15.06 Flashcards
What two types of turbines is there
Axial And radial flow
What does the turbine state provide power to drive?
Accessory gearbox & compressors
What are the two main components of a turbine ?
Stationary guide vanes
Turbine nozzle guide vanes
How many stages does a radial flow turbine always have?
One!
Where are radial flow turbines normally used?
They’re only used on small gas turbine engines like an APU
What are the pros and cons of a radial flow turbine
Advantage: they’re a simple design so easy to manufacture
Disadvantage: only allow small airflow
Less efficient
Where are axial flow turbines used?
Modern by bypass engines
What are the advantages of a axial flow turbine?
They can be built up with any number of stages, sufficient enough to drive gearbox and large fan
Secondly they allow very high air flow required to create thrust on bypass engines
What does the turbine convert gas energy into?
Torque
The gas flow from the combustion chambered is accelerated by what?
The convergent duct between the nozzle guide vanes
A turbine which makes the rotation only by the impact of gas flow in the rotor blade is called what?
An impulse turbine, it’s recognisable by the special shape of the rotor blade and they’re generally found on very old gas turbine engines.
Turbines must operate in very extreme environments, what two things must turbine materials be able to withstand?
Extremely high temps and very high centrifugal forces
Two factors reduce turbine life what are they?
- Material fatigue caused by many cycles
2. Corrosion causes by sulphuric acid due to high sulphur levels in fuel and high temp
What is material deformation known as?
Creep
What factors can increase the rate of creep?
High engine speeds and high temperatures and the amount of time
What are the two main reasons why turbines are cooled in modern engines?
- To increase service life done by internal cooling of nozzle guide vanes and rotor blades
- Better turbine efficiency, done by case cooling
What is convection cooling?
It’s the easiest method and it’s when cooling air flow passes through hollow turbine nozzle vanes and rotor blades
How does impingement cooling work?
Better cooling method, the airflow first flows through an insert fixed in the hollow turbine aerofoil which has many small holes which serves