DOCSLIB.ORG

Characteristics of Linear Alternator Performance Under Thermoacoustic-Power- Conversion Conditions

Total Page：16

File Type：pdf, Size：1020Kb

Download full-text PDF Read full-text
Characteristics of Linear Alternator Performance Under Thermoacoustic-Power- Conversion Conditions THE AMERICAN UNIVERSITY IN CAIRO SCHOOL OF SCIENCES AND ENGINEERING CHARACTERISTICS OF LINEAR ALTERNATOR PERFORMANCE UNDER THERMOACOUSTIC-POWER- CONVERSION CONDITIONS BY AHMED YASSIN ABDELWAHED IBRAHIM A thesis submitted in partial fulfillment of the requirements for the degree of Master of Science in Mechanical Engineering Under the supervision of: Prof. Ehab Abdel-Rahman Professor, Physics Department The American University in Cairo Prof. Mohamed Amr Serag Eldin Professor, Mechanical Engineering Department The American University in Cairo Dr. Abdelmaged Hafez Ibrahim Essawey Research Post-Doctoral Scholar The American University in Cairo November 2018 Acknowledgement The work that this thesis encompasses was made possible with the support of many individuals and organizations. First of all, I would like to thank my advisor Prof. Ehab Abdel- Rahman the head of the Thermoacoustics research team who provided me and the rest of the team with the needed scientific guidance and advanced facilities in the Thermoacoustic Research Lab throughout many years of research. Thanks also to my advisor Prof. Mohamed Amr Serag-Eldein who helped me a lot with his long and strong experience in the renewable energy field to produce this thesis work. For sure I would like to thank my advisor Dr. Abdelmaged H. Ibrahim Essawey whose experience, flexibility, technical guidance, and day-to-day follow up helped me produce the results of this work and made it easier to get over the many barriers in the field of the Thermoacoustics and linear alternators. I also have a great deal of gratitude for Prof. Steven Garrett (Penn State University) and Dr. Kai Wang (Imperial College) whom knowledge and experience in thermoacoustic engines and their applications are great. Their prompt replies on my questions enabled me to significantly enhance the analytical model. Additionally, for sure I would like to thank Prof. Gregory W. Swift (Los Alamos Labs) for his great help in the modeling of the load resistance and the power-factor- correcting capacitor in DELTAEC software. I am very thankful to John Corey, Phillip Spoor and Gordon Miller of Q-Drive (Rix Industries, Chart Industries in the past) for the technical support they provided on many aspects of linear alternators. For sure, I would like to thank Dr. Islam Ramadan who assisted on the numerical simulations using DELTAEC software, Eng. Moamen Bellah Abdelmawgoud who built the initial form of the experimental setup, and Eng. Khaled El Beltagey who assisted in the development of the experimental setup along the years. I am also thankful to every member in the thermoacoustic research team for the fruitful discussions, technical support, and the great time I had during this research period. The American University in Cairo provided access to numerous scientific resources, a research grant, and two conference grants that enabled me to greatly develop this work and assisted II in the building, continuous and smooth running of the experimental setup and presenting nine publications in international conferences and meetings. This work was possible with the financial assistance of the European Union. The contents of this document are the sole responsibility of the master student and can under no circumstances be regarded as reflecting the position of the European Union. I am very thankful for the Egyptian Academy of Scientific Research and Technology which partly funded the development of the initial form of the experimental setup used. This work is a new step of my research work in the space systems field that I have started under supervision of Dr.Mohammed Khalil Ibrahim, Prof. Atef Omar Sherif, Prof.Bahy-El Dein Argon and Dr.Ayman Kassem in Space Systems Technology Laboratory (SSTL), aerospace engineering department-Cairo University. I would like to thank all of these professors and the previous leader of this laboratory Eng.Samy Amin (Avelabs). Many thanks go to my parents (Dr.Yassin Ibrahim and Mrs.Hanim El Saadany) who give me all what they have of love and support. III Contents Acknowledgement .......................................................................................................................... II Contents ........................................................................................................................................ IV List of Figures .............................................................................................................................. VII List of Tables ................................................................................................................................ XI Nomenclature ............................................................................................................................... XII Abstract ........................................................................................................................................ XV 1. Introduction .............................................................................................................................. 1 1.1 Thermoacoustic Engines .................................................................................................. 1 1.1.1 Standing wave thermoacoustic engine ...................................................................... 1 1.1.1.1 Standing wave thermoacoustic engine components .............................................. 2 1.1.1.1.1 Heat source ............................................................................................................ 2 1.1.1.1.2 Heat exchanger ...................................................................................................... 