Thesis Template (Single-Sided)

Total Page:16

File Type:pdf, Size:1020Kb

Thesis Template (Single-Sided) CRANFIELD UNIVERSITY MARIA ROYO BONO INTEGRATION OF GAS TURBINE PERFORMANCE MODEL WITH DIESEL ENGINE PERFORMANCE MODEL FOR MARINE APPLICATION SCHOOL OF AEROSPACE TRANSPORT AND MANUFACTURING Thermal Power MSc Academic Year: 2016 - 2017 Supervisor: Suresh Sampath August 2017 CRANFIELD UNIVERSITY SCHOOL OF AEROSPACE TRANSPORT AND MANUFACTURING Thermal Power MSc Academic Year 2016 - 2017 MARIA ROYO BONO INTEGRATION OF GAS TURBINE PERFORMANCE MODEL WITH DIESEL ENGINE PERFORMANCE MODEL FOR MARINE APPLICATION Supervisor: Suresh Sampath August 2017 This thesis is submitted in partial fulfilment of the requirements for the degree of Thermal Power (NB. This section can be removed if the award of the degree is based solely on examination of the thesis) © Cranfield University 2017. All rights reserved. No part of this publication may be reproduced without the written permission of the copyright owner. ABSTRACT The design of a marine propulsion system for naval application is challenging, since the high-performance requirements to accomplish a certain mission, usually do not agree with an efficient operation. For this reason, the development of alternative propulsion systems, such as the combination of different prime movers emerged. One of the most efficient arrangement is the CODAG configuration, which combines the use of diesel engines and gas turbines. In this way, the operating profile of a particular vessel can be optimised for high performance and low consumption. This project involves the development of a CODAG propulsion system model in order to optimise the operating profile of a specific vessel. The required power for a particular scenario has been obtained using a Matlab code. It integrates the performance of two high speed diesel engines and an aero-derivative gas turbine based on the GE-LM2500. A matching methodology has been generated to couple the prime movers and the vessels propulsive device. In addition, Turbomatch simulations have been executed to understand the influence of ambient temperature on the gas turbine performance and therefore, on the performance of the CODAG propulsion system. In the same way, the degradation of the gas turbine has been analysed. As a result, it has been built a tool that integrates the above-mentioned features capable of assessing the vessel’s fuel consumption for a given operating profile. The developed tool exhibits a great potential to optimise the performance of vessels with a CODAG propulsion system. Depending on the vessel requirements, the optimization could be among a wide range of possibilities. Also, different CODAG configurations, such as adding another gas turbine, or removing one diesel engines can be analysed. Keywords: CODAG, Diesel engine, Gas turbine, Fuel consumption, Integration, Engines- propeller matching i ACKNOWLEDGEMENTS My family for the psychological support throughout this intense year. Their encouragement gave me the strength to overcome all the difficulties that I have faced during my entire life. My family in Cranfield for all the shared moments, this year would not have been the same without having known all of you. My supervisor, Doctor Suresh Sampath, and his colleague, Amit Batra, for giving me the opportunity and help to develop my research project. ii TABLE OF CONTENTS ABSTRACT ......................................................................................................... i ACKNOWLEDGEMENTS.................................................................................... ii LIST OF FIGURES ............................................................................................. v LIST OF TABLES ............................................................................................. viii LIST OF EQUATIONS ........................................................................................ ix NOMENCLATURE ............................................................................................. xi 1 INTRODUCTION ............................................................................................. 1 1.1 Aim and objectives .................................................................................... 2 1.2 Thesis structure ........................................................................................ 2 2 LITERATURE REVIEW ................................................................................... 4 2.1 Marine propulsion plants evolution through history ................................... 4 2.2 Marine propulsion system selection .......................................................... 6 2.2.1 Marine propulsion system main components ..................................... 6 2.2.2 Marine propulsion system classification depending on the prime mover type .................................................................................................. 8 2.2.3 Factors that influence on the propulsion plant selection ..................... 9 2.3 Combined power plants .......................................................................... 10 2.3.1 COSAG: Combined steam turbine and gas turbine .......................... 11 2.3.2 COGAS: Combined gas turbine and steam turbine .......................... 12 2.3.3 CODAD: Combined diesel engine and diesel engine ....................... 13 2.3.4 CODOG: Combined diesel engine or gas turbine ............................ 13 2.3.5 CODAG: Combined diesel engine and gas turbine .......................... 14 2.3.6 COGOG: Combined gas turbine or gas turbine ................................ 16 2.3.7 CODLAG: Combined electric-diesel engine and gas turbine ............ 