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EASA PART 66 MODULE 15 P2 - GAS TURBINE ENGINE

EASA PART 66 MODULE 15 GAS TURBINE ENGINE PART 2
(15.4 Compressors 15.5 Combustion Section 15.6 Turbine Section 15.7 Exhaust)

15.4 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.



15.5 Combustion Section
Constructional features and principles of operation.

15.6 Turbine Section Operation and characteristics of different turbine blade types;

  • Blade to disk attachment;
  • Nozzle guide vanes;
  • Causes and effects of turbine blade stress and creep.

15.7 Exhaust Constructional features and principles of operation;

  • Convergent, divergent and variable area nozzles;
  • Engine noise reduction;
  • Thrust reversers.

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