Ny Gasturbinteknik 2012-2014 Gas Turbine Developments Rapport 2013
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Full Speed String Test on GE LM6000PF Gas Turbine
FULL SPEED STRING TEST ON LM6000PF GAS TURBINE DRIVEN REFRIGERATION COMPRESSORS Sameer S. Patwardhan Mark Weatherwax Lead Machinery Engineer Consulting Machinery Engineer Bechtel Oil, Gas & Chemical Chevron Energy Technology Company Houston, Texas, USA Perth, WA, Australia Feroze Meher-Homji Davide Cappetti Principal Rotating Equipment Engineer Special Projects & LNG Lead Project Engineer Bechtel Oil, Gas & Chemical GE Oil & Gas Houston, Texas, USA Florence, Italy Antonio Musardo Gianni Iannuzzi Natural Gas Project Engineering Manager Special Testing Design Engineering Manager GE Oil & Gas GE Oil & Gas Florence, Italy Florence, Italy Sameer S. Patwardhan is the Senior/Lead Rotating Machinery Engineer for Bechtel Oil, Gas and Chemical, Inc. in Houston, Texas. His current responsibilities include Leading a team of rotating machinery engineers on a LNG project, Responsible Engineer for the main Refrigeration Compressors and Gas Turbine Generators on the Wheatstone LNG project and Selection, design, and testing of new rotating equipment along with the start-up, commissioning and troubleshooting support for new and existing equipment. Mr. Patwardhan has more than 12 years of experience with rotating equipment and engineering design. Prior to joining Bechtel in 2005, he was employed by General Electric Energy. Mr. Patwardhan has a B.E. degree in Mechanical Engineering from Pune University, India, a M.S. degree in Mechanical Engineering from State University of New York at Buffalo and a M.B.A. in Energy Management from the University of Houston. He is currently Chairman of the API 613 Task Force and an active task force member of API 692, 672, 617 and 614. He is also a Professional Engineer in the State of Texas. -
Complete Notes Of
LECTURER NOTES ON POWER PLANT ENGINEERING 1 POWER PLANT ENGINEERING UNIT-I INTRODUCTION TO POWER PLANTs STEAM POWER PLANT: A thermal power station is a power plant in which the prime mover is steam driven. Water is heated, turns into steam and spins a steam turbine which drives an electrical generator. After it passes through the turbine, the steam is condensed in a condenser and recycled to where it was heated; this is known as a Rankine cycle. The greatest variation in the design of thermal power stations is due to the different fuel sources. Some prefer to use the term energy center because such facilities convert forms of heat energy into electricity. Some thermal power plants also deliver heat energy for industrial purposes, for district heating, or for desalination of water as well as delivering electrical power. A large proportion of CO2 is produced by the worlds fossil fired thermal power plants; efforts to reduce these outputs are various and widespread. 2 The four main circuits one would come across in any thermal power plant layout are -Coal andAshCircuit -AirandGasCircuit Feed Water and Steam Circuit Cooling Water Circuit Coal and Ash Circuit Coal and Ash circuit in a thermal power plant layout mainly takes care of feeding the boiler with coal from the storage for combustion. The ash that is generated during combustion is collected at the back of the boiler and removed to the ash storage by scrap conveyors. The combustion in the Coal and Ash circuit is controlled by regulating the speed and the quality of coal entering the grate and the damper openings. -
Y ...Signature Redacted
Modeling Brake Specific Fuel Consumption to Support Exploration of Doubly Fed Electric Machines in Naval Engineering Applications by Michael R. Rowles, Jr. B.E., Electrical Engineering, Naval Architecture, State University of New York, Maritime College, 2006 Submitted to the Department of Mechanical Engineering in Partial Fulfillment of the Requirements for the Degrees of Naval Engineer and Master of Science in Naval Architecture and Marine Engineering at the MASSACHUSETTS INSTITUTE OF TECHNOLOGY June 2016. 2016 Michael R. Rowles, Jr. All rights reserved. The author hereby grants to MIT permission to reproduce and to distribute publicly paper and electronic copies of this thesis document in whole or in part in any medium now known or hereafter c: A uth or ........................................... Signature redacted Department of Mechanical Engineering A may 22,k 2016 C ertified by ............................ Signature redacted .... Weston L. Gray, CDR, USN Associate Professor of the Practice, Naval Construction and Engineering redacted ..Thesis Reader Certified by .......... Signature Ll James L. Kirtley Professor of Electrical Engineering redacted Isis Supervisor Accepted by ............ SSignatu gnatu re ...................... Rohan Abeyaratne MASSACHUSETTS INSTITUTE Chairman, Committee on Graduate Students OF TECHNOLOGY Quentin Berg Professor of Mechanics Department of Mechanical Engineering JUN 02 2016 LIBRARIES ARCHIVES Modeling Brake Specific Fuel Consumption to Support Exploration of Doubly Fed Electric Machines in Naval Engineering Applications by Michael R. Rowles, Jr. Submitted to the Department of Mechanical Engineering on May 12, 2016 in Partial Fulfillment of the Requirements for Degrees of Naval Engineer and Master of Science in Mechanical Engineering Abstract The dynamic operational nature of naval power and propulsion requires Ship Design and Program Managers to design and select prime movers using a much more complex speed profile rather than typical of commercial vessels. -
PATROL COMBATANT MISSILE HYDROFOIL- DESIGN DEVELOPMENT and PRODUCTION- a BRIEF HISTORY by David S
PATROL COMBATANT MISSILE HYDROFOIL- DESIGN DEVELOPMENT AND PRODUCTION- A BRIEF HISTORY by David S. Oiling and Richard G. Merritt Boeing Marine Systems Published as Boeing Document 0312-80948-1, December 1980, and in the January-February issue of IIHigh-Speed Surface Craft," London ABOUT THE AUTHORS DAVID S. OLLING - Mechanical Specialist Engineer, PHM Variants Preliminary Design BS, Mechanical Engineering, University of Washington, 1967 With Boeing 21 years o 17 years in Advanced Marine Systems design, preliminary design, engineering liaison and testing organizations RICHARD G. MERRITT - Manager of PHM Variants Preliminary Design BS, Civil Engineering, Yale University, 1950 MS, Civil Engineering, California Institute of Technology, 1951 Degree of Civil Engineer, California Institute of Technology, 1953 Executive Program in Business Administration, Columbia University, 1967 With Boeing 17 years o 1 year as engineer with U.S. Naval Ordnance Test Station, Pasadena, before joining Boeing. o 6 years on airplane and missile system structural research. o 21 years in advanced marine system technology management, including supervision of hydrofoil technology staff, project design, and preliminary design groups. o Member of American Institute of Aeronautics and Astronautics, serving on AIAA technical committee on marine systems and technology. o Author of 12 articles in scientific and professional journals. PATROL COMBATANT MISSILE (HYDROFOIL) Design, Development and Production - A Brief History by David S. OUing and Richard G. Merritt, Boeing Marine Systems INTRODUCTION 1974. Its completion (PHM 2) was later incorporated into the production program, In 1972 three NATO navies formally agreed reference 3. to proceed with the joint development of a warship pro ject. The United States took the Major Events leadership before the "Memorandum of Understanding" was signed by the Federal Developing a new, sophisticated naval ship Republic of Germany and Italy and awarded system requires a considerable investment a letter contract to The Boeing Company of time, talent and money. -
Assistance in Determining BACT for Simple-Cycle Natural Gas Turbine
/date stamped July 5, 2000/ AR-18J Donald E. Sutton, P.E., Manager Permit Section, Division of Air Pollution Control Illinois Environmental Protection Agency P.O. Box 19506 Springfield, IL 62794-9506 Dear Mr. Sutton: Thank you for your letter dated May 30, 2000, in which you requested USEPA’s assistance in determining Best Available Control Technology (BACT) under Prevention of Significant Deterioration (PSD) rules found at 40 CFR 52.21 for a simple-cycle natural gas turbine peaker project proposed by Standard Energy Ventures (SEV). Specifically, you asked for our perspective on the nature of aeroderivative turbines and whether they should be treated as a separate category of equipment from other turbines. SEV has proposed 25 parts per million (ppm) and water injection as BACT for control of emissions of nitrogen oxides (NOx). Instead of determining whether turbines derived from those used in the aerospace industry, known as aeroderivative turbines, warrant treatment under PSD as a separate category of equipment from other turbines, we chose alternatively to look at other aeroderivative turbines around the country and see what BACT determinations there were. Our investigation of BACT for units similar to those described in the application (Pratt & Whitney FT8 "Twin Pacs", two 25 megawatt (MW) natural gas-fired aeroderivative turbines driving one electric generator), showed that catalytic control of NOx emissions, to below the 25 ppm level proposed by SEV, is technically feasible. We found that several slightly larger, yet arguably similar aeroderivative units in other States utilize selective catalytic reduction (SCR) and/or water injection to control NOx emissions down to 15 ppm and even as low as 5 ppm permitted levels, with actual tested levels below these values. -