16 2.3.8 Combined propulsion plant comparison ........................................... 17 2.4 CODAG propulsion system prime movers .............................................. 20 2.4.1 Diesel engine ................................................................................... 20 2.4.2 Gas turbine ....................................................................................... 21 2.4.3 Prime movers comparison: diesel engine and gas turbine ............... 24 2.5 Marine gas turbine degradation .............................................................. 26 2.5.1 Recoverable and non-recoverable degradation ............................... 27 2.5.2 Degradation mechanisms ................................................................. 27 3 METHODOLOGY .......................................................................................... 30 3.1 CODAG propulsion plant configuration ................................................... 30 3.1.1 Diesel engine ................................................................................... 30 3.1.2 Gas turbine ....................................................................................... 31 3.2 Marine vessel power prediction model .................................................... 32 3.2.1 Marine vessel selection .................................................................... 34 3.2.2 Hull resistance module ..................................................................... 35 3.2.3 Wake, thrust deduction and relative rotative efficiency..................... 40 iii 3.2.4 Screw propeller module .................................................................... 42 3.2.5 Shaft losses ...................................................................................... 46 3.2.6 Gearbox losses ................................................................................ 46 3.3 Turbomatch gas turbine model ............................................................... 48 4 ENGINES-PROPELLER MATCHING ........................................................... 51 4.1 Diesel engine-propeller matching ........................................................... 52 4.2 Gas turbine-propeller matching ............................................................... 54 5 OVERALL MARINE POWER PLANT PERFORMANCE ............................... 59 5.1 Theoretical background .......................................................................... 60 5.2 Ambient temperature effect ..................................................................... 63 5.2.1 Ambient temperature effect on the marine propulsion plant ............. 70 5.3 Gas engine degradation effect ................................................................ 73 5.3.1 Components degradation ................................................................. 74 5.3.2 Overall degradation effect ................................................................ 80 5.3.3 Degradation effect on the marine propulsion plant ........................... 84 5.4 Ambient temperature and engine degradation combined effect on the marine propulsion plant................................................................................. 87 5.5 Simulation of a vessel’s operating profile ................................................ 91 6 CONCLUSIONS AND RECOMENDATIONS ................................................ 92 6.1 Recommendations .................................................................................. 95 REFERENCES ................................................................................................. 96 APPENDICES .................................................................................................. 99 iv LIST OF FIGURES Figure 2-1. Chronological line of marine propulsion systems evolution .............. 6 Figure 2-2. COSAG components distribution ................................................... 12 Figure 2-3. COGAS components distribution
Recommended publications
  • 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.
    [Show full text]
  • Security & Defence European
    a 7.90 D European & Security ES & Defence 4/2016 International Security and Defence Journal Protected Logistic Vehicles ISSN 1617-7983 • www.euro-sd.com • Naval Propulsion South Africa‘s Defence Exports Navies and shipbuilders are shifting to hybrid The South African defence industry has a remarkable breadth of capa- and integrated electric concepts. bilities and an even more remarkable depth in certain technologies. August 2016 Jamie Shea: NATO‘s Warsaw Summit Politics · Armed Forces · Procurement · Technology The backbone of every strong troop. Mercedes-Benz Defence Vehicles. When your mission is clear. When there’s no road for miles around. And when you need to give all you’ve got, your equipment needs to be the best. At times like these, we’re right by your side. Mercedes-Benz Defence Vehicles: armoured, highly capable off-road and logistics vehicles with payloads ranging from 0.5 to 110 t. Mobilising safety and efficiency: www.mercedes-benz.com/defence-vehicles Editorial EU Put to the Test What had long been regarded as inconceiv- The second main argument of the Brexit able became a reality on the morning of 23 campaigners was less about a “democratic June 2016. The British voted to leave the sense of citizenship” than of material self- European Union. The majority that voted for interest. Despite all the exception rulings "Brexit", at just over 52 percent, was slim, granted, the United Kingdom is among and a great deal smaller than the 67 percent the net contribution payers in the EU. This who voted to stay in the then EEC in 1975, money, it was suggested, could be put to but ignoring the majority vote is impossible.