3 1.1.1.1.3 Stack ...................................................................................................................... 3 1.1.1.1.4 Working Gas ......................................................................................................... 3 1.1.1.1.5 Resonator ............................................................................................................... 3 1.1.2 Travelling wave thermoacoustic engine ................................................................... 4 1.1.1.2 Travelling wave thermoacoustic engine components ........................................... 6 1.1.1.2.1 Main cold and hot heat exchangers ....................................................................... 6 1.1.1.2.2 Regenerator ........................................................................................................... 6 1.1.1.2.3 Thermal buffer tube (TBT) ................................................................................... 7 1.1.1.2.4 Secondary cold heat exchanger ............................................................................. 7 1.1.1.2.5 Feedback inertance tube ........................................................................................ 7 1.1.1.2.6 Compliance............................................................................................................ 7 1.1.1.2.7 Jet pump ................................................................................................................ 7 1.1.3 Advantages and limitations of thermoacoustic engines ............................................ 8 1.2 Linear Alternators ............................................................................................................ 9 1.2.1 Types of linear alternators ........................................................................................ 9 1.2.2 Advantages and limitations of moving magnet linear alternators .......................... 11 1.2.3 Linear alternators’ connections in thermoacoustic power converters ..................... 16 IV 1.2.4 Anti-drift network across the linear alternator’s piston .......................................... 17 1.3 Thesis Scope ................................................................................................................... 19 2. Literature Review .................................................................................................................. 21 3. Experimental Setup and DELTAEC Simulations .................................................................. 27 3.1 DELTAEC Simulations.................................................................................................. 35 4. Results: Analytical Model ..................................................................................................... 37 4.1 Analytical Model Derivation .......................................................................................... 37 4.1.1 Estimation of linear alternator performance indices ............................................... 41 4.1.2 Estimation of effective coil inductance................................................................... 46 4.2 Analytical Model Validation .......................................................................................... 49 4.3 Optimization of Piston Area and Load Resistance......................................................... 53 4.4 Summary of Analytical Model Results .......................................................................... 56 5. Results: Experimental Parametric Study ............................................................................... 59 5.1 Experimental Parametric Study under Linear Load Condition ...................................... 60 5.1.1 Effects of the operating frequency .......................................................................... 62 5.1.2 Effects of the
Load more

Recommended publications
  • A BRIEF INTRODUCTION to TUBULAR LINEAR MOTORS Linear Motors Provide Direct Thrust for Positioning a Payload, Eliminating the Need for Rotary-To-Linear Conversion
    PRODUCT OVERVIEW – DIRECT-DRIVE LINEAR MOTOR SYSTEMS A BRIEF INTRODUCTION TO TUBULAR LINEAR MOTORS Linear motors provide direct thrust for positioning a payload, eliminating the need for rotary-to-linear conversion. The three main direct-drive linear motion systems on the market today – iron-core, U-channel, and tubular linear motors – each have distinct advantages and disadvantages with respect to specific applications, for example regarding form factor, achievable force density, and efficiency. Understanding the differences will enable a designer to select the best motor option. Iron-core motor • Magnetic saturation The basic structure of the iron-core motor (Figure 1) is When the generated forces are pushed beyond the similar to that of an unrolled rotary motor with discrete normal operating range, the iron will reach magnetic stator and magnetic poles. It has a set of electromagnetic saturation and the force-to-current relationship coils wrapped around an iron core. The end effect of this is becomes non-linear, making control more difficult. to increase the amount of magnetic field generated by the • Large footprint coils, as the iron will contribute to the generated field The basic construction of iron-core motors requires a through realigning microscopic magnetic domains in the fairly large footprint. iron with the magnetic field from the coils. This is the major • Lateral and attractive (non-useful) forces advantage of the iron-core motor: for a given input of These forces are inherent to the motor design and current, a significant amount of force can be generated. require additional constraints. However, there are some disadvantages/behaviours that U-channel motor have to be considered: One of the main features of the U-channel motor (Figure 2) • Cogging is the absence of iron from the critical locations in the This is the movement of the motor’s iron forcer so as to motor.
