توربین گاز
- شروع کننده موضوع amir-pars
- تاریخ شروع
عمده کاربرد توربین گاز در صنایع هوایی است که البته امروزه از ان برای تولید انرژی الکتریکی مورد استفاده شایانی قرار گرفته است بطوری که 90% از برق تولیدی کشور از این طریق حاصل میشود
توربین گاز شامل سه قسمت اصلی میباشد:
1 - کمپرسور
2 - محفظه احتراق
3 - توربین
که بصورت سیکل برایتون عمل میکند
البته شامل تجهیزات کمکی و سیستم های فرعی نیز میباشد که اگر مایل باشید در مورد هر کدام توضیح خواهم داد
توربین گاز شامل سه قسمت اصلی میباشد:
1 - کمپرسور
2 - محفظه احتراق
3 - توربین
که بصورت سیکل برایتون عمل میکند
البته شامل تجهیزات کمکی و سیستم های فرعی نیز میباشد که اگر مایل باشید در مورد هر کدام توضیح خواهم داد
http://www.www.iran-eng.ir/d:fig2aدوست گرامی با دو مرحله ای کردن توربین راندمان افزایش می یابد
SHABNAM60
عضو جدید
از این سیستم در دو قسمت توربین گاز استفاده میشود
1 - روی شفت کمپرسور محل قرار گرفتن inner casingا برای هدایت کامل هوای فشرده به سمت محفظه احتراق و جلوگیری از نشتی این هوای فشرده به بیرون . شیارهایی تعبیه شده که حکم ابندی بین این دو قطعه را دارد همچنین در ورودی پره های توربین روی شفت ان و در بعضی موارد بین پره های متحرک و پوسته . و پره های ثابت و روتور از این سیستم ابندی خشک بوسیله هوای فشرده یا گاز حاصل از احتراق استفاده می شود
2 - همانطور که میدانید یاتاقان ها نیاز به روغنکاری دارند لذا برای جلوگیری از فرار روغن بین یاتاقان ها و شفت در حال چرخش. از هوای فشرده ردیف 4 و 5 کمپرسور گرفته و ان را به سمت محفظه یاتاقان ها هدایت کرده که این فشار هوا در دو سوی یاتاقان مانع از ریزش روغن میشود
که این هم نوعی ابندی بوسیله هوای خشک هست
از این سیستم در دو قسمت توربین گاز استفاده میشود
1 - روی شفت کمپرسور محل قرار گرفتن inner casingا برای هدایت کامل هوای فشرده به سمت محفظه احتراق و جلوگیری از نشتی این هوای فشرده به بیرون . شیارهایی تعبیه شده که حکم ابندی بین این دو قطعه را دارد همچنین در ورودی پره های توربین روی شفت ان و در بعضی موارد بین پره های متحرک و پوسته . و پره های ثابت و روتور از این سیستم ابندی خشک بوسیله هوای فشرده یا گاز حاصل از احتراق استفاده می شود
2 - همانطور که میدانید یاتاقان ها نیاز به روغنکاری دارند لذا برای جلوگیری از فرار روغن بین یاتاقان ها و شفت در حال چرخش. از هوای فشرده ردیف 4 و 5 کمپرسور گرفته و ان را به سمت محفظه یاتاقان ها هدایت کرده که این فشار هوا در دو سوی یاتاقان مانع از ریزش روغن میشود
که این هم نوعی ابندی بوسیله هوای خشک هست
1 - روی شفت کمپرسور محل قرار گرفتن inner casingا برای هدایت کامل هوای فشرده به سمت محفظه احتراق و جلوگیری از نشتی این هوای فشرده به بیرون . شیارهایی تعبیه شده که حکم ابندی بین این دو قطعه را دارد همچنین در ورودی پره های توربین روی شفت ان و در بعضی موارد بین پره های متحرک و پوسته . و پره های ثابت و روتور از این سیستم ابندی خشک بوسیله هوای فشرده یا گاز حاصل از احتراق استفاده می شود
2 - همانطور که میدانید یاتاقان ها نیاز به روغنکاری دارند لذا برای جلوگیری از فرار روغن بین یاتاقان ها و شفت در حال چرخش. از هوای فشرده ردیف 4 و 5 کمپرسور گرفته و ان را به سمت محفظه یاتاقان ها هدایت کرده که این فشار هوا در دو سوی یاتاقان مانع از ریزش روغن میشود
که این هم نوعی ابندی بوسیله هوای خشک هست
Aerothermodynamics of Gas Turbine Rocket Propulsion, Third Edition (Aiaa Education Series)
By Gordon C. Oates
* Publisher: AIAA (American Institute of Aeronautics & Ast
* Number Of Pages: 456
* Publication Date: 1997-06
* ISBN / ASIN: 1563472414
Book Description Includes software This seminal book on gas turbine technology has been a best-seller since it was first
published in 1984. It now includes a comprehensive set of software programs that complement the text with problems and