    [Show full text]
  • 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.
    [Show full text]
  • 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.
    [Show full text]
  • 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.
    [Show full text]
  • 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.
    [Show full text]
  • The Market for Gas Turbine Marine Engines
    The Market for Gas Turbine Marine Engines Product Code #F649 A Special Focused Market Segment Analysis by: Industrial & Marine Turbine Forecast - Gas & Steam Turbines Analysis 4 The Market for Gas Turbine Marine Engines 2010-2019 Table of Contents Executive Summary .................................................................................................................................................2 Introduction................................................................................................................................................................3 Methodology ..............................................................................................................................................................5 Trends and the Competitive Environment .........................................................................................................6 Manufacturers Review.............................................................................................................................................8 Russian Marine Gas Turbines .............................................................................................................................16 Market Statistics .....................................................................................................................................................17 Table 1 - The Market for Gas Turbine Marine Engines Unit Production by Headquarters/Company/Program 2010 - 2019 ................................................18 Table
    [Show full text]
  • 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.
    [Show full text]
  • UNIT-1 COAL BASED THERMAL POWER PLANTS PART-A 1. What Are the Types of Power Plants?
    ME6701 POWER PLANT ENGINEERING/ EEE DEPT/R SENTHI KUMAR VEL TECH HIGH TECH DR. RANGARAJAN DR.SAKUNTHALA ENGINEERING COLLEGE UNIT-1 COAL BASED THERMAL POWER PLANTS PART-A 1. What are the types of power plants? 1. Thermal Power Plant 2. Diesel Power Plant 3. Nuclear Power Plant 4. Hydel Power Plant 5. Steam Power Plant 6. Gas Power Plant 7. Wind Power Plant 8. Geo Thermal 9. Bio – Gas 10. M.H.D. Power Plant 2. What are the flow circuits of a thermal Power Plant? 1. Coal and ash circuits. 2. Air and Gas 3. Feed water and steam 4. Cooling and water circuits 3. List the different types of components (or) systems used in steam (or) thermal power plant? 1. Coal handling system. 2. Ash handling system. 3. Boiler 4. Prime mover 5. Draught system. a. Induced Draught b. Forced Draught 4.What are the merits of thermal power plants? 1.The unit capacity of thermal power plant is more. 2.The cost of unit decreases with the increase in unit capacity 3. Life of the plant is more (25-30 years) as compared to diesel plant (2-5 years) 4. Repair and maintenance cost is low when compared with diesel plant 5. Initial cost of the plant is less than nuclear plants 6. Suitable for varying load conditions. 5. What are the Demerits of thermal power plants? Demerits of thermal Power Plants: 1. Thermal plant are less efficient than diesel plants 2. Starting up the plant and brining into service takes more time 3. Cooling water required is more 4.
    [Show full text]
  • 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.
