’OLI SUBMISSION DATE : 20TH MAY 2009 PROJECT TITLE : MODELING WARD LEONARD SPEED CONTROL SYSTEM SUBJECT: TO TAKE THE NECESSARY MEASUREMENT AND TO DESIGN AND CONSTRUCT A THREE KILOWART SET. THIS PROJECT IS SUBMITTED IN PARTIAL FULFILMENT FOR THE AWARD OF THE DEGREE OF BSc. ELECTRICAL & ELECTRONIC ENGINEERING, UNIVERSITY OF NAIROBI. ACKNOWLEGEMENT I acknowledge with gratitude the help of; 1. Dr. Mang’oli, my supervisor, Chairman in the Institute of Research and a Senior lecturer in the Department of Electrical and Electronics Engineering in University of Nairobi; for is un-tiring efforts at his supervision and for providing the back ground without which this work could not have been possible. 2. John Githaiga, Kenya Airports Authority Engineer and the Manager in charge of the Engineering Department; for instructing me and giving the authority to operate their systems during their days of maintenance. Also for his cooperation to make sure that the data collected was correct and for is signing and approving it. 3. Mr. Jeremiah, a Senior Electrical Auto Card Teacher at Zetech College; for his kind supervision during the circuit design. 4. The University of Nairobi workshop staff and stores staff; for their cooperation. 5. My sisters Anthea and Sylvia; for their hearty support during the financial challenges. ii Sebastian M. Muthusi ABSTRACT A D.C. Generator is connected in series opposed to the polarity of a D.C. power source supplying a dc. Drive motor. The back ground of the ward Leonard speed control system is explained in chapter two. -
Electrical Engineering
ESE-2016 Answer key of (Objective Paper-II) Electrical Engineering solutions Answer Key of Electrical Engg. Objective Paper-II (ESE - 2016) SET - A 1. Compared to the salient-pole Hydroelectric 4. The regulation of a transformer in which ohmic generators, the steam and the gas-turbine have loss is 1% of the output and reactance drop is cylindrical rotors for 5% of the voltage, when operating at 0.8 power factor lagging, is (a) Better air-circulation in the machine (a) 3.8% (b) 4.8% (b) Reducing the eddy-current losses in the rotor (c) 5.2% (d) 5.8% (c) Accommodating larger number of turns in Sol. (a) the field winding 5. In a power transformer, the core loss is 50 W (d) Providing higher mechanical strength at 40 Hz and 100 W at 60 Hz, under the against the centrifugal stress condition of same maximum flux density in both Sol. (d) cases. The core loss at 50 Hz will be 2. Consider the following losses for short circuit (a) 64 W (b) 73 W test on a transformer: (c) 82 W (d) 91 W 1. Copper loss Sol. (b) 2. Copper and iron losses 6. Consider the following advantages of a 3. Eddy current and hysteresis losses distributed winding in a rotating machine: 4. Friction and windage losses 1. Better utilization of core as a number of evenly placed small slots are used Which of the above is/are correct ? 2. Improved waveform as harmonic emf’s are (a) 1 only (b) 2 only reduced (c) 3 only (d) 2, 3 and 4 3. -
EXPERIMENTAL LIQUID METAL SLIP RING PROJECT by R. B. Clark HUGHES AIRCRAFT COMPANY Prepared for NATIONAL AERONAUTICS and SPACE A
NASA CR-.72780 EXPERIMENTAL LIQUID METAL SLIP RING PROJECT by R. B. Clark HUGHES AIRCRAFT COMPANY prepared for NATIONAL AERONAUTICS AND SPACE ADMINISTRATION NASA Lewis Research Center Contract NAS 3-1 1537 Robert R. Lovell, Project Manager I NOTICE I This report was prepared as an account of Government-sponsored work, Neither the United States, nor the National Aeronautics and Space Administration (NASA), nor any person acting on behalf of NASA: A. ) Makes any warranty or representation, expressed or implied, with respect to the accuracy, completeness, or usefulness of the information contained in this report, or that the use of any information, apparatus, method, or process disclosed in this report may not infringe privately-owned rights; or B. ) Assumes any liabilities with respect to the use of, or for damages resulting from the use of, any information, apparatus, method or process disclosed in this report. As used above, "person acting on behalf of NASA" includes any employee or contractor of NASA, or employee of such contractor, to the extent that such employee or contractor of NASA or employee of such contractor prepares, disseminates, or provides access to any information pursuant to his employment or contract with NASA, or his employment with such contractor. Requests for copies of this report should be referred to National Aeronautics and Space Administration Scientific and Technical Information Facility P. 0. Box 33 College Park, Md. 20740 NASA CR-72780 FINAL REPORT EXPERIMENTAL LIQUID METAL SLIP RING PROJECT R. B. Clark HUGHES AIRCRAFT COMPANY Space Systems Division Los Angeles, California 90009 prepared for NATIONAL AERONAUTICS AND SPACE ADMINISTRATION June 22, 1970 Contract NAS 3-1 1537 NASA Lewis Research Center Cleveland, Ohio Robert R.