design analyses. Software topics included are: atmosphere programs, quasi-one-dimensional flows programs (ideal constant-
area heat interaction, adiabatic constant-area flow with friction, rocket nozzle performance, normal shock waves, oblique
shock waves), gas turbine programs (engine cycle analysis and engine off-design performance), and rocket combustion
programs (Tc and Pc given, Hc and Pc given, isentropic expansion). Used as a standard text in more than 50 universities,
the book and software will continue to fulfill the need for a comprehensive modern book on the principles of propulsion.
System Requirements:IBM PC 386/486/586/Pentium or compatible; 640 Kb RAM hard disk with 1.0 Mb of available disk
space; EGA or better video capability
http://rapidshare.com/files/26738161/Aerothermodynamics_of_Gas_turbine_and_Rocket_propulsion.rar (4634 KB).
http://rapidshare.com/files/26729736/aerothermodynamics_of_gas_turbine_and_rocket_propulsion.rar (5156 KB).
http://gigapedia.org/redirect.id:9db13066d610caa81996eb3421a2c8db.url
~~~
Advanced Gas Turbine Cycles : A Brief Review of Power Generation Thermodynamics
ISBN: 0080442730
Author: J. Horlock
Publisher: Pergamon
Edition: (July 18, 2003)
Pages: 188 pages
Primarily this book describes the thermodynamics of gas turbine cycles. The search for high gas turbine efficiency has
produced many variations on the simple A´open circuitA´ plant, involving the use of heat exchangers, reheating and
intercooling, water and steam injection, cogeneration and combined cycle plants. These are described fully in the text. A
review of recent proposals for a number of novel gas turbine cycles is also included. In the past few years work has been
directed towards developing gas turbines which produce less carbon dioxide, or plants from which the CO2 can be
disposed of; the implications of a carbon tax on electricity pricing are considered. In presenting this wide survey of gas
turbine cycles for power generation the author calls on both his academic experience (at Cambridge and Liverpool
Universities, the Gas Turbine Laboratory at MIT and Penn State University) and his industrial work (primarily with Rolls
Royce, plc.) The book will be essential reading for final year and masters students in mechanical engineering, and for
practising engineers.
http://rapidshare.de/files/21089021/HORLOCK__J._H.__2003_._Advanced_Gas_Turbine_Cycles.rar
http://mihd.net/kyjcsn
PASS: www.blueportal.org
~~~
Gas Turbine Handbook: Principles and Practices
By Tony Giampaolo
* Publisher: Marcel Dekker
* Number Of Pages: 405
* Publication Date: 2002-12-12
* ISBN / ASIN: 08247099
Book Description:
The second edition of a bestseller, this comprehensive reference provides the fundamental information required to
understand both the operation and proper application of all types of gas turbines. The completely updated second edition
adds a new section on use of inlet cooling for power augmentation and NOx control. It explores the full spectrum of gas
turbines hardware, typical application scenarios, and operating parameters, controls, inlet treatments, inspection, trouble-
shooting, and more. The author discusses strategies that can help readers avoid problems before they occur and provides
tips that enable diagnosis of problems in their early stages and analysis of failures to prevent their recurrence
http://rapidshare.com/files/8842104/Gas_Turbine_Handbook.rar (9060 KB).