    [Show full text]
  • การพัฒนาของเรือรบรุ่นใหม่ และเทคโนโลยีระบบบูรณาการ the Evolution of Warships and Integrated Systems Technology ตอนจบ นาวาเอก คำรณ พิสณฑ์ยุทธการ
    บทความ การพัฒนาของเรือรบรุ่นใหม่ และเทคโนโลยีระบบบูรณาการ The Evolution of Warships and Integrated Systems Technology ตอนจบ นาวาเอก คำรณ พิสณฑ์ยุทธการ ารบูรณาการระบบต่าง ๆ ในเรือรบ ในขอบเขตจำกัดหรือสามารถฟื้นตัวกลับมารบได้ (Warship Integrated Systems) ในเวลาอันรวดเร็ว โดยพัฒนาทั้งในรูปแบบของการ กตามที่ได้กล่าวไปแล้วว่า การบูรณาการระบบต่าง ๆ พัฒนารูปร่างของเรือ (Shape) และภาพเงาร่าง บนเรือ มีจุดมุ่งหมายที่จะให้เกิดความมีประสิทธิภาพ (Signature) ของเรือ ระบบบูรณาการที่มีการนำมา ในการทำการรบทั้งในทางรุกและทางรับ โดยเน้น ใช้บนเรือแล้วในปัจจุบัน ประกอบไปด้วยระบบต่าง ๆ การพัฒนาระบบแบบบูรณาการไปที่หลักการ ๒ ดังนี้ ประการ คือ การพัฒนาระบบบูรณาการด้านขีด การบูรณาการระบบสะพานเดินเรือ (Integrated ความสามารถในการรบทางเรือสมัยใหม่ (Modern Bridge System : IBS) Warfighting Capabilities) และการพัฒนาระบบ การบูรณาการระบบอำนวยการรบ (Integrated บูรณาการด้านความอยู่รอดของเรือ (Survivability) Combat Management System : ICMS) ซึ่งแบ่งเป็น การป้องกันการยิงถูกเรือ (Hit Avoidance) การบูรณาการระบบบริหารจัดการระบบ ตามขั้นตอนการรบแต่ละขั้นตอน ความทนทานต่อ เรือต่าง ๆ (Integrated Platform Management ความเสียหายของเรือ (Damage Tolerance) ให้อยู่ System : IPMS) นาวิกศาสตร์ ปีที่ ๙๔ ฉบับที่ ๑๑ พฤศจิกายน ๒๕๕๔ ๐17 การบูรณาการระบบสื่อสาร (Integrated เป็นระบบแรกของเรือที่มีการพัฒนาให้เป็นระบบ Communication System : ICS) บูรณาการขึ้น โดยการนำแผนที่เดินเรือมาทำงาน การบูรณาการระบบเสากระโดงเรือ (Integrated ร่วมกับเรดาร์ ไยโรและเครื่องวัดความเร็วเรือ (Log) Mast System : IMS) สะพานเดินเรือของเรือรบรุ่นเก่า ๆ เครื่องมือเดินเรือ การบูรณาการระบบขับเคลื่อนของเรือ (Combined เรดาร์เดินเรือ
    [Show full text]
  • Division of Marine Engineering
    ΝATIONAL TECHNICAL UNIVERSITY OF ATHENS SCHOOL OF NAVAL ARCHITECTURE AND MARINE ENGINEERING DIVISION OF MARINE ENGINEERING DIPLOMA THESIS Techno-economic Evaluation of Various Energy Systems for LNG Carriers ANDRIANOS KONSTANTINOS ATHENS, JULY 2006 SUPERVISOR PROFESSOR: CH. FRANGOPOULOS Devoted to my family for their love, patience and support and especially to my beloved mother Aimilia S. Rakka- Andrianou who will live forever in our hearts. CONTENTS Foreword Acknowledgements 1. INTRODUCTION 1 2. LNG CARRIER PROPULSION PLANTS DESCRIPTION 3 2.1 Steam Turbine 3 2.1.1 General information-technological development 3 2.1.2 Conventional steam turbine propulsion plant 5 2.1.3 Advantages and drawbacks for a steam turbine propulsion plant installation 8 2.2 Gas Turbine 9 2.2.1 General information-technological development 9 2.2.1.1 Marine aero-derivative gas turbines manufacturers 10 2.2.1.2 Gas turbine myths and misunderstandings 12 2.2.1.3 Advantages of marine aero-derivative gas turbines 13 2.2.1.4 Disadvantages of marine aero-derivative gas turbines 15 2.2.1.5 Gas turbines for LNG carriers 16 2.2.2 Typical gas turbine propulsion plant 19 2.2.3 Advantages and drawbacks for a gas turbine propulsion plant installation 20 2.3 Combined Gas and Steam Turbine 21 2.3.1 General information-technological development 21 2.3.2 Typical combined gas and steam turbine propulsion plant 29 2.3.3 Advantages and drawbacks for a combined gas and steam turbine propulsion plant installation 31 2.4 Slow Speed Diesel Engine 33 2.4.1 General information-technological
    [Show full text]