    [Show full text]
  • High Speed Linear Induction Motor Efficiency Optimization
    Calhoun: The NPS Institutional Archive Theses and Dissertations Thesis Collection 2005-06 High speed linear induction motor efficiency optimization Johnson, Andrew P. (Andrew Peter) http://hdl.handle.net/10945/11052 High Speed Linear Induction Motor Efficiency Optimization by Andrew P. Johnson B.S. Electrical Engineering SUNY Buffalo, 1994 Submitted to the Department of Ocean Engineering and the Department of Electrical Engineering and Computer Science in Partial Fulfillment of the Requirements for the Degree of Naval Engineer and Master of Science in Electrical Engineering and Computer Science at the Massachusetts Institute of Technology June 2005 ©Andrew P. Johnson, all rights reserved. MIT hereby grants the U.S. Government permission to reproduce and to distribute publicly paper and electronic copies of this thesis document in whole or in part. Signature of A uthor ................ ............................... D.epartment of Ocean Engineering May 7, 2005 Certified by. ..... ........James .... ... ....... ... L. Kirtley, Jr. Professor of Electrical Engineering // Thesis Supervisor Certified by......................•........... ...... ........................S•:• Timothy J. McCoy ssoci t Professor of Naval Construction and Engineering Thesis Reader Accepted by ................................................. Michael S. Triantafyllou /,--...- Chai -ommittee on Graduate Students - Depa fnO' cean Engineering Accepted by . .......... .... .....-............ .............. Arthur C. Smith Chairman, Committee on Graduate Students DISTRIBUTION
    [Show full text]
  • Industrial Linear Motors
    Industrial Linear Motors Smart solutions are driven by PRODUCT OVERVIEW www.linmot.com Precision and dynamics In the products and in the everyday life of NTI AG, these values ​​are inseparable. NTI AG NTI AG is a global manufacturer of high quality tubular style linear motors and linear motor systems and thus focuses on the development, production and distribution of linear direct drives for use in industrial environments. Founded in 1993 as an independent business unit of the Sulzer Group, NTI AG has been in operation since 2000 as an independent company. NTI AG headquarters are located in Spreitenbach, near Zurich in Switzerland. In addition to three production sites in Switzerland and Slovakia, NTI AG maintains a sales and support office LinMot® USA Inc. to cover the Americas. Mission The brands LinMot® for industrial linear motors and MagSpring® for magnetic springs are offered LinMot offers its customers a sophisticated and dedicated linear to customers worldwide. NTI AG drive system that can be easily integrated into all leading control maintains an experienced customer systems. A high degree of standardization, delivery from stock and consultant sales and support a worldwide distribution network insure the immediate availability network of over 80 locations and excellent customer support. worldwide. For the realization of linear motion Our aim is to push linear direct drive technology and make it a NTI AG is always a competent and standard machine design element. We offer highly efficient drive reliable partner. solutions that make a major contribution to the overall resource conservation effort. 2 3 Linear Motors Position and Temperature sensors Electronic nameplate Stator Winding Slider with Neodynium Magnets Payload Mounting LinMot linear motors employ a direct electromagnetic principle.