http://www.sendspace.com/file/zaxeqx
~~~
Elements of Propulsion: Gas Turbines And Rockets (AIAA Education) (Aiaa Education Series)
By Jack D. Mattingly
* Publisher: AIAA (American Institute of Aeronautics & Ast
* Number Of Pages: 867
* Publication Date: 2006-08-30
* ISBN / ASIN: 1563477793
This text provides a complete introduction to gas turbine and rocket propulsion for aerospace and mechanical engineers.
Building on the very successful Elements of Gas Turbine Propulsion, textbook coverage has been expanded to include
rocket propulsion and the material on gas dynamics has been dramatically improved. The text is divided into four parts:
basic concepts and gas dynamics; analysis of rocket propulsion systems; parametric (design point) and performance (off-
design) analysis of air breathing propulsion systems; and analysis and design of major gas turbine engine components (fans,
compressors, turbines, inlets, nozzles, main burners, and afterburners).
Design concepts are introduced early (aircraft and rocket performance in an introductory chapter) and integrated
throughout. Written with extensive student input on the design of the book, the book builds upon definitions and gradually
develops the thermodynamics, gas dynamics, rocket engine analysis, and gas turbine engine principles. The book contains
over 100 worked examples and numerous homework problems so concepts are applied after they are introduced. Over 600
illustrations and pictures show basic concepts, trends, and design examples. Eight computer programs accompany the text,
which allow for rapid calculation of trends, what if questions, conceptual design, homework problems, and homework
verification. The software runs in the Windows operating system on PC-compatible systems.
About the Author
Jack D. Mattingly received his B.S. and M.S. in Mechanical Engineering from the University of Notre Dame, and his Ph.D.
in Aeronautics and Astronautics at the University of Washington. While studying for his doctorate under Gordon C. Oates, he
pioneered research in the mixing of coannular swirling flows and developed a major new test facility. During his 40 years of
experience in analysis and design of propulsion and thermodynamic systems, he has written two engineering textbooks,
developed aerothermodynamic cycle analysis models, and created engineering software for air-breathing propulsion
systems. Dr. Mattingly was previously at the Aero Propulsion Laboratory at Wright-Patterson AFB where he directed
exploratory and advanced development programs aimed at improving the performance, reliability, and durability of gas
turbine engine components. He retired from active duty with the U.S. Air Force in 1989 and joined the faculty of Seattle
University. In 2000 he retired from Seattle University as Professor Emeritus in Mechanical Engineering to dedicate his
efforts to writing this textbook and a new edition of Aircraft Engine Design, teaching short courses, and consulting. Dr.
Mattingly has more than 35 years of experience in Engineering Education, earlier as a senior member of the Department of
Aeronautics at the United States Air Force Academy, where he established a top undergraduate propulsion program. In
addition, he has taught and done research in propulsion and thermal energy systems at the Air Force Institute of
Technology, University of Washington, University of Notre Dame, University of Wisconsin, and IBM Corp. He was also
founder of the AIAA/Air Breathing Propulsion Team Aircraft Engine Design Competition for undergraduate students. Among
his many distinguished teaching awards is Outstanding Educator for 1992 from Seattle University. Having published more
than 25 technical papers, articles, and textbooks in his field, Dr. Mattingly authored Elements of Gas Turbine Propulsion
(1995) and was co-author of Aircraft Engine Design, Second Edition (2002), an unprecedented conceptual design textbook
for air breathing engines that won the 2005 AIAA Summerfield Book Award
http://gigapedia.org/redirect.id:d30de969fdf0113499c0d16636a64039.url
http://gigapedia.org/redirect.id:d30de969fdf0113499c0d16636a64039.url
http://gigapedia.org/redirect.id:257843f77e37b30f3bba6bc1d6e401f1.url
~~~
Gas Turbine Engineering Handbooks
Publisher: Fairmont Press
Number Of Pages: 437
Publication Date: 2006-03-30
ISBN / ASIN: 0849390567
Book Description This comprehensive, best-selling reference provides the fundamental information needed to understand
the operation and proper application of all types of gas turbines. It explores the full spectrum of gas turbine hardware,
typical application scenarios, and operating parameters, controls, inlet treatments, inspection, and troubleshooting. This
latest edition includes a new chapter on microturbines and additional case studies. The author places special emphasis on
strategies that can help readers avoid problems before they occur, providing tips that will enable diagnosis of problems in
their early stages and analysis of failures to prevent their recurrence
http://rapidshare.com/files/1188583...rinciples_and_practices_ISBN10-0881735159.rar (10905 KB).
