1. Being able to systematically understand the thermodynamic cycle, aerodynamic principles, and cooperative mechanisms among major components of gas turbine engines (including compressors, combustion chambers, and turbines), and to qualitatively analyze the influence of parameters such as rotational speed and altitude on engine performance.
2. Capable of accurately identifying key structural configurations of aero engines-including overall layout, rotor support systems, and major connections-while demonstrating a deep comprehension of the inherent logic that “principle determines structure, and structure realizes function.”
3. Possessing an initial capability in systems thinking and engineering analysis, being able to apply theoretical knowledge to basic performance estimations and logical reasoning of typical failures, thereby establishing a solid foundation for advanced professional work in engine design, manufacturing, maintenance, and fault diagnosis.