Module 15. Gas Turbine Engine (Part-66)
Module 15. Gas Turbine Engine (Part-66)
Duration
420 hours training
Number of Participants
None.
Price
None.
Content
Content: Part-66 Module 15. Gas Turbine Engine
1. Fundamentals
- Potential energy, kinetic energy, Newton's laws of motion, Brayton cycle;
- The relationship between force, work, power, energy, velocity,acceleration;
- Constructional arrangement and operation of turbojet, turbofan,turboshaft, turboprop.
2. Engine Performance
- Gross thrust, net thrust, choked nozzle thrust, thrust distribution, resultantthrust, thrust horsepower, equivalent shaft horsepower, specific fuelconsumption;
- Engine efficiencies;
- By-pass ratio and engine pressure ratio;
- Pressure, temperature and velocity of the gas flow;
- Engine ratings, static thrust, influence of speed, altitude and hot climate, flat rating, limitations.
3. Inlet
- Compressor inlet ducts;
- Effects of various inlet configurations;
- Ice protection.
4. Compressors
- Axial and centrifugal types;
- Constructional features and operating principles and applications;
- Fan balancing;
- Operation;
- Causes and effects of compressor stall and surge;
- Methods of air flow control: bleed valves, variable inlet guide vanes,variable stator vanes, rotating stator blades;
- Compressor ratio.
5. Combustion Section
- Constructional features and principles of operation.
6. Turbine Section
- Operation and characteristics of different turbine blade types;
- Blade to disk attachment;
- Nozzle guide vanes;
- Causes and effects of turbine blade stress andcreep.
7. Exhaust
- Constructional features and principles of operation;
- Convergent, divergent and variable area nozzles;
- Engine noise reduction;
- Thrust reversers.
8. Bearings and Seals
- Constructional features and principles of operation.
9. Lubricants and Fuels
- Properties and specifications;
- Fuel additives;
- Safety precautions.
10. Lubrication Systems
- System operation/lay-out and components.
11. Fuel Systems
- Operation of engine control and fuel meteringsystems including electronic engine control(FADEC);
- Systems lay-out and components.
12. Air Systems
- Operation of engine air distribution and anti-ice control systems, includinginternal cooling, sealing and external air services.
13. Starting and Ignition Systems
- Operation of engine start systems and components;
- Ignition systems and components;
- Maintenance safety requirements.
14. Engine Indication Systems
- Exhaust Gas Temperature/Interstage Turbine Temperature;
- Engine Thrust Indication: Engine Pressure Ratio, engine turbinedischarge pressure or jet pipe pressure systems;
- Oil pressure and temperature;
- Fuel pressure and flow;
- Engine speed;
- Vibration measurement and indication;
- Torque;Power.
15. Power Augmentation Systems
- Operation and applications;
- Water injection, water methanol;
- Afterburner systems.
16. Turbo-prop Engines
- Gas coupled/free turbine and gear coupled turbines;
- Reduction gears;
- Integrated engine and propeller controls;
- Overspeed safety devices.
17. Turbo-shaft engines
- Arrangements, drive systems, reduction gearing, couplings, controlsystems.
18. Auxiliary Power Units (APUs)
- Purpose, operation, protective systems.
19. Powerplant Installation
- Configuration of firewalls, cowlings, acoustic panels, engine mounts, antivibrationmounts, hoses, pipes, feeders, connectors, wiring looms, controlcables and rods, lifting points and drains.
20. Fire Protection Systems
- Operation of detection and extinguishing systems.
21. Engine Monitoring and Ground Operation
- Procedures for starting and ground run-up;
- Interpretation of engine power output and parameters;
- Trend (including oil analysis, vibration and boroscope) monitoring;
- Inspection of engine and components to criteria, tolerances and dataspecified by engine manufacturer;
- Compressor washing/cleaning;
- Foreign Object Damage.
22. Engine Storage and Preservation
- Preservation and depreservation for the engine and accessories/systems.
Objectives
None.
Target Group
None.
Aircraft Engine
None.
Prerequisites
None.
Examination
None.