Capacity Expansion Study Gowanus and Narrows Generating Stations ______
Capacity Expansion Study Gowanus and Narrows Generating Stations __________________________________________________________________________ Capacity Expansion Study For The Gowanus and Narrows Generating Stations Prepared For Astoria Generating Company, L.P. 400 Madison Avenue New York, New York 10017 Prepared by Burns and Roe Enterprises, Inc. 800 Kinderkamack Road Oradell, NJ 07649 Burns and Roe Enterprises, Inc October 19, 2006 Capacity Expansion Study Gowanus and Narrows Generating Stations __________________________________________________________________________ TABLE OF CONTENTS 1.0 Introduction and Methodology 2.0 Conceptual Layouts 2.1 Narrows Conceptual Layouts 2.2 Gowanus Conceptual Layouts 3.0 Preferred Layout Options 3.1 Narrows Barge Option 3.2 Gowanus South Pier Options 4.0 Indicative Cost Estimates 4.1 Gowanus Land based Options 4.1.1 Basis and Assumptions 4.1.2 Order of Magnitude Installed Costs 4.1.3 Comparative Plant Installed Costs 4.1.4 Supplemental Pricing Information 4.2 Narrows Power Barge Option 5.0 Thermal Performance Estimates 6.0 Emissions Performance Estimates 7.0 Electrical Interconnection and System Impacts 8.0 Other Information and Data Appendix 1: Conceptual Layout Sketches Appendix 2: The Power Barge Corporation Budgetary Quote Appendix 3: Coflex “Technip” Flexible Pipe Information Burns and Roe Enterprises, Inc October 19, 2006 Capacity Expansion Study Gowanus and Narrows Generating Stations ___________________________________________________________________________ 1.0 Introduction and Methodology In accordance with Task Order No. 001 between Astoria Generating Company, L.P. (Astoria) and Burns and Roe Enterprises, Inc. (BREI) dated July 27, 2007, BREI has completed a Conceptual Capacity Expansion Study to assist Astoria in developing an overall capacity expansion strategy for the Gowanus and Narrows Generating Stations; and to identify any critical hurdles that must be overcome to facilitate adding capacity at these sites. -
Lm2500 High Pressure Turbine Blade Refurbishment
THE AMERICAN SOSETY OF MECHANICAL ENGINEERS 345 E. 47th St, Now York, N.Y. 10017 96-GT214 - ..0 The Society shall not be responsible for statements or opinions advanced In papers or discussion at meetings of the Society or of its Divisions or : Sections, or printed in its publications. Discussion Is printed only If the paper is published in an ASME Journal. Authorization to photocopy 0 material for internal or personal use under circumstance not falling within the fair use provisions of the Copyright Act is granted by ASME to libraries and other users registered with the Copyright Clearance Center (CCC) Transactional Reporting Service provided that the base fee of • $0.30 per page is paid directly to the CCC, 27 Congress Street, Salem MA 01970. Requests for special permission or bulk reproduction shoukf be ad- , dressed to the ASME Tedmical Pubrsleng Department Copyright C 1996 by ASME All Rights Reserved Printed In U.S.A.._ , LM2500 HIGH PRESSURE TURBINE BLADE REFURBISHMENT Downloaded from http://asmedigitalcollection.asme.org/GT/proceedings-pdf/GT1996/78736/V002T03A003/2406979/v002t03a003-96-gt-214.pdf by guest on 28 September 2021 1111111111I III VIII Matthew J. Driscoll Peter P. Descar Jr. Naval Surface Warfare Center Naval Surface Warfare Center Philadelphia, Pennsylvania Philadelphia, Pennsylvania Gerald B. Katz Walter E. Coward Naval Surface Warfare Center Naval Sea Systems Command Philadelphia, Pennsylvania Washington DC ABSTRACT were not segregated, their relevant historical data was lost when As a cost savings measure, aircraft engine users often have hot the blades were stored. Because these blades came from several section components reconditioned and re-installed during engine different ship classes, the lost information includes total operating rebuilds and overhauls. -
MEP Testimony
