ADVANCED GAS TURBINE THEORY AND DESIGN FUNDAMENTALS
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Course Title:
ADVANCED GAS TURBINE THEORY AND DESIGN FUNDAMENTALS
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Course Code:
OTO6134
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Type of Course:
Optional
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Level of Course:
Third Cycle
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Year of Study:
2
6
Semester:
4
7
ECTS Credits Allocated:
6
8
Theoretical (hour/week):
3
9
Practice (hour/week) :
0
10
Laboratory (hour/week) :
0
11
Prerequisites:
None
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Recommended optional programme components:
None
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Language:
Turkish
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Mode of Delivery:
Face to face
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Course Coordinator:
Prof. Dr. RUKİYE ERTAN
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Course Lecturers:
Yok
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Contactinformation of the Course Coordinator:
Prof. Dr. Ali Sürmen surmen@uludag.edu.tr +90 (224) 294 1965 Mühendislik Fakültesi Otomotiv Mühendisliği Bölümü
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Website:
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Objective of the Course:
For the use of gas turbine engine/power plants in power generation
Teaching the analysis, working principles of aircraft/jet engines, and transferring the theory for thermodynamic designs.
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Contribution of the Course to Professional Development
Upon completion of this course, students are expected to have the following knowledge and skills:
1. Recognizing the construction and basic structure of gas turbines
2. Recognizing the basic concepts and equipment of gas turbines
3. To learn about energy generation and thermodynamic relations with gas turbines.
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Learning Outcomes:
1
Thermodynamic principles of gas turbines;
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Ideal gas cycles and the simple Brayton cycle;
3
The use of gas turbines in practical life, understanding of common problems and solutions, developing the working methodology.;
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Gas turbine cycles for aircraft (jet) engines;
5
Thermodynamics of high speed fluids;
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Course Content:
Week
Theoretical
Practical
1
Introduction to gas turbines and gas turbine engines
2
Introduction to gas turbine thermodynamics
3
Ideal gas cycles and the simple Brayton cycle
4
Brayton cycle with regenerator
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Brayton cycle with intercooling and intermediate heating
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Brayton cycle with intercooling - intermediate heating and regenerator
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Gas turbine cycle for aircraft (jet) engines
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Analysis of jet / aircraft engines
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Thermodynamics of high speed fluids
10
Ideal turbo jet cycle analysis
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Turbo-prop engines (ideal cycle calculation)
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Design parameters in turbines
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Components of steam and gas turbines (compressors, combustion chambers and boilers)
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Production technologies of turbine blades and gas turbines
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Textbooks, References and/or Other Materials:
1. Gas Turbine Theory 5th Edition 2. Elements of Gas Turbine Propulsion; Mattingly, McGraw Hill, 1996 3. Gas Türbinleri; Çetinkaya Y. ; Nobel Yayın Dağıtım, 1997 4. Buhar ve Gaz Türbinli Gemi Tesisleri; Eyice, S. ; Kocaeli Devlet Müh. Mim. Akademisi Geliştirme Vakfı, 1982
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Assesment
TERM LEARNING ACTIVITIES
NUMBER
PERCENT
Midterm Exam
0
0
Quiz
0
0
Homeworks, Performances
2
40
Final Exam
1
60
Total
3
100
Contribution of Term (Year) Learning Activities to Success Grade
40
Contribution of Final Exam to Success Grade
60
Total
100
Measurement and Evaluation Techniques Used in the Course
Midterm exam is given as the average of 4 or 5 homework grades, including at least one or two questions that require in-depth analysis on each topic. The final exam is given in the form of "homework" similar to the yearly assignments but more comprehensive. Course evaluation is done over a midterm and a final exam.
Information
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ECTS / WORK LOAD TABLE
Activites
NUMBER
TIME [Hour]
Total WorkLoad [Hour]
Theoretical
14
3
42
Practicals/Labs
0
0
0
Self Study and Preparation
10
6
60
Homeworks, Performances
2
30
60
Projects
0
0
0
Field Studies
0
0
0
Midtermexams
0
0
0
Others
0
0
0
Final Exams
1
18
18
Total WorkLoad
180
Total workload/ 30 hr
6
ECTS Credit of the Course
6
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CONTRIBUTION OF LEARNING OUTCOMES TO PROGRAMME QUALIFICATIONS
