Thermal Machines
Objectives
General characterization
Code
12041
Credits
3.0
Responsible teacher
José Fernando de Almeida Dias
Hours
Weekly - 3
Total - 64
Teaching language
Português
Prerequisites
For the discipline of Air conditioning and Refrigeration it is supposed a strong domain of subjects learned in the disciplines of Applied Thermodynamics, Fluid Dynamics I and II, and Heat Transmission.
Bibliography
PowerPoints of the classes – available in the course page of CLIP.
Main Bibliography
Motores de Combustão Interna – Jorge Martins – Publindústria
Gas Turbine Theory - H. Cohen, G.F.C. Rogers e H. Saravanamutto - Longman
Other Bibliography
Internal Combustion Engine Fundamentals - John B. Heywood - McGraw-Hill
Motores Endotérmicos – Dante Giacosa – Ediciones Omega
Internal Combustion Engines - C.R. Ferguson - J Wiley
Elements of Gas Turbine Propulsion – J. D. Mattingly - McGraw-Hill
Jet Propulsion – Nicholas Cumpsty – Cambridge Univ. Press
An Introduction to Combustion – Stephen R. Turns - McGraw-Hill
Teaching method
Evaluation method
1- The assessment involves making:
a_ 1 group project of a gas turbine;
b_ 1 group poject aboutreciprocating engines to be presented in the seminar course;
c_ 1 individual discussion of the project undertaken.
2- The final grade is individual and is given by:
Final Grade = (0.5 ×project) + (0.20 × work) + ((0.30 × individual discussion).
Subject matter
Reciprocating engines: Engine classification. Engine components. Spark-ignition (SI) engine operation cycle. Compression-ignition (CI) engine operation cycle. Examples of SI and Diesel engines. Engine design and operation parameters. Indicated and brake power. Operating variables which affect SI engine performance, efficiency and emissions. SI engine combustion chamber design. Variables which affect CI engine performance, efficiency and emissions. Supercharged and turbocharged engine performance.
Combustion: Combustion modes and flame types. Knock and surface ignition. Octane index and Cetane index. Pollutant formation and control.
Gas Turbines: Gas turbine for aircraft propulsion. Intake and propelling nozzle efficiencies. Simple turboject. The turbofan engine. The turboprop engine. Thrust augmentation. Centrifugal and axial flow compressors. Combustion systems. Axial and radial flow turbines. Prediction of performance of simple gas turbines.