CH2M HILL 2485 Natomas Park Drive Suite 600 Sacramento, CA 95833 Tel 916-920-0300 Fax 916-920-8463 December 20, 2010 DOCKET 382914 09-AFC-3 Mr. Craig Hoffman Project Manager DATE DEC 20 2010 California Energy Commission RECD. DEC 20 2010 1516 Ninth Street Sacramento, CA 95814-5512 Subject: Mariposa Energy Project (09-AFC-03) Applicant’s Testimony Dear Mr. Hoffman: Attached please find 1 hard copy and 1 electronic copy on CD-ROM of the Mariposa Energy Project Applicant’s Testimony. If you have any questions about this matter, please contact me at (916) 286-0348. Sincerely, CH2M HILL Doug Urry AFC Project Manager Attachment cc: C. Curry, Mariposa Energy, LLC. B. Buchynsky, Mariposa Energy, LLC. Mariposa Energy Project (09-AFC-03) Applicant’s Testimony Submitted to California Energy Commission Submitted by Mariposa Energy, LLC With Assistance from 2485 Natomas Park Drive Suite 600 Sacramento, CA 95833 December 2010 Contents Section Page Project Description ........................................................................................................................ 1 Electrical Transmission ................................................................................................................. 9 Air Quality and Greenhouse Gas Emissions ........................................................................... 13 Biological Resources .................................................................................................................... 25 Cultural Resources ..................................................................................................................... -
Appendix B Supporting Material for BACT Review for Electrical Generation Technologies
Appendix B Supporting Material for BACT Review For Electrical Generation Technologies I. INTRODUCTION Discussed in detail below are recommended emission levels for electrical generation sources using small gas turbines (rated at less than 50 MW in size), reciprocating engines using fossil fuel, and gas turbines / reciprocating engines using waste gas. The discussion below is based upon the requirements for determining Best Available Control Technology (BACT) in California and that BACT in California is equivalent to federal requirements for lowest achievable emission rate (LAER). BACT is generally specified as the most stringent emission level of these three alternative minimum requirements: 1) the most stringent emission control contained in any approved State Implementation Plan (SIP); 2) the most effective control achieved in practice; and 3) the most efficient emission control technique found by the district to be both technologically feasible and cost effective. This appendix provides the basis for the information presented in Chapter V (BACT for Electrical Generation Technologies). This appendix addresses BACT determinations for oxides of nitrogen (NOx), volatile organic compounds (VOC), carbon monoxide (CO), and particulate matter (PM). For the most effective control achieved in practice, examples were provided of emission levels specified in preconstruction permits issued by California districts and other states, and the most stringent emission levels achieved in practice. For each example cited, the following information is included: the name of the facility the equipment is located at, the applicable California district or State making the determination, a description of the basic equipment, and the method of control used to reduce emissions. In addition, for the control techniques required, the status of the permit (authority to construct/permit to construct or permit to operate) and the emission levels established by the permitting agency are provided. -
Our New Edition of Our Annual Newsletter, Your Information Source to the Canadian Gas Turbine Industry. the IAGT
Welcome to our new edition of our annual newsletter, your information source to the Canadian gas turbine industry. The IAGT Gas Turbine Newsletter summarizes some previous Committee activities, and addresses today’s developments to inform you about upcoming events and new developments of interest to all of us connected to the industry. The newsletter is available on the IAGT website at iagtcommittee.com. Contributions, feedback and suggestions to the Symposium and to the Newsletter are welcome and can be sent via e-mail to the addresses on the back page. The Industrial Application of Gas Turbines (IAGT) Committee, formed in 1973 under the sponsorship of the National Research Council of Canada, is a Technical Advisory Group to Canadian industry