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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. -
Gallery of USAF Weapons Note: Inventory Numbers Are Total Active Inventory Figures As of Sept
Gallery of USAF Weapons Note: Inventory numbers are total active inventory figures as of Sept. 30, 2011. ■ 2012 USAF Almanac Bombers B-1 Lancer Brief: A long-range, air refuelable multirole bomber capable of flying intercontinental missions and penetrating enemy defenses with the largest payload of guided and unguided weapons in the Air Force inventory. Function: Long-range conventional bomber. Operator: ACC, AFMC. First Flight: Dec. 23, 1974 (B-1A); Oct. 18, 1984 (B-1B). Delivered: June 1985-May 1988. IOC: Oct. 1, 1986, Dyess AFB, Tex. (B-1B). Production: 104. Inventory: 66. Aircraft Location: Dyess AFB, Tex.; Edwards AFB, Calif.; Eglin AFB, Fla.; Ellsworth AFB, S.D. Contractor: Boeing, AIL Systems, General Electric. Power Plant: four General Electric F101-GE-102 turbofans, each 30,780 lb thrust. Accommodation: pilot, copilot, and two WSOs (offensive and defensive), on zero/zero ACES II ejection seats. Dimensions: span 137 ft (spread forward) to 79 ft (swept aft), length 146 ft, height 34 ft. B-1B Lancer (SSgt. Brian Ferguson) Weight: max T-O 477,000 lb. Ceiling: more than 30,000 ft. carriage, improved onboard computers, improved B-2 Spirit Performance: speed 900+ mph at S-L, range communications. Sniper targeting pod added in Brief: Stealthy, long-range multirole bomber that intercontinental. mid-2008. Receiving Fully Integrated Data Link can deliver nuclear and conventional munitions Armament: three internal weapons bays capable of (FIDL) upgrade to include Link 16 and Joint Range anywhere on the globe. accommodating a wide range of weapons incl up to Extension data link, enabling permanent LOS and Function: Long-range heavy bomber. -
The Aircraft Propulsion the Aircraft Propulsion
THE AIRCRAFT PROPULSION Aircraft propulsion Contact: Ing. Miroslav Šplíchal, Ph.D. [email protected] Office: A1/0427 Aircraft propulsion Organization of the course Topics of the lectures: 1. History of AE, basic of thermodynamic of heat engines, 2-stroke and 4-stroke cycle 2. Basic parameters of piston engines, types of piston engines 3. Design of piston engines, crank mechanism, 4. Design of piston engines - auxiliary systems of piston engines, 5. Performance characteristics increase performance, propeller. 6. Turbine engines, introduction, input system, centrifugal compressor. 7. Turbine engines - axial compressor, combustion chamber. 8. Turbine engines – turbine, nozzles. 9. Turbine engines - increasing performance, construction of gas turbine engines, 10. Turbine engines - auxiliary systems, fuel-control system. 11. Turboprop engines, gearboxes, performance. 12. Maintenance of turbine engines 13. Ramjet engines and Rocket engines Aircraft propulsion Organization of the course Topics of the seminars: 1. Basic parameters of piston engine + presentation (1-7)- 3.10.2017 2. Parameters of centrifugal flow compressor + presentation(8-14) - 17.10.2017 3. Loading of turbine blade + presentation (15-21)- 31.10.2017 4. Jet engine cycle + presentation (22-28) - 14.11.2017 5. Presentation alternative date Seminar work: Aircraft engines presentation A short PowerPoint presentation, aprox. 10 minutes long. Content of presentation: - a brief history of the engine - the main innovation introduced by engine - engine drawing / cross-section - -
The Power for Flight: NASA's Contributions To
The Power Power The forFlight NASA’s Contributions to Aircraft Propulsion for for Flight Jeremy R. Kinney ThePower for NASA’s Contributions to Aircraft Propulsion Flight Jeremy R. Kinney Library of Congress Cataloging-in-Publication Data Names: Kinney, Jeremy R., author. Title: The power for flight : NASA’s contributions to aircraft propulsion / Jeremy R. Kinney. Description: Washington, DC : National Aeronautics and Space Administration, [2017] | Includes bibliographical references and index. Identifiers: LCCN 2017027182 (print) | LCCN 2017028761 (ebook) | ISBN 9781626830387 (Epub) | ISBN 9781626830370 (hardcover) ) | ISBN 9781626830394 (softcover) Subjects: LCSH: United States. National Aeronautics and Space Administration– Research–History. | Airplanes–Jet propulsion–Research–United States– History. | Airplanes–Motors–Research–United States–History. Classification: LCC TL521.312 (ebook) | LCC TL521.312 .K47 2017 (print) | DDC 629.134/35072073–dc23 LC record available at https://lccn.loc.gov/2017027182 Copyright © 2017 by the National Aeronautics and Space Administration. The opinions expressed in this volume are those of the authors and do not necessarily reflect the official positions of the United States Government or of the National Aeronautics and Space Administration. This publication is available as a free download at http://www.nasa.gov/ebooks National Aeronautics and Space Administration Washington, DC Table of Contents Dedication v Acknowledgments vi Foreword vii Chapter 1: The NACA and Aircraft Propulsion, 1915–1958.................................1 Chapter 2: NASA Gets to Work, 1958–1975 ..................................................... 