Aircraft Engines & Gas Turbines
Professional aerospace engineering training focused on aircraft jet engines, gas turbine performance, engine components, thermodynamic behaviour and modern propulsion system design considerations.
Aircraft Engines & Gas Turbines
This professional training programme develops a technical understanding of aircraft jet engines and gas turbines, with emphasis on component performance, engine characteristics, design limitations and future trends.
Course Overview
The programme examines the performance and characteristics of aircraft jet engines and industrial gas turbines through the thermodynamic and fluid-mechanical behaviour of major engine components.
It covers inlets, compressors, combustors, turbines and nozzles, together with engine configurations, material limitations and important future design considerations.
Training Objectives
- Understand aircraft engine operating principles.
- Analyse fundamental gas turbine performance.
- Understand major engine component functions.
- Evaluate thermodynamic and fluid-mechanical behaviour.
- Understand modern turbofan configurations.
- Recognise key engine design limitations and trade-offs.
Who Should Attend
Engineering Professionals
- Aerospace Engineers
- Aircraft Engine Engineers
- Propulsion Engineers
- Gas Turbine Engineers
- Mechanical Engineers
- Thermal and Fluid Engineering Professionals
Technical & Research Professionals
- Engine Performance Professionals
- Propulsion System Analysts
- Aircraft Design Professionals
- Aerospace Researchers
- Technical Project Engineers
- Engineering Managers and Technical Leads
5-Day Professional Training Programme
A structured programme covering aircraft engine components, gas turbine performance, engine configurations and modern aerospace propulsion design.
Day 1 — Aircraft Engine Fundamentals
- Aircraft jet engine fundamentals
- Gas turbine operating principles
- Engine performance characteristics
- Thermodynamic foundations
- Fluid-mechanical behaviour of engines
- Engine performance requirements
Day 2 — Inlets & Compressors
- Aircraft engine inlet systems
- Inlet flow behaviour
- Compressor operating principles
- Compressor performance considerations
- Pressure and temperature relationships
- Component-level performance analysis
Day 3 — Combustors & Turbines
- Combustor operating principles
- Combustion and energy conversion
- Turbine operating fundamentals
- Turbine performance characteristics
- Thermal and mechanical considerations
- Engine component interaction
Day 4 — Nozzles & Engine Configurations
- Engine nozzle fundamentals
- Exhaust flow and thrust generation
- Turbojet engine configurations
- Turbofan engine configurations
- Advanced turbofan concepts
- Engine performance comparison
Day 5 — Future Engine Design
- Material properties and engine limitations
- Engine weight considerations
- Fuel consumption reduction
- Noise reduction considerations
- Pollutant formation and reduction
- Future aircraft engine design trends
Aircraft Engine Engineering in Practice
Apply engine performance and component-level engineering principles to modern aircraft propulsion systems and future engine design challenges.