http://mihd.net/9hvtxp
~~~
Gas Turbine Engineering Handbook, Third Edition
Author: Meherwan P Boyce
Publisher: Gulf Professional Publishing; 2006
Publication Date: 2006-04-28
ISBN: 0750678461
Number Of Pages: 962
Clifford M. Simmang, Texas A&M University
The handbook should find its place in all the reference
libraries of those engineers and technicians
who have even a small responsibility for design
and operation of gas turbines.
This text refers to an out of print or unavailable edition of this title.
http://rapidshare.com/files/5975231/Gas_Turbine_Engineering_Handbook-3rd.rar (36659 KB).
OR
http://rapidshare.com/files/14396375/The_Gas_Turbine_Engineering_Handbook.rar (31970 KB).
rar pass = TQN0750678461
~~~
Elements of Gas Turbine Propulsion
ISBN: 1563477785
Title: Elements of Gas Turbine Propulsion (Aiaa Education Series)
Author: Jack D. Mattingly
Publisher: AIAA (American Institute of Aeronautics & Ast
Publication Date: 2005-08-01
Number Of Pages: 949
This text provides an introduction to gas turbine engines and jet propulsion for aerospace or mechanical engineers. The
text is divided into four parts: introduction to aircraft propulsion; basic concepts and one-dimensional/gas dynamics;
parametric (design point) and performance (off-design) analysis of air breathing propulsion systems; and analysis and design
of major gas turbine engine components (fans, compressors, turbines, inlets, nozzles, main burners, and afterburners
http://rapidshare.de/files/22503702/Mattingly__Jack_D._-_Elements_Of_Gas_Turbine_Propulsion.pdf
~~~
Gas Turbine Performance
ISBN: 063206434X
Title: Gas Turbine Performance
Author: Philip P. Walsh Paul Fletcher
Publisher: Blackwell Science
Publication Date: 2004-10-30
Number Of Pages: 646
http://rapidshare.com/files/9659281/gtp.rar (6757 KB).
http://mihd.net/2vhxj3
~~~Gas Turbine Engineering Handbook, Second Edition
Incompressible Flow Turbomachines
By Meherwan P Boyce
* Publisher: Gulf Professional Publishing
* Number Of Pages: 640
* Publication Date: 2001-12-21
* ISBN / ASIN: 0884157326
Book Description The gas turbine is a power plant that produces a great amount of energy for its size and weight and thus
has found increasing service in the past 20 years in the petrochemical industry and utilities throughout the world. The gas
turbine's compactness, weight, and multiple fuel applications make it a natural power plant for offshore platforms.
http://rapidshare.de/files/21061023...as_Turbine_Engineering_Handbook__2nd_ed._.rar
By Gordon C. Oates
* Publisher: AIAA (American Institute of Aeronautics & Ast
* Number Of Pages: 456
* Publication Date: 1997-06
* ISBN / ASIN: 1563472414
Book Description Includes software This seminal book on gas turbine technology has been a best-seller since it was first
published in 1984. It now includes a comprehensive set of software programs that complement the text with problems and
design analyses. Software topics included are: atmosphere programs, quasi-one-dimensional flows programs (ideal constant-
area heat interaction, adiabatic constant-area flow with friction, rocket nozzle performance, normal shock waves, oblique
shock waves), gas turbine programs (engine cycle analysis and engine off-design performance), and rocket combustion
programs (Tc and Pc given, Hc and Pc given, isentropic expansion). Used as a standard text in more than 50 universities,
the book and software will continue to fulfill the need for a comprehensive modern book on the principles of propulsion.