49 Chapter 3: The Shift Toward Commercial Aviation, 1966–1975 ...................... 73 Chapter 4: The Quest for Propulsive Efficiency, 1976–1989 ......................... 103 Chapter 5: Propulsion Control Enters the Computer Era, 1976–1998 ........... 139 Chapter 6: Transiting to a New Century, 1990–2008 .................................... -
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. -
Broad Specificationfuels on High B ,Passturbofan Engine Combustors
A/',d_*,,e'/_-/_2 _ Y/ 3 1176 00156 6455 NASA-CR-159641 19790025034 NASA CR-159641 R79AEG504 I,:. Analytical Evaluation of the Impact of " Broad SpecificationFuels on High B_,passTurbofan Engine Combustors FINAL REPORT August 1979 By J. R. Taylor General Electric Company Aircraft Engine Group Cincinnati., OH 45215 Ll_[1_.i[_!_,ll"_l'ti'lit_P7'll_i, ;:t! ,<::iY.ig LANGLEY RE.SEARCH CENTER LIBRARy,NASA HAMPTON,.VIRGINIA . " NATIONAL AERONAUTICS AND SPACEADMINISTRATION LEWISPrepRarEedSEARCHfor: CENTER -: ...... 21000 BROOKPARKROAD CLEVELAND, OHIO 44135 NAS3-20799 1. Report No. I 2. GovernmentA_:cessionNo. 3. Recipient'sCatalogNo. NASA CR-159641 I 4. Title and Subtitle 5. Report Date Analytical Evaluation of the Impact of Broad Specification Fuels August 1979 on High Bypass Turbofan Engine Combustors 6. PerformingOrganizationCode 7. Author{'s) 8. PerformingOrganizationReport No. J.R. Taylor R79AEG504 10. Work Unit No. 9. PerformingOrganizationName andAddress General Electric Company 11. Contractor Grant No. - Aircraft Engine Group Cincinnati, Ohlo 45215 NAS3-20799 13. Type of Report and PeriodCovered 12. SponsoringAgencyName and Address Contractor Report National Aeronautics and Space Administration 14. SponsoringAgency Code Washington, D.C. 20546 15. SupplementaryNotes Project Manager: A.L. Smith, NASA-Lewis Research Center, Cleveland, Ohlo 44135 16.Abstra_ An in-depth analysis of six conceptual combustor designs for the CF6-50 hlgh bypass turbofan engine and slx conceptual combustor designs for the NASA/GE E3 high bypass turbofan engine was performed to provide an assessment of the major problems anticipated in using broad specification fuels in these aircraft engine combustion systems. The conceptual eombustor designs are representative of both state-of-the-art and advanced state-of-the-art combustion systems. -
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. -
The Market for Aviation Turbofan Engines
The Market for Aviation Turbofan Engines Product Code #F640 A Special Focused Market Segment Analysis by: Aviation Gas Turbine Forecast Analysis 1 The Market for Aviation Turbofan Engines 2010-2019 Table of Contents Executive Summary .................................................................................................................................................2 Introduction................................................................................................................................................................2 Trends..........................................................................................................................................................................3 Market Focus .............................................................................................................................................................3 Competitive Environment.......................................................................................................................................4 Figure 1 - The Market for Aviation Turbofan Engines Unit Production 2010 - 2019 (Bar Graph) .................................................................................6 Figure 2 - The Market for Aviation Turbofan Engines Value of Production 2010 - 2019 (Bar Graph)...........................................................................6 Manufacturers Review.............................................................................................................................................7 -
Testing Down to the Last Detail