    [Show full text]
  • Methods for Improving Efficiency of Linear Induction Motor for Urban
    512 Methods for Improving Efficiency of Linear Induction Motor for Urban Transit∗ Nobuo FUJII∗∗, Toshiyuki HOSHI∗∗ and Yuichi TANABE∗∗ To improve the efficiency of the linear induction motors (LIMs) for transportation, the compensation of end effect for LIM with the restriction of length and the long LIM with small end effect essentially are discussed respectively. Based on the proposed concept, the com- pensation method of the magnet rotator type and AC coil type of compensators are developed respectively. The utility is not yet confirmed. As for the long LIM with length of 10 m, the analysis shows that the efficiencies are about 85% at 40 km/h and above 90% at 360 km/h respectively. Key Words: Linear Motor, Linear Induction Motor, LIM, Linear Drives, Transportation, Traction, Subway, Electromagnetic Analysis, End Effect, Compensator length of LIM, the compensation of end effect is the only 1. Introduction method for remarkable improve of the characteristics. The In a part of new type transit, linear induction motors compensating winding method was proposed previous- (1) ff (LIMs) have been used as a direct electromagnetic drive ly , but it was not e ective. The authors have proposed ff (2) device without adhesion. In Japan, the LIM-driven train the new type of end e ect compensator . The proposed ff has been used in the subway in some large cities, as the method is based on the new concept that the end e ect can LIM reduces the construction cost of tunnel because the be compensated only by supplying the eddy current syn- thin shape makes the sectional area of tunnel small and the chronizing with the LIM frequency in front of LIM, which large gradability enables the minimum length of the route.
    [Show full text]
  • Electromagnetic Launcher: Review of Various Structures
    Published by : International Journal of Engineering Research & Technology (IJERT) http://www.ijert.org ISSN: 2278-0181 Vol. 9 Issue 09, September-2020 Electromagnetic Launcher : Review of Various Structures Siddhi Santosh Reelkar Prof. Dr. U. V. Patil Department of Electrical Engineering, Department of Electrical Engineering, Government College of Engineering, Government College of Engineering, Karad Karad Prof. Dr. V. V. Khatavkar Department of Electrical Engineering, P.E.S. Modern college of Engineering, Pune Hrishikesh Mehta Utkarsh Alset Aethertec Innovative Solutions, Aethertec Innovative Solutions, Bavdhan, Pune Bavdhan, Pune Abstract— A theoretic review of electromagnetic coil-gun This paper is mainly focusing the basic principle of launcher and its types are illustrated in this paper. In recent electromagnetic coil-gun launcher, inductance and resistance years conventional launchers like steam launchers, chemical calculations, construction and modeling concept of different launchers are replaced by electromagnetic launchers with coil-gun launcher. auxiliary benefits. The electromagnetic launchers like rail- gun and coil-gun elevated with multi pole field structure delivers II. WORKING PRINCIPLE great muzzle velocity and huge repulse force in limited time. Rail gun has two parallel rails from which object is launched. Various types of coil-gun electromagnetic launchers are When current passes through the rails to the object it compared in this paper for its structures and characteristics. The paper focuses on the basic formulae for calculating the produces arc. Because of high current pulse it has more values of inductance and resistance of electromagnetic contact friction losses [4]. Compare to the rail-gun launcher, launchers. Coil-gun launchers have no contact friction losses as there is no electrical contact between coils and object.
