15.6 TURBINE SECTION Flashcards
The gas generator turbine is to absorb approximately —-% of total pressure energy from exhaust gases
60-70%
Where is the turbine section of a gas turbine engine located
- Aft
- directly behind the combustion chamber outlet
What are the 2 different types of turbines on gas turbine engines
- radial flow turbine
- axial flow turbine
The 2 types of turbine have the same main components which are?
- stationary vanes (turbine nozzle guide vanes)
- set of moving rotor blades
Explain radial flow turbines
- always single-stage turbines
- used on small gas turbine engines (e.g. APU)
What are the disadvantages of radial flow turbines
- allow small airflow and less efficient (high aerodynamic losses)
Advantages of radial flow turbines
- simple design
- easy to manufacture
Explain axial flow turbines
- can be built with any number of turbine stages as necessary
Advantage of axial flow turbines
- allow very high airflow that is required to create high thrust
On modern gas turbine engines, which flow turbine is used
Axial
What does the turbine convert
Gas energy from combustion chamber into torque to drive turbine shaft
Explain impulse turbine
Turbine that makes rotation only by the impact of the gas flow on rotor blades
What are the 3 classification of turbine blades
- Impulse configuration
- Reaction configuration
- Reaction-impulse configuration
Explain impulse configuration
- pressure drop across each stage occurs in the fixed nozzle guide vanes (due to convergent shape)
- increase gas velocity, reducing pressure
Explain reaction configuration
- the fixed nozzle guide vanes are designed to alter the gas flow direction without changing the pressure
