Turbinen-Luftstrahl-Triebwerke

More information

Remarks

Introduction, flight propulsion systems and their components

Requirements for aircraft engines, propulsion efficiency

Thermodynamic and gas-dynamic fundamentals, design calculation, thrust engine

Components of air-suction engines

Design and project planning of aero engines

Design of the engine and its components, selected chapters and current development


Learning Objectives:

Students will be able to:

  • compare the design of modern jet engines
  • analyze the operation of modern jet engines
  • apply the thermodynamic and fluid mechanical fundamentals of jet engines
  • explain the main components inlet, compressor, combustor, turbine and thrust nozzle and select them according to appropriate criteria
  • evaluate approaches to reducing pollutant emissions, noise and fuel consumption


Workload:

Attendance time: 21 h
Self-study: 42 h


Examination:

oral
Duration: 30 minutes

Aids: none

References

Hagen, H.: Aero gas turbines and their performance, G. Braun Verlag, 1982
Hünnecke, K.: Aero engines, their technology and function, Motorbuch Verlag, 1993
Saravanamuttoo, H.; Rogers, G.; Cohen, H.: Gas Turbine Theory, 5th Ed., 04/2001
Rolls-Royce: The Jet Engine, ISBN:0902121235, 2005