    [Show full text]
  • Linear Induction Motor
    Linear Induction Motor Electrical and Computer Engineering Tyler Berchtold, Mason Biernat and Tim Zastawny Project Advisor: Professor Steven Gutschlag 4/21/2016 2 Outline of Presentation • Background and Project Overview • Microcontroller System • Final Design • Economic Analysis • Hardware • State of Work Completed • Conclusion 3 Outline of Presentation • Background and Project Overview • Microcontroller System • Final Design • Economic Analysis • Hardware • State of Work Completed • Conclusion 4 Alternating Current Induction Machines • Most common AC machine in industry • Produces magnetic fields in an infinite loop of rotary motion • Current-carrying coils create a rotating magnetic field • Stator wrapped around rotor [1] [2] 5 Rotary To Linear [3] 6 Linear Induction Motor Background • Alternating Current (AC) electric motor • Powered by a three phase voltage scheme • Force and motion are produced by a linearly moving magnetic field • Used in industry for linear motion and to turn large diameter wheels [4] 7 Project Overview • Design, construct, and test a linear induction motor (LIM) • Powered by a three-phase voltage input • Rotate a simulated linear track and cannot exceed 1,200 RPM • Monitor speed, output power, and input frequency • Controllable output speed [5] 8 Initial Design Process • Linear to Rotary Model • 0.4572 [m] diameter 퐿 = 훳푟 (1.1) • 0.3048 [m] arbitrary stator length • Stator contour designed for a small air gap • Arc length determined from stator length and diameter • Converted arc length from a linear motor to the circumference of a rotary motor • Used rotary equations to determine required [6] frequency and verify number of poles 9 Rotational to Linear Speed (1.2) (1.3) 10 Pole Pitch and Speed (1.4) • For fixed length stator τ= L/p • L = Arc Length τ A B C A B C [7] 11 Linear Synchronous Speed Ideal Linear Synchronous Speed vs.
    [Show full text]
  • Molecular Dynamics Simulations of a Linear Nanomotor Driven by Thermophoretic Forces
    Downloaded from orbit.dtu.dk on: Oct 05, 2021 Molecular Dynamics Simulations of a Linear Nanomotor Driven by Thermophoretic Forces Zambrano, Harvey A; Walther, Jens Honore; Jaffe, Richard L. Publication date: 2009 Document Version Publisher's PDF, also known as Version of record Link back to DTU Orbit Citation (APA): Zambrano, H. A., Walther, J. H., & Jaffe, R. L. (2009). Molecular Dynamics Simulations of a Linear Nanomotor Driven by Thermophoretic Forces. Poster session presented at NanoEurope Symposium 2009 : Moving Nanotechnology to Market, Rapperswil, Switzerland. General rights Copyright and moral rights for the publications made accessible in the public portal are retained by the authors and/or other copyright owners and it is a condition of accessing publications that users recognise and abide by the legal requirements associated with these rights. Users may download and print one copy of any publication from the public portal for the purpose of private study or research. You may not further distribute the material or use it for any profit-making activity or commercial gain You may freely distribute the URL identifying the publication in the public portal If you believe that this document breaches copyright please contact us providing details, and we will remove access to the work immediately and investigate your claim. Molecular Dynamics Simulations of a Linear Nanomotor Driven by Thermophoretic Forces Harvey A. Zambranoa, Jens H. Walthera,b and Richard L. Jaffec aDepartment of Mechanical Engineering, DTU, Denmark. bChair of Computational Science, ETH Zurich, Switzerland. cNASA Ames Research Center, Moffett Field, CA 94035, USA. We conduct molecular dynamics simulations of a molecular linear motor consisting of coaxial carbon nanotubes with a long outer carbon nanotube confining and guiding the motion of an inner short, capsule-like nanotube.
    [Show full text]
  • Linear Motors Innovative Motion Control
    Linear Motors Innovative Motion Control ABOUT ETEL LINEAR MOTORS What is a linear motor? Linear motors are a special class of synchronous brushless servo motors. They work like torque Over the last 20 years, direct drive linear motors have provided significant performance motors, but are opened up and rolled out flat. Through the electromagnetic interaction between improvements in numerous applications covering a wide range of high-tech industries. Today, a coil assembly (primary part) and a permanent magnet assembly (secondary part), the electrical direct drive technology is recognized as a leading solution towards meeting the requirements of energy is converted to linear mechanical energy with a high level of efficiency. Other common high productivity, improved accuracy, and increased dynamics of modern machinery. names for the primary component are motor, moving part, slider or glider, while the secondary part is also called magnetic way or magnet track. Direct drive essentially means the load and motor are directly connected; or in other words, the motor “directly drives” the load. Significant improvement to stiffness and a more compact solution Since linear motors are designed to produce high force at low speeds or even when stationary, are among the benefits of this technology. In addition to providing high dynamic performance, the sizing is not based on power but purely on force, contrary to traditional drives. linear motors reduce cost of ownership, simplify the design of the machine and eliminate wear and maintenance. The moving part of a linear motor is directly coupled to the machine load, saving space, simplifying machine design, eliminating backlash, and removing potential failure sources such as Since its founding in 1974, ETEL has been exclusively dedicated to the development of direct ballscrew systems, couplings, belts, or other mechanical transmissions.