System Requirements:IBM PC 386/486/586/Pentium or compatible; 640 Kb RAM hard disk with 1.0 Mb of available disk
space; EGA or better video capability
http://rapidshare.com/files/26738161/Aerothermodynamics_of_Gas_turbine_and_Rocket_propulsion.rar (4634 KB).
http://rapidshare.com/files/26729736/aerothermodynamics_of_gas_turbine_and_rocket_propulsion.rar (5156 KB).
http://gigapedia.org/redirect.id:9db13066d610caa81996eb3421a2c8db.url
~~~
Advanced Gas Turbine Cycles : A Brief Review of Power Generation Thermodynamics
ISBN: 0080442730
Author: J. Horlock
Publisher: Pergamon
Edition: (July 18, 2003)
Pages: 188 pages
Primarily this book describes the thermodynamics of gas turbine cycles. The search for high gas turbine efficiency has
produced many variations on the simple A´open circuitA´ plant, involving the use of heat exchangers, reheating and
intercooling, water and steam injection, cogeneration and combined cycle plants. These are described fully in the text. A
review of recent proposals for a number of novel gas turbine cycles is also included. In the past few years work has been
directed towards developing gas turbines which produce less carbon dioxide, or plants from which the CO2 can be
disposed of; the implications of a carbon tax on electricity pricing are considered. In presenting this wide survey of gas
turbine cycles for power generation the author calls on both his academic experience (at Cambridge and Liverpool
Universities, the Gas Turbine Laboratory at MIT and Penn State University) and his industrial work (primarily with Rolls
Royce, plc.) The book will be essential reading for final year and masters students in mechanical engineering, and for
practising engineers.
http://rapidshare.de/files/21089021/HORLOCK__J._H.__2003_._Advanced_Gas_Turbine_Cycles.rar
http://mihd.net/kyjcsn
PASS: www.blueportal.org
~~~
Gas Turbine Handbook: Principles and Practices
By Tony Giampaolo
* Publisher: Marcel Dekker
* Number Of Pages: 405
* Publication Date: 2002-12-12
* ISBN / ASIN: 08247099
Book Description:
The second edition of a bestseller, this comprehensive reference provides the fundamental information required to
understand both the operation and proper application of all types of gas turbines. The completely updated second edition
adds a new section on use of inlet cooling for power augmentation and NOx control. It explores the full spectrum of gas
turbines hardware, typical application scenarios, and operating parameters, controls, inlet treatments, inspection, trouble-
shooting, and more. The author discusses strategies that can help readers avoid problems before they occur and provides
tips that enable diagnosis of problems in their early stages and analysis of failures to prevent their recurrence
http://rapidshare.com/files/8842104/Gas_Turbine_Handbook.rar (9060 KB).
http://www.sendspace.com/file/zaxeqx
~~~
Elements of Propulsion: Gas Turbines And Rockets (AIAA Education) (Aiaa Education Series)
By Jack D. Mattingly
* Publisher: AIAA (American Institute of Aeronautics & Ast
* Number Of Pages: 867
* Publication Date: 2006-08-30
* ISBN / ASIN: 1563477793
This text provides a complete introduction to gas turbine and rocket propulsion for aerospace and mechanical engineers.
Building on the very successful Elements of Gas Turbine Propulsion, textbook coverage has been expanded to include
rocket propulsion and the material on gas dynamics has been dramatically improved. The text is divided into four parts:
basic concepts and gas dynamics; analysis of rocket propulsion systems; parametric (design point) and performance (off-
design) analysis of air breathing propulsion systems; and analysis and design of major gas turbine engine components (fans,
compressors, turbines, inlets, nozzles, main burners, and afterburners).
