2023-2024 / AERO0015-1

Mechanical design of turbomachinery

Duration

26h Th, 26h Pr, 30h Proj.

Number of credits

 Master of Science (MSc) in Aerospace Engineering, professional focus in turbomachinery aeromechanics (THRUST)5 crédits 
 Master of Science (MSc) in Aerospace Engineering5 crédits 

Lecturer

Loïc Salles

Language(s) of instruction

English language

Organisation and examination

Teaching in the first semester, review in January

Schedule

Schedule online

Units courses prerequisite and corequisite

Prerequisite or corequisite units are presented within each program

Learning unit contents

Turbomachinery Rotordynamics : Types of Modelling, Computation of Forward and Backward Critical Speeds, Campbell Diagram, Stability Analysis, Harmonic and Transient Responses, Multi-rotor behavior, Design of bearings, Instability Phenomena. Dynamics of Blades and Disks : Campbell Diagram, External Excitation Sources, Aeroelastic Problems, Bird Impact. Static Analysis of Compressor Blades : Leaning, Effect of Pre-Twist, Bending/Torsion Coupling. Static Analysis of Disks : Design Criteria. Lifetime Calculations of Turbine Blades.

Learning outcomes of the learning unit

The objective is to present the methods used in the aeronautical industry to analyze the dynamical behavior of turbomachines and to design mechanical components of turbojet engines such as compressor and turbine blades and disks.

Prerequisite knowledge and skills

This course requires basic knowledge in structural dynamics and of the finite element method.

Planned learning activities and teaching methods

Projects will be assigned to the students. It will give hands-on practice with methods used for the mechanical design of turbomachines.

Mode of delivery (face to face, distance learning, hybrid learning)

Face-to-face course


Additional information:

The course is organised face-to-face during the 1st quadrimester.

Recommended or required readings

Royce, Rolls. The jet engine. John Wiley & Sons, 2015.

Friswell, Michael I. Dynamics of rotating machines. Cambridge university press, 2010.

Rao, J. S. Turbomachine blade vibration. New Age International, 1991.

Exam(s) in session

Any session

- In-person

written exam ( open-ended questions ) AND oral exam

Written work / report


Additional information:

The final grade will be based on the written or oral exam of theory, the homework and their oral presentation. The exam will consist of answering questions on the course materials. Special attention will be devoted to the knowledge and to the understanding of the theoretical concepts. No document is allowed for the examination.

The assessment is based on the weighted geometric average of the projects and the exam. The final note is calculated as follows:

                  Final note = (Projects)^(0.7) * (Exam)^(0.3)

Work placement(s)

Organisational remarks and main changes to the course

If the sanitary conditions do not allow to be present at the university, the exam will be organised orally by visio-conference.

Contacts

Loic Salles (l.salles@uliege.be)

Association of one or more MOOCs