    [Show full text]
  • Piezoelectric Inertia Motors—A Critical Review of History, Concepts, Design, Applications, and Perspectives
    Review Piezoelectric Inertia Motors—A Critical Review of History, Concepts, Design, Applications, and Perspectives Matthias Hunstig Grube 14, 33098 Paderborn, Germany; [email protected] Academic Editor: Delbert Tesar Received: 26 November 2016; Accepted: 18 January 2017; Published: 6 February 2017 Abstract: Piezoelectric inertia motors—also known as stick-slip motors or (smooth) impact drives—use the inertia of a body to drive it in small steps by means of an uninterrupted friction contact. In addition to the typical advantages of piezoelectric motors, they are especially suited for miniaturisation due to their simple structure and inherent fine-positioning capability. Originally developed for positioning in microscopy in the 1980s, they have nowadays also found application in mass-produced consumer goods. Recent research results are likely to enable more applications of piezoelectric inertia motors in the future. This contribution gives a critical overview of their historical development, functional principles, and related terminology. The most relevant aspects regarding their design—i.e., friction contact, solid state actuator, and electrical excitation—are discussed, including aspects of control and simulation. The article closes with an outlook on possible future developments and research perspectives. Keywords: inertia motor; stick-slip motor; smooth impact drive; piezeoelectric motor; review 1. Introduction Piezoelectric actuators have long been used in diverse applications, especially because of their short response time and high resolution. The major drawback of these solid state actuators in positioning applications is their small stroke: actuators made of state-of-the-art lead zirconate titanate (PZT) ceramics only reach strains up to 2 . A typical piezoelectric actuator with 10 mm length thus reaches a maximum stroke of only 20 µm.h Bending actuator designs [1] and other mechanisms [2] can increase the stroke at the expense of stiffness and actuation force ([3]; [4] (pp.
    [Show full text]
  • Linear Motor for Linear Compressor K
    Purdue University Purdue e-Pubs International Compressor Engineering Conference School of Mechanical Engineering 2002 Linear Motor For Linear Compressor K. Park LG Electronics Inc. E. Hong LG Electronics Inc. H. K. Lee LG Electronics Inc. Follow this and additional works at: https://docs.lib.purdue.edu/icec Park, K.; Hong, E.; and Lee, H. K., " Linear Motor For Linear Compressor " (2002). International Compressor Engineering Conference. Paper 1544. https://docs.lib.purdue.edu/icec/1544 This document has been made available through Purdue e-Pubs, a service of the Purdue University Libraries. Please contact [email protected] for additional information. Complete proceedings may be acquired in print and on CD-ROM directly from the Ray W. Herrick Laboratories at https://engineering.purdue.edu/ Herrick/Events/orderlit.html C12-1 LINEAR MOTOR FOR LINEAR COMPRESSOR *Kyeongbae Park, Senior Research Engineer, Digital Appliance Laboratory, LG Electronics Inc, 327-23 Gasan-dong, Geumchen-gu, Seoul, Korea; Phone: 82-2-818-7953, Email: [email protected] Eunpyo Hong, Senior Research Engineer, Digital Appliance Laboratory, LG Electronics Inc, 327-23 Gasan-dong, Geumchen-gu, Seoul, Korea; Phone: 82-2-818-7950, Email: [email protected] Hyeong-Kook Lee, Chief Research Engineer, Digital Appliance Laboratory, LG Electronics Inc, 327-23 Gasan-dong, Geumchen-gu, Seoul, Korea; Phone: 82-2-818-3502, Email: [email protected] ABSTRACT In contrast to the conventional rotational compressors, the linear compressor is driven by a linear motor directly coupled with a piston. So the performance of the linear compressor is strongly dependent on the characteristics of the linear motor. In addition to high efficiency, the parameters of a linear motor should be nearly constant regardless of the amount of the current flow and position of the piston in order to control the position of piston without an additional sensor.