Design concepts are introduced early (aircraft and rocket performance in an introductory chapter) and integrated
throughout. Written with extensive student input on the design of the book, the book builds upon definitions and gradually
develops the thermodynamics, gas dynamics, rocket engine analysis, and gas turbine engine principles. The book contains
over 100 worked examples and numerous homework problems so concepts are applied after they are introduced. Over 600
illustrations and pictures show basic concepts, trends, and design examples. Eight computer programs accompany the text,
which allow for rapid calculation of trends, what if questions, conceptual design, homework problems, and homework
verification. The software runs in the Windows operating system on PC-compatible systems.
About the Author
Jack D. Mattingly received his B.S. and M.S. in Mechanical Engineering from the University of Notre Dame, and his Ph.D.
in Aeronautics and Astronautics at the University of Washington. While studying for his doctorate under Gordon C. Oates, he
pioneered research in the mixing of coannular swirling flows and developed a major new test facility. During his 40 years of
experience in analysis and design of propulsion and thermodynamic systems, he has written two engineering textbooks,
developed aerothermodynamic cycle analysis models, and created engineering software for air-breathing propulsion
systems. Dr. Mattingly was previously at the Aero Propulsion Laboratory at Wright-Patterson AFB where he directed
exploratory and advanced development programs aimed at improving the performance, reliability, and durability of gas
turbine engine components. He retired from active duty with the U.S. Air Force in 1989 and joined the faculty of Seattle
University. In 2000 he retired from Seattle University as Professor Emeritus in Mechanical Engineering to dedicate his
efforts to writing this textbook and a new edition of Aircraft Engine Design, teaching short courses, and consulting. Dr.
Mattingly has more than 35 years of experience in Engineering Education, earlier as a senior member of the Department of
Aeronautics at the United States Air Force Academy, where he established a top undergraduate propulsion program. In
addition, he has taught and done research in propulsion and thermal energy systems at the Air Force Institute of
Technology, University of Washington, University of Notre Dame, University of Wisconsin, and IBM Corp. He was also
founder of the AIAA/Air Breathing Propulsion Team Aircraft Engine Design Competition for undergraduate students. Among
his many distinguished teaching awards is Outstanding Educator for 1992 from Seattle University. Having published more
than 25 technical papers, articles, and textbooks in his field, Dr. Mattingly authored Elements of Gas Turbine Propulsion
(1995) and was co-author of Aircraft Engine Design, Second Edition (2002), an unprecedented conceptual design textbook
for air breathing engines that won the 2005 AIAA Summerfield Book Award
http://gigapedia.org/redirect.id:d30de969fdf0113499c0d16636a64039.url
http://gigapedia.org/redirect.id:d30de969fdf0113499c0d16636a64039.url
http://gigapedia.org/redirect.id:257843f77e37b30f3bba6bc1d6e401f1.url
~~~
Gas Turbine Engineering Handbooks
Publisher: Fairmont Press
Number Of Pages: 437
Publication Date: 2006-03-30
ISBN / ASIN: 0849390567
Book Description This comprehensive, best-selling reference provides the fundamental information needed to understand
the operation and proper application of all types of gas turbines. It explores the full spectrum of gas turbine hardware,
typical application scenarios, and operating parameters, controls, inlet treatments, inspection, and troubleshooting. This
latest edition includes a new chapter on microturbines and additional case studies. The author places special emphasis on
strategies that can help readers avoid problems before they occur, providing tips that will enable diagnosis of problems in
their early stages and analysis of failures to prevent their recurrence
http://rapidshare.com/files/1188583...rinciples_and_practices_ISBN10-0881735159.rar (10905 KB).
http://mihd.net/9hvtxp
~~~
Gas Turbine Engineering Handbook, Third Edition
Author: Meherwan P Boyce
Publisher: Gulf Professional Publishing; 2006
Publication Date: 2006-04-28
ISBN: 0750678461
Number Of Pages: 962
Clifford M. Simmang, Texas A&M University
The handbook should find its place in all the reference
libraries of those engineers and technicians
who have even a small responsibility for design
and operation of gas turbines.
