5 ECTS credits
140 h study time

Offer 1 with catalog number 4016330FNR for all students in the 1st semester at a (F) Master - specialised level.

Semester
1st semester
Enrollment based on exam contract
Impossible
Grading method
Grading (scale from 0 to 20)
Can retake in second session
Yes
Enrollment Requirements
Registration for Aircraft Propulsion is allowed if one has successfully accomplished or is registered for 30 ECTS of (semi)common courses of the Master in Electromechanical Engineering, AE track (Dutch program idem).
Taught in
English
Partnership Agreement
Under interuniversity agreement for degree program
Faculty
Faculty of Engineering
Department
Applied Mechanics
External partners
Université libre de Bruxelles
Educational team
Patrick Hendrick (course titular)
Activities and contact hours
36 contact hours Lecture
24 contact hours Seminar, Exercises or Practicals
Course Content

The valid fiche can be found at the following link : MECA-H507. Change the language to English in the dropdown menu on top of the page.

Thermodynamics of turboengines, performances and optimisation, flight domain, future developments. Study of the components as parts of the turboengine, inlets, compressors, combustion chambers, turbines, exhaust pipes and nozzles. Problems due to these components in flight as well as in maintenance and useful life predictions. The equilibrium working points and steady state lines of engines, monitoring, engine control by the pilot, the fuel control.

Previous knowledge : Theoretical mechanics, technical thermodynamics applied on compressors and turbines, basic concepts of aerodynamics and nozzles (sub- and supersonic flow), of strength and properties of materials, of the control theory.

Additional info

Study material : Courses of Professor Jacques, published by VUB (4 parts). Nr. 409 - Energetische studie der propulsiemotoren, part I : Theory, Nr. 410 part II : Figures / Nr. 413 - Inlaten, compressoren en verbrandingskamers van straalmotoren, part I : Theory, Nr. 414 - part II : Figures / Nr. 411 - Turbines en uitlaten, part I : Theory, Nr. 412 - part II : Figures / Nr. 418 - Werkingslijnen, sturing en regeling, part I : Theory, Nr. 419 - part II : Figures.

Complementary study material : documents on performance of engines, modern evolutions, characteristics of materials, used for the numerical applications and exercises.

Learning Outcomes

General competencies

Acquire a scientific thorough knowledge of the gasturbines, turbojet- and fanengines, turbopropulsors and their major components.

Knowledge oriented competences

Having in-depth knowledge and understanding of exact sciences with the specificity of their application to engineering.

Knowledge oriented competences

Having in-depth knowledge and understanding of integrated structural design methods in the framework of a global design strategy.

Knowledge oriented competences

Having in-depth knowledge and understanding of the advanced methods and theories to schematize and model complex problems or processes.

Knowledge oriented competences

Having a broad scientific knowledge, understanding and skills to be able to design, produce and maintain complex mechanical, electrical and/or energy systems with a focus on products, systems and services. E.g. codepo project, courses around renewable, sustainable mobility,...

Knowledge oriented competences

Having an in-depth understanding of safety standards and rules with respect to mechanical, electrical and energy systems.

Scientific competences

Can present and defend results in a scientifically sound way, using contemporary communication tools, for a national as well as for an international professional or lay audience.

Grading

The final grade is composed based on the following categories:
Other Exam determines 100% of the final mark.

Within the Other Exam category, the following assignments need to be completed:

  • exam with a relative weight of 1 which comprises 100% of the final mark.

Additional info regarding evaluation

Oral and written examination.  Oral examination is with closed book on theoretical questions with preparation time.  Written examination is with open book and documentation, several exercises are proposed.

Examination requirements : The theoretical principles must be understood and explained, based on the engineering sciences acquired in the previous training. The theory must be applied on numerical problems, knowledge of the physical quantities and units, and use of the information and charts provided by the manufacturers.

Allowed unsatisfactory mark
The supplementary Teaching and Examination Regulations of your faculty stipulate whether an allowed unsatisfactory mark for this programme unit is permitted.

Academic context

This offer is part of the following study plans:
Master of Electromechanical Engineering: Aeronautics and Aerospace (only offered in Dutch)
Master of Electromechanical Engineering: Aeronautics