Duration
26h Th, 26h Pr
Number of credits
Lecturer
Language(s) of instruction
French language
Organisation and examination
Teaching in the first semester, review in January
Schedule
Units courses prerequisite and corequisite
Prerequisite or corequisite units are presented within each program
Learning unit contents
Classification of turbomachines;
Fluid dynamics applied to energy conversion
- Recap Fluid Dynamics: conservation equations; similarity; lift and drag;
- Mechanical and thermal energy, entropy;
- Turbomachines: frames of reference, Euler equation, rothalpy; velocity triangles; total conditions in the absolute and relative frame;
- Axial passages: force balances, power exchanges and losses; similarity, stage coefficients;
- Radial passages with or without blades
- Recapitulation: hydraulic forms of energy, head, head losses and hydraulic diagrams
- cavitation
- similarity: classification, scaling rules and extrapolation
- radial and axial pumps
- energy balance
- estimation of the conditions throughout the machine
- operating characteristics
- cavitation and NPSH
- operating point in a circuit: head, flow rate and NPSH
- control strategy: throttling, speed regulation, bypass
- multistage pumps, trimming and suppliers catalogues
- state equations; Mollier h-s diagram; polytropes;
- Mach number and sonic effects; total conditions; shocks
- duct flows with heat, friction and area change
- iterative estimation of flow conditions
- Eulers equation, rothalpy, total conditions in the absolute and relative frame, stage Mollier h-s diagram
- iterative estimation of the thermodynamic conditions in the turbomachine
- similarity scaling, corrected and reduced conditions
- axial and radial compressors
- definition of efficiencies
- speed characteristics and operating limits
- flow in typical compressor passages
- instabilities and remediation
- axial and radial turbines and link to applications
- definition of efficiencies of machine, stage and passage
- operating maps;
- Steam turbines: choice of stage types through the machine; regulation.
- Gas turbine blades: cooling
- component matching
- gas turbines, civil and military jet engines
- Turbochargers
Learning outcomes of the learning unit
- Understand the operation, the choice and the design consideration of the machine / stages in function of the application, its duty and the operating conditions;
- Estimate the operating point of a machine in an installation;
- Reconstruct the thermodynamic and fluid dynamic conditions in key locations of the machine and based on that provide an estimate of the performance;
- Provide a rough predesign of a stage or a simple machine;
Prerequisite knowledge and skills
Ideally, the student should have followed, or have obtained a similar knowledge as described in, the courses
- MECA0011 (Elements de mécanique des fluides)
- MECA0025 (Mécanique des fluides)
- MECA0002 (Thermodynamique appliquée et introduction aux machines thermiques)
Planned learning activities and teaching methods
- Weekly course sessions, on average 3 hours of theory and 1/2 hour of exercises
- 1 lab for measuring the performance of a turbomachine per group of 2 students
- 1 individual project on the design/performance analysis of a machine
Mode of delivery (face to face, distance learning, hybrid learning)
Face-to-face course
Course materials and recommended or required readings
Platform(s) used for course materials:
- eCampus
Further information:
Course notes and exercise compendium on e-campus;
Tables and articles e-campus.
Recommended generalizing books (available in applied sciences library,* electronic format)
- Fundamentals of Turbomachines, E. Dick
- Turbomachinery Flow Physics and Dynamic Performance, M. Schobeiri
- The Dynamics and Thermodynamics of Compressible Fluid Flow, E. Shapiro
- Aero-Thermodynamics and flow in Turbomachines, M.H. Vavra
- Hydrodynamics of Pumps, C.E. Brennen*
- Design and analysis of radial compressors, R. Van den Braembussche*
- Axial flow turbines, fluid mechanics and thermodynamics, J.H. Horlock
- Axial flow compressors, fluid mechanics and thermodynamics, J.H. Horlock
- Compressor aerodynamics, N. Cumpsty
- Jet propulsion : a simple guide to the aerodynamic and thermodynamic design and performance of jet engines, N. Cumpsty
Exam(s) in session
Any session
- In-person
written exam ( open-ended questions ) AND oral exam
Written work / report
Further information:
The total grade is composed of the marks on
- the report of the lab session
- the oral exam on theory
- the written exam on exercises
Work placement(s)
N/A
Organisational remarks and main changes to the course
Contacts
It is to first pose questions on theory, exercises and projects, either directly during the course sessions, or on the dedicated forum on e-campus, in order to share the information with as many as possible and to have a rather immediate answer. If still needed, personal or group appointments can be made via mail
- Koen Hillewaert (enseignant) koen.hillewaert@uliege.be
- Nicolas Leclère (assistant) n.leclere@uliege.be
Association of one or more MOOCs
There is no MOOC associated with this course.