This text refers to an out of print or unavailable edition of this title.
http://rapidshare.com/files/5975231/Gas_Turbine_Engineering_Handbook-3rd.rar (36659 KB).
OR
http://rapidshare.com/files/14396375/The_Gas_Turbine_Engineering_Handbook.rar (31970 KB).
rar pass = TQN0750678461
~~~
Elements of Gas Turbine Propulsion
ISBN: 1563477785
Title: Elements of Gas Turbine Propulsion (Aiaa Education Series)
Author: Jack D. Mattingly
Publisher: AIAA (American Institute of Aeronautics & Ast
Publication Date: 2005-08-01
Number Of Pages: 949
This text provides an introduction to gas turbine engines and jet propulsion for aerospace or mechanical engineers. The
text is divided into four parts: introduction to aircraft propulsion; basic concepts and one-dimensional/gas dynamics;
parametric (design point) and performance (off-design) analysis of air breathing propulsion systems; and analysis and design
of major gas turbine engine components (fans, compressors, turbines, inlets, nozzles, main burners, and afterburners
http://rapidshare.de/files/22503702/Mattingly__Jack_D._-_Elements_Of_Gas_Turbine_Propulsion.pdf
~~~
Gas Turbine Performance
ISBN: 063206434X
Title: Gas Turbine Performance
Author: Philip P. Walsh Paul Fletcher
Publisher: Blackwell Science
Publication Date: 2004-10-30
Number Of Pages: 646
http://rapidshare.com/files/9659281/gtp.rar (6757 KB).
http://mihd.net/2vhxj3
~~~Gas Turbine Engineering Handbook, Second Edition
Incompressible Flow Turbomachines
By Meherwan P Boyce
* Publisher: Gulf Professional Publishing
* Number Of Pages: 640
* Publication Date: 2001-12-21
* ISBN / ASIN: 0884157326
Book Description The gas turbine is a power plant that produces a great amount of energy for its size and weight and thus
has found increasing service in the past 20 years in the petrochemical industry and utilities throughout the world. The gas
turbine's compactness, weight, and multiple fuel applications make it a natural power plant for offshore platforms.
http://rapidshare.de/files/21061023...as_Turbine_Engineering_Handbook__2nd_ed._.rar
dada_morteza
عضو جدید
سلام امیر جان
من یک کتاب راجع به توربین های گازی می خواستم بهم معرفی کنی که حدالمقدور فارسی باشه چون زبان من زیاد خوب نیست.
متشکرم
tsp.co
عضو جدید
تقریبا همه کتابهایی که برای توربوماشینها نوشته شدن در زمینه طراحی کمپرسورها نیز مطلب زیادی دارن ( البته کتابهای غیرفارسی) . تو همین تاپیک هندبوکهای خیلی خوبی رو در زمینه توربینهای گازی دوستان زحمت کشیدن و گذاشتن. در مورد توربوماشینها هم تو قسمت دانلود کتابهای مهندسی مکانیک می تونید کتابهای خوبی رو پیدا کنید. متاسفانه چون ما ایرانیها بیشتر مصرف کننده ایم تا تولید کننده به زیان فارسی چیز جالبی رو پیدا نمی کنید. اگه یه خورده هم درزمینه CFD اطلاع جمع آوری کنید بهتون خیلی کمک می کنه.
موفق باشید!
موفق باشید!
soheilmehrad
عضو جدید
سلام میخواستم بپرسم در مورد پیلهای سوختی پلیمری مطلب دارین؟
میشه جواب بدین
سلام خسته نباشین من نیاز به یک پروژه در رابطه با توربین گاز دارم میتونین کمکم کنین؟
اینم
آدرس mailam
shere_shere_shere@yahoo.com
لطفا کمکم کنید
لطفا کمکم کنید
اینم آدرس mailam
shere_shere_shere@yahoo.com
لطفا کمکم کنید
سلام خسته نباشین من نیاز به یک پروژه در رابطه با توربین گاز دارم میتونین کمکم کنین؟
اینم آدرس mailam
shere_shere_shere@yahoo.com
فرهنگ
مدیر بازنشسته
این کاری که تو شرکت موادکاران در بخش توليدش انجام میدن.
