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Educational guide | |||||||||||||||||||||
| IDENTIFYING DATA | 2023_24 | |||||||||||||||||||||
| Subject | JET ENGINES | Code | 00710024 | |||||||||||||||||||
| Study programme | ||||||||||||||||||||||
| Descriptors | Credit. | Type | Year | Period | ||||||||||||||||||
| 6 | Compulsory | Third | ||||||||||||||||||||
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| General description | ||||||||||||||||||||||
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| Competencias |
| Code | |
| C2 | CMECES2 That students know how to apply their knowledge to their work or vocation in a professional manner and possess the skills that are usually demonstrated through the development and defense of arguments and the resolution of problems within their area of study. |
| C3 | CMECES3 That students have the ability to gather and interpret relevant data (normally within their area of study) to make judgments that include reflection on relevant issues of a social, scientific or ethical nature. |
| C4 | CMECES4 That students can transmit information, ideas, problems and solutions to both a specialised and non-specialised audience |
| Learning aims |
| Competences | |||
| A8703 A8772 A8956 A8960 A8978 |
B958 B959 B960 B961 B964 |
C2 C3 C4 |
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| A8703 A8772 A8827 A8942 A8956 A8978 |
B958 B959 B960 B961 B964 |
C2 C3 C4 |
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| Contents |
| Topic | Sub-topic |
| Bloque I: INTRODUCTION | Tema 1: JET ENGINE INTRODUCTION Historical introduction and jet engine evolution |
| Bloque II: JET ENGINE ARCHITECTURE | Tema 1: ARCHITECTURE AND CLASSIFICATION Jet engine classification and basic configuration |
| Bloque III: THERMODYNAMIC CYCLE ANALYSIS | Tema 1: REAL THERMODYNAMIC CYCLE Ideal to real thermodynamic cycle aproximations of jet engines |
| Bloque IV: ENGINE COMPONENT ANALYSIS | Tema 1: INTAKES Architecture and performance Tema 2: AXIAL COMPRESSORS Architecture and performance Tema 3: RADIAL COMPRESSORS Architecture and performance Tema 4: COMBUSTORS AND AFTERBURNERS Architecture and performance Tema 5: TURBINES Architecture and performance Tema 6: NOZZLES Architecture and performance |
| Bloque V: ENGINE PERFORMANCE | Tema 1: TURBENE AND COMPRESSOR SHAFT Compressor-turbine matching Tema 2: PERFORMANCE MAPS Compressor and turbine maps |
| Planning |
| Methodologies :: Tests | |||||||||
| Class hours | Hours outside the classroom | Total hours | |||||||
| Lecture | 0 | 0 | 0 | ||||||
| Mixed tests | 2 | 0 | 2 | ||||||
| (*)The information in the planning table is for guidance only and does not take into account the heterogeneity of the students. | |||||||||
| Methodologies |
| Description | |
| Lecture |
| Personalized attention |
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| Assessment |
| Description | Qualification | ||
| Mixed tests | 100 % | ||
| Other comments and second call | |||
| Sources of information |
| Access to Recommended Bibliography in the Catalog ULE |
| Basic |
Jack D. Mattingly,, Elements of Gas Turbine Propulsion, Mac Graw-Hlll, New York, 1988
Hill & Peterson, Mechanics and Thermodynamícs of Propulsion, Addison-Wesley Reading, Massachusets, 1992 |
| Complementary |
Rolls Royce , The Jet Englne , Rolls Royce , Derby, 1986
Jack D. Mattingly , Aircraft Engine Design , American Institute of Aeronautics and Astronautics , New York, 1987
Daly, Mark , Jane's Aero Engines , IHS , 2012
J.L. Montañes García , Motores de reacción y turbinas de gas , ETSI Aeronáuticos, Madrid, 2005 |
| Recommendations |
| Subjects that it is recommended to have taken before | ||||||
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