and government. The group provides a forum for the exchange and dissemination of ideas and the communication of new developments related to the industrial application of gas turbines in Canada. Presently under the sponsorship of the Canadian Gas Association and the National Research Council, the IAGT Committee's specific functions relate to the organization of a biennial technical symposium and a fall Forum held on alternate years from the Symposium. The Symposium provides the venue for the presentation of technical papers and discussion panels covering all aspects of industrial gas turbine operation as well as providing a forum for reviewing directives, guidelines, codes and practices, as issued by Regulatory Agencies, which impact directly on the application of gas turbines. The IAGT Committee members are listed on the website and we thank those members who volunteer their time and effort to the Canadian Gas Turbine Industry. -
Aero Engine Intercooling Conceptual Design and Experimental Validation of an Aero Engine Intercooler
Aero Engine Intercooling Conceptual design and experimental validation of an aero engine intercooler XIN ZHAO Department of Applied Mechanics CHALMERS UNIVERSITY OF TECHNOLOGY Gothenburg, Sweden 2016 THESIS FOR THE DEGREE OF DOCTOR OF PHILOSOPHY IN THERMO AND FLUID DYNAMICS Aero Engine Intercooling Conceptual design and experimental validation of an aero engine intercooler XIN ZHAO Department of Applied Mechanics CHALMERS UNIVERSITY OF TECHNOLOGY Gothenburg, Sweden 2016 Aero Engine Intercooling Conceptual design and experimental validation of an aero engine intercooler XIN ZHAO ISBN 978-91-7597-380-7 c XIN ZHAO, 2016 Doktorsavhandlingar vid Chalmers tekniska h¨ogskola Ny serie nr. 4061 ISSN 0346-718X Department of Applied Mechanics Chalmers University of Technology SE-412 96 Gothenburg Sweden Telephone: +46 (0)31-772 1000 Chalmers Reproservice Gothenburg, Sweden 2016 Aero Engine Intercooling Conceptual design and experimental validation of an aero engine intercooler Thesis for the degree of Doctor of Philosophy in Thermo and Fluid Dynamics XIN ZHAO Department of Applied Mechanics Chalmers University of Technology Abstract Intercooling has the potential to provide a shortcut to the next generation aero engines with higher bypass ratio (BPR), higher overall pressure ratio (OPR) and higher turbine inlet temperature (TIT) by lowering the high pressure compressor (HPC) delivery temperature. To be able to establish a systematic understanding of aero engine intercooling, the heat transfer and pressure loss characteristics of a given intercooler architecture need to be known in the parameter range anticipated for the engine optimization. A two-pass cross flow tubular heat exchanger for aero engine intercooling applications was hence developed by the means of computational fluid dynamics (CFD). -
LHD 8: a Step Toward the All Electric Warship
Thomas Dalton, Abe Boughner, C. David Mako and Cdr. Norbert Doerry, USN LHD 8: A Step Toward the All Electric Warship ABSTRACT (Figure 1) are designed to support Marine Corps air and amphibious assaults against The recently commissioned Iwo Jima defended positions ashore. The propulsion (LHD 7) is the last ship with plant for the first seven ships of the Wasp conventional steam propulsion that class consists of two independent steam the U.S. Navy plans to build. The boilers and two 35,000 hp steam turbine LHD 8 is the next ship of the class engines capable of driving the ship at over and will be built as a modified repeat 20 knots. This basic steam propulsion design of the LHD 7. The key approach was adopted from the earlier, circa modifications are steam propulsion 1960’s, steam propulsion plant of the being replaced with a hybrid Tarawa (LHA 1) class. In the early 1990s propulsion system of main gas turbine the U.S. Navy made a general decision to engines augmented with auxiliary phase out conventionally powered steam propulsion motors and electric ships due to the high cost of maintenance powered auxiliaries replacing those and manning. During construction of the powered by steam. The LHD 8 will LHD 5, 6 & 7, the Navy conducted a global also be the first USN surface ship to search to replace the steam plant with implement a 4160 VAC Zonal alternative power systems. At that time a Electrical Distribution System (AC General Electric LM2500 gas turbine engine ZEDS) as well as the integrated (25,000 hp) was the only gas turbine engine power system concept for electrical qualified for propulsion of U.S.