1/2010 Testing down to the last detail MTU Aero Engines Holding AG Customers + PartnersTechnology + Science MTU Global Dachauer Straße 665 80995 Munich • Germany Tel. +49 89 1489-0 Fax +49 89 1489-5500 Power for the Jumbo Jet Hardfaced tips for top MTU support for the [email protected] www.mtu.de and the Dreamliner efficiency “flying gas station” Contents Editorial Cover Story Dear Readers: Testing down to the last detail 4 – 7 Finally, yes finally, the bird is on the wing. However, the program highlights something Late last year, the new A400M military trans- else too—something we have witnessed re- Customers + Partners port aircraft successfully completed its long- peatedly in the past. Almost all the major Power for the Jumbo Jet and 8 – 11 awaited, eagerly anticipated maiden flight commercial and military aircraft programs the Dreamliner above the Spanish city of Seville. The relief that have ever been initiated in Europe and A boost for the MRJ 12 – 15 Testing down to the last detail was palpable throughout the industry; delays the United States have been subject to to the project had been creating too much delays, some of them massive. In this respect, Four TP400-D6 engines lift Europe’s new military transport, the A400M, up into turbulence all round. Now, the ongoing flight the A400M is no exception. As things stand the air—now almost an everyday occurrence at Seville airport. Since the maiden Technology + Science test program is demonstrating the superior at present, in pure economic terms, MTU flight in December 2009, flight testing has been in full swing. -
Shuttle/Progress in Aircraft Design Since 1903
197402:3386-002 -TABLE OF CONTENTS _. AIRCRAFT PAGE AIRCRAFT PAGE AeroncaC-2 28 Granville Bros.R-1 "Super Sportster" 33 BeechModel 18 42 GrummanF3F-2 36 Bell Model204 73 GrummanF4F-3 "Wildcat" 43 Bell P-59A "Airacomet" 57 GrummanF8F-1 "Bearcat" 60 • Bell XS-1 63 GrummanF-14A "Tomcat" 92 BldriotXI 5 HandleyPage0/400 7 BoeingModel40B 23 HawkerSiddeley"Harrier" 88 ; _. BoeingModel80A-1 27 Kellett YO-60 58 BoeingModel367-80 71 Lear Jet Model23 84 BoeingMode=377 "Stratocruiser" 64 Lockheed1049 "Super Constellation" 68 BoeingModel727 82 LockheedP-38F .ightning" 47 ; BoeingModel 737 89 LockheedP-80A "Shooting Star" 59 Bo_ingModel747 90 LockheedYF-12A 83 BoeingB-17F "Flying Fortress" 39 Lockheed"Vega" 25 BoeingB-29 "Superfortress" 56 Martin MB-2 18 BoeingB-47E 66 Martin PBM-3C "Mariner" 48 Bo_;ngB-52 "Stratofortress" 69 McDonnellF-4B "Phantom I1" 77 Boeing F4B-4 32 McDonnellDouglasF-15A"Eagle" 93 BoeingP-26A 31 MoraneSaulnierType N 6 CessnaModel421 87 Navy-CurtissNC-4 17 Cierva autogiro 20 Nieuport XVII C.1 9 ConsolidatedB-24D "Liberator" 49 NorthAmericanB.25H "Mitchell" 51 ConsolidatedPBY-5A'Catalina" 37 North AmericanF-86F "Sabre" 65 ConvairB-36D 62 North AmericanF-100D "Super Sabre" 70 Convair B-58A"Hustler" 74 North AmericanP-51B "Mustang" 52 , ConvairF-106A "Delta Dart" 75 NorthAmericanX-15 79 L Curtiss JN-4D"Jenny" 12 Piper J-3 "Cub" 44 CurtissP-6E "Hawk" 30 Piper "Cherokee140" 80 CurtissP-36A 38 Pitcairn PA-5"Mailwing" 24 : CurtissP-40B 46 Republic P-47D "Thunderbolt" 53 _ CurtissPW-8 19 RoyalAircraft FactoryR.E.8 8 De Havilland DH-4 13 RyanNYP "Spirit of St. -
Preliminary Design and Integration Studies
NASA CR-135444 R78AEG510 ENERGY EFFICIENT ENGINE Preliminary Design and Integration Studies FINAL REPORT by ADVANCED ENGINEERING AND TECHNOLOGY PROGRAMS DEPARTMENT GENERAL ^£ ELECTRIC «(NASA-CE-135'm) ENEFGY ?TFICIENT EKGIME: N70-31108 PS ELI «IN?. BY CES3G4 \Kl ЩЧЕСРАТТГЛ1 STUDIFS Pinal Report, Jar;. 1977 - Apr. 1978 (Gereral Electric Co.) 417 p ЧС Ы8/м? АС1 CSCI 21E 'Jncla G3/07 3C236 SEPTEMBER 1978 t<4j i Sri t r- -. -i-/^-« СУ») ^A ЗЛ OCiUT? Prepared For NATIONAL AERONAUTICS and SPACE ADMINISTRATION Lewis Research Center 21000 Brookpark Road Cleveland, Ohio 44135 NAS3-20627 1 Report No. 2. Government Accession No. 3. Recipient's Catalog No. NASA CR-135444 4. Title and Subtitle 5. Report Date Energy Efficient Engine - Preliminary Design and September, 1978 Integration Study - Final Report 6. Performing Organization Code 7. Author(s) 8. Performing Organization Report No. R.P. Johnston, R. Hirschkron, C.C. Koch, R.E. Neitzel, R78AEG510 P.W. Vinson 10. Work Unit No. 9. Performing Organization Name and Address 716-01-02 General Electric Company Aircraft Engine Group 11. Contract or Grant No. Cincinnati, Ohio 45215 NAS3-20627 13. Type of Report and Period Covered 12 Sponsoring Agency Name and Address Final; Jan. 1977-April 1978 National Aeronautics and Space Administration Lewis Research Center 14. Sponsoring Agency Code 21000 Brookpark Road, Cleveland, Ohio 44135 15 Supplementary Notes Project Manager: Neal T. Saunders, NASA-Lewis Research Center, Cleveland, Ohio 44135 Project Engineer: Gerald A. Kraft, NASA-Lewis Research Center, Cleveland, Ohio .44135 16 Abstract Parametric design and mission evaluations of advanced turbofan configurations were conducted for future transport aircraft application.