در بخش توليد، از روش ريختهگري دقيق استفاده ميشود. به اين صورت كه ابتدا از يك مدل مومي مطابق با پره مورد نظر، براي ساخت قالب سراميكي استفاده ميشود؛ طراحي و ساخت قالبهاي تزريق موم با استفاده از ماشينهايCNC انجام ميشود. سپس مدل مومي قطعات با استفاده از ماشين تزريق، توليد ميشود. در مرحلة بعد، با ايجاد پوشش سراميكي بر روي اين مدلها، قالب سراميكي براي ريختهگري به كورههاي پيشرفته القايي و تحت خلاء فرستاده ميشود. ذوب و ريختهگري آلياژهاي فعال، همچون فولادهاي مخصوص و سوپرآلياژها، با استفاده از تكنولوژي ذوب القايي در خلاء انجام ميشود. ذوب القايي در خلاء صورت ميگيرد و براي قطعات فولادي معمولي و آلياژهاي غيرآهني از شيوههاي ذوب القايي معمولي و روشهاي مرسوم ديگر استفاده ميشود. به طور كلي، قطعات توليدي در اين روش نسبت به روشهاي ديگر ريختهگري، از سطح صاف مطلوبتري برخوردار ميباشند. بعد از عمل ريختهگري در قالبهاي سراميكي، پره حاصل براي برشكاري، تميزكاري و تمام‌كاري، به كارگاههايي كه بدين منظور در شركت ساخته شده است، روانه ميشوند.
منبع:
http://naft.itan.ir/?ID=924
سایت شرکت:
www.Mavadkaran.com
در بخش توليد، از روش ريختهگري دقيق استفاده ميشود. به اين صورت كه ابتدا از يك مدل مومي مطابق با پره مورد نظر، براي ساخت قالب سراميكي استفاده ميشود؛ طراحي و ساخت قالبهاي تزريق موم با استفاده از ماشينهايCNC انجام ميشود. سپس مدل مومي قطعات با استفاده از ماشين تزريق، توليد ميشود. در مرحلة بعد، با ايجاد پوشش سراميكي بر روي اين مدلها، قالب سراميكي براي ريختهگري به كورههاي پيشرفته القايي و تحت خلاء فرستاده ميشود. ذوب و ريختهگري آلياژهاي فعال، همچون فولادهاي مخصوص و سوپرآلياژها، با استفاده از تكنولوژي ذوب القايي در خلاء انجام ميشود. ذوب القايي در خلاء صورت ميگيرد و براي قطعات فولادي معمولي و آلياژهاي غيرآهني از شيوههاي ذوب القايي معمولي و روشهاي مرسوم ديگر استفاده ميشود. به طور كلي، قطعات توليدي در اين روش نسبت به روشهاي ديگر ريختهگري، از سطح صاف مطلوبتري برخوردار ميباشند. بعد از عمل ريختهگري در قالبهاي سراميكي، پره حاصل براي برشكاري، تميزكاري و تمام‌كاري، به كارگاههايي كه بدين منظور در شركت ساخته شده است، روانه ميشوند.
منبع:
http://naft.itan.ir/?ID=924
سایت شرکت:
www.Mavadkaran.com
سلام. اگه در مورد چگونگی تحلیل و بررسی نیروهای وارد به پره ی توربین گاز مطلبی داری ممنون می شم کمکم کنی.
ضربه ای افزایش فشار در پره ی ثابت است
ولی در عکس العملی افزایش فشار در پره های متحرک است
توربين ژنراتور گ
عضو جدید
سلام در مورد توربين ژنراتورهاي گازي مطلب مي خواهم.
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