    [Show full text]
  • Development of a Low-Inductance Linear Alternator for Stirling Power Convertors
    NASA/TM—2017-219699 AIAA–2017–4961 Development of a Low-Inductance Linear Alternator for Stirling Power Convertors Steven M. Geng and Nicholas A. Schifer Glenn Research Center, Cleveland, Ohio November 2017 NASA STI Program . in Profile Since its founding, NASA has been dedicated • CONTRACTOR REPORT. Scientific and to the advancement of aeronautics and space science. technical findings by NASA-sponsored The NASA Scientific and Technical Information (STI) contractors and grantees. Program plays a key part in helping NASA maintain this important role. • CONFERENCE PUBLICATION. Collected papers from scientific and technical conferences, symposia, seminars, or other The NASA STI Program operates under the auspices meetings sponsored or co-sponsored by NASA. of the Agency Chief Information Officer. It collects, organizes, provides for archiving, and disseminates • SPECIAL PUBLICATION. Scientific, NASA’s STI. The NASA STI Program provides access technical, or historical information from to the NASA Technical Report Server—Registered NASA programs, projects, and missions, often (NTRS Reg) and NASA Technical Report Server— concerned with subjects having substantial Public (NTRS) thus providing one of the largest public interest. collections of aeronautical and space science STI in the world. Results are published in both non-NASA • TECHNICAL TRANSLATION. English- channels and by NASA in the NASA STI Report language translations of foreign scientific and Series, which includes the following report types: technical material pertinent to NASA’s mission. • TECHNICAL PUBLICATION. Reports of For more information about the NASA STI completed research or a major significant phase program, see the following: of research that present the results of NASA programs and include extensive data or theoretical • Access the NASA STI program home page at analysis.
    [Show full text]
  • Development of Resonating Oscillating Linear Engine Alternator; Instrumentation and Control
    Graduate Theses, Dissertations, and Problem Reports 2018 Development of Resonating Oscillating Linear Engine Alternator; Instrumentation and Control Fereshteh Mahmudzadeh Follow this and additional works at: https://researchrepository.wvu.edu/etd Recommended Citation Mahmudzadeh, Fereshteh, "Development of Resonating Oscillating Linear Engine Alternator; Instrumentation and Control" (2018). Graduate Theses, Dissertations, and Problem Reports. 7211. https://researchrepository.wvu.edu/etd/7211 This Thesis is protected by copyright and/or related rights. It has been brought to you by the The Research Repository @ WVU with permission from the rights-holder(s). You are free to use this Thesis in any way that is permitted by the copyright and related rights legislation that applies to your use. For other uses you must obtain permission from the rights-holder(s) directly, unless additional rights are indicated by a Creative Commons license in the record and/ or on the work itself. This Thesis has been accepted for inclusion in WVU Graduate Theses, Dissertations, and Problem Reports collection by an authorized administrator of The Research Repository @ WVU. For more information, please contact [email protected]. Development of Resonating Oscillating Linear Engine Alternator; Instrumentation and Control Fereshteh Mahmudzadeh Thesis submitted to the College of Engineering and Mineral Resources at West Virginia University in partial fulfillment of the requirements for the degree of Master of Science In Electrical Engineering Parviz Famouri, Ph.D., Chair Muhammad A. Choudhry, Ph.D. Katerina Goseva-Popstojanova, Ph.D. Lane Department of Computer Science and Electrical Engineering Morgantown, West Virginia 2018 Keywords: Linear Engine Alternator, Control Copyright 2018 Fereshteh Mahmudzadeh Abstract Development of Resonating Oscillating Linear Engine Alternator; Instrumentation and Control Fereshteh Mahmudzadeh The Oscillating Linear Engine and Alternator (OLEA) machine is a micro power generator that operates on natural gas.
    [Show full text]