Educational guide | ||||||||||||||||||||||||||||||||||||||||
IDENTIFYING DATA | 2024_25 | |||||||||||||||||||||||||||||||||||||||
Subject | AIRCRAFT ENGINE INSTALLATION | Code | 00710343 | |||||||||||||||||||||||||||||||||||||
Study programme |
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Descriptors | Credit. | Type | Year | Period | ||||||||||||||||||||||||||||||||||||
6 | Compulsory | Fourth | Second |
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Language |
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Prerequisites | ||||||||||||||||||||||||||||||||||||||||
Department | ING.MECANICA,INFORMAT.AEROESP. |
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Coordinador |
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jgong@unileon.es ddomf@unileon.es dlopr@unileon.es |
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Lecturers |
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Web | http:// | |||||||||||||||||||||||||||||||||||||||
General description | ||||||||||||||||||||||||||||||||||||||||
Tribunales de Revisión |
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Competencias |
Code | |
A17712 | |
A17713 | |
B958 | |
B960 | |
B961 | |
B5474 | |
B5477 | |
C1 | CMECES1 That students have demonstrated possession and understanding of knowledge in an area of study that is based on general secondary education, and is usually found at a level that, although supported by advanced textbooks, also includes some aspects that involve knowledge from the cutting edge of their field of study |
C4 | CMECES4 That students can transmit information, ideas, problems and solutions to both a specialised and non-specialised audience |
C5 | CMECES5 That students have developed those learning skills necessary to undertake further studies with a high degree of autonomy |
Learning aims |
Competences | |||
To learn the calculation and modeling methods of the different components and auxiliary systems of the aviation engine | A17712 A17713 |
B958 B960 B961 B5474 B5477 |
C1 C4 C5 |
To apply magnitude measurement techniques | A17712 A17713 |
B958 B960 B961 B5474 B5477 |
C1 C4 C5 |
To know methods and systems necessary to carry out automatic engine control | A17712 A17713 |
B958 B960 B961 B5474 B5477 |
C1 C4 C5 |
Contents |
Topic | Sub-topic |
Bloque I: SYSTEMS AND THEORY OF LUBRICATION | Lesson 1: THEORY OF LUBRICATION Lesson 2: LUBRICATION SYSTEMS OF RECIPROCATING ENGINES Lesson 3: LUBRICATION SYSTEMS OF JET ENGINES |
Bloque II: INTERNAL AIR AND REFRIGERATION SYSTEMS | Lesson 1: PNEUMATIC SYSTEMS OF JET ENGINES Lesson 2: COOLING OF JET ENGINES |
Bloque III: POWER EXTRACTION SYSTEMS, GEARS AND REDUCERS | Lesson 1: ACCESSORY GEAR BOXES Lesson 2: GEAR-BOX SYSTEMS |
Bloque IV: STARTING AND IGNITION SYSTEMS | Lesson 1: STARTING SYSTEMS OF JET ENGINES Lesson 2: IGNITION SYSTEMS OF JET ENGINES |
Bloque V: INCREASING THRUST AND THRUST VARIATIOR SYSTEMS | Lesson 1: POST-COMBUSTION SYSTEMS Lesson 2: WATER INJECTION SYSTEMS Lesson 3: BRAKING SYSTEMS OF JET ENGINES Lesson 4: VTOL AND VECTORED THRUST SYSTEMS |
Bloque VI: ANTI-ICE AND ANTI-FIRE SYSTEMS | Lesson 1: DEFROST AND ANTI-ICE SYSTEMS Lesson 2: ANTI-FIRE SYSTEMS OF JET ENGINES |
Bloque VII: MEASUREMENT AND INDICATIONS SYSTEMS | Tema 1: MEASUREMENT AND INDICATIONS SYSTEMS |
Bloque VIII: FUEL CONTROL SYSTEMS | Tema 1: FUEL CONTROL SYSTEMS OF RECIPROCATING ENGINES Tema 2: FUEL CONTROL SYSTEMS OF JET ENGINES |
Planning |
Methodologies :: Tests | |||||||||
Class hours | Hours outside the classroom | Total hours | |||||||
Problem solving, classroom exercises | 20 | 30 | 50 | ||||||
Laboratory practicals | 8 | 15 | 23 | ||||||
Personal tuition | 1 | 0 | 1 | ||||||
Lecture | 28 | 45 | 73 | ||||||
Mixed tests | 2.5 | 0 | 2.5 | ||||||
0.5 | 0 | 0.5 | |||||||
(*)The information in the planning table is for guidance only and does not take into account the heterogeneity of the students. |
Methodologies |
Description | |
Problem solving, classroom exercises | |
Laboratory practicals | |
Personal tuition | |
Lecture |
Personalized attention |
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Assessment |
Description | Qualification | ||
Mixed tests | Written test with theoretical questions and exercises. | 75% | |
Individual or group report about the activies or topics covered during the course. | 25% | ||
Other comments and second call | |||
(1) The completion of the requested work (individual or group), as well as possible field practices/outings, will be mandatory for the preparation of the final evaluation and its completion may be subject to the availability of the necessary resources and facilities. (2) The preparation of the final mark, weighted between the assignments and the mixed tests, may be subject to obtaining a minimum grade in each of the parts. (3) In the second call, the score related to the work carried out during the course will be kept |
Sources of information |
Access to Recommended Bibliography in the Catalog ULE |
Basic |
Jack L. Kerrebrock, Aircraft Engines and Gas Turbines, MIT, 1992 Bernie MacIsaac, Roy Langton, Gas turbine propulsion systems, Willey, 2011 |
Complementary |
Martín Cuesta Álvarez, Motores de Reacción, Paraninfo, Borja Galmés Belmonte, Motores de Reacción y Turbinas de Gas, Paraninfo, Mattingly, Heiser, Pratt, Aircraft Engine Design, AIAA Education Series, Mattingly, J.D., Elements of Gas Turbine Propulsion, Mc Graw-Hill, Meherwan P. Boyce, Gas turbine engineering handbook, Elsevier/Butterworth-Heinemann, 2012 Hill, Petterson, Mechanics and Thermodinamic of Propulsion, Addison Wesley, Antonio Esteban Oñate, Motores de pistón para aviones, Módulo 16, EASA66, Paraninfo, Oates, G. C., The Aerothermodynamics of Gas Turbine and Rocket Propulsion, AIAA Education Series, |
Recommendations |
Other comments | |
The implementation of the different activities in this teaching guide is subject to the existence of sufficient technical, material and human resources. Completing the practices in the laboratory/computer classroom and assignments is mandatory to pass the subject. The final grade of the subject may require obtaining a minimum grade in any of the parts that compose the evaluation. The elements that compose the evaluation can be sequenced throughout the course according to the different parts they consist of. In the second call, the score related to the practices in the computer laboratory/classroom and work carried out during the course will be kept. Many of the information sources are in English but there are parts in Spanish |