| １． |
Outline |
|
The functions and performances of such turbo-engines as turbojet engine, turbofan engine, etc. are studied based on the basic knowledge of thermodynamics, aerodynamics, etc..
Students will acquire the knowledge and techniques for the calculation related to DP1 and DP2.
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| ２． |
Objectives |
|
The target of this lecture is for students to acquire an ability to understand the principle of the function of the turbojet engine, turbofan engine, turbo-prop engine and the turbo-shaft engine applied to the aero-propulsion system.
Students will also be able to understand the characteristics of each type and the differences of functions between them.
|
| ３． |
Grading Policy |
|
Graded by evaluation of report submitted by students.
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| ４． |
Textbook and Reference |
|
No text is used.
Materials including figures, pictures and movies are indicated on slide.
These will be presented by LMS.
|
| ５． |
Requirements (Assignments) |
|
Preparation (about 1.5 hour);The materials used in the lesson will be presented beforehand through LMS, so please read them and do research by yourself which you do not understand and deepen your knowledge about gas turbine. Please also summarize what you do not understand in a notebook and ask questions by writing on a paper distributed every lesson.
Review (about 1.5 hour); The materials used in the lesson are presented by LMS, so please use them for review about function, performance, and formulas equation of gas turbine. And also answer of exercises will be presented by LMS, so please become able to perform the calculation.
|
| ６． |
Note |
|
The contents of the lesson may be changed according to the progress.
|
| ７． |
Schedule |
|
| １. Types and characteristics of the aero-engine |
| ２. Overview of the turbo-engines |
| ３. Power of the turbo-engine |
| ４. Efficiency of the turbo-engine |
| ５. Basic components of the turbo-engine-1:Basic structure |
| ６. Basic components of the turob-engine-2:Air-inlet, Fan and Compressor |
| ７. Basic components of the turbo-engine-3:Combustion chamber and Turbine |
| ８. Basic components of the turbo-engine-4:Exhaust system and Accessories |
| ９. Conservation of momentum |
| 10. Characteristics of multi-staged compressors |
| 11. Compressor stall (surging) |
| 12. Flutter of the turbine blades |
| 13. Accessories of the turbo-engine-1:Fuel supply subsystem and ignition subsystem |
| 14. Accessories of the turbo-engine-2:Contorl subsystem and Lubrication subsystem |
| 15. Materials used for the turbo-engine |
|
| １． |
Outline |
|
The functions and performances of such turbo-engines as turbojet engine, turbofan engine, etc. are studied based on the basic knowledge of thermodynamics, aerodynamics, etc..
Students will acquire the knowledge and techniques for the calculation related to DP1 and DP2.
|
| ２． |
Objectives |
|
The target of this lecture is for students to acquire an ability to understand the principle of the function of the turbojet engine, turbofan engine, turbo-prop engine and the turbo-shaft engine applied to the aero-propulsion system.
Students will also be able to understand the characteristics of each type and the differences of functions between them.
|
| ３． |
Grading Policy |
|
Graded by evaluation of report submitted by students.
|
| ４． |
Textbook and Reference |
|
No text is used.
Materials including figures, pictures and movies are indicated on slide.
These will be presented by LMS.
|
| ５． |
Requirements (Assignments) |
|
Preparation (about 1.5 hour);The materials used in the lesson will be presented beforehand through LMS, so please read them and do research by yourself which you do not understand and deepen your knowledge about gas turbine. Please also summarize what you do not understand in a notebook and ask questions by writing on a paper distributed every lesson.
Review (about 1.5 hour); The materials used in the lesson are presented by LMS, so please use them for review about function, performance, and formulas equation of gas turbine. And also answer of exercises will be presented by LMS, so please become able to perform the calculation.
|
| ６． |
Note |
|
The contents of the lesson may be changed according to the progress.
|
| ７． |
Schedule |
|
| １. Types and characteristics of the aero-engine |
| ２. Overview of the turbo-engines |
| ３. Power of the turbo-engine |
| ４. Efficiency of the turbo-engine |
| ５. Basic components of the turbo-engine-1:Basic structure |
| ６. Basic components of the turob-engine-2:Air-inlet, Fan and Compressor |
| ７. Basic components of the turbo-engine-3:Combustion chamber and Turbine |
| ８. Basic components of the turbo-engine-4:Exhaust system and Accessories |
| ９. Conservation of momentum |
| 10. Characteristics of multi-staged compressors |
| 11. Compressor stall (surging) |
| 12. Flutter of the turbine blades |
| 13. Accessories of the turbo-engine-1:Fuel supply subsystem and ignition subsystem |
| 14. Accessories of the turbo-engine-2:Contorl subsystem and Lubrication subsystem |
| 15. Materials used for the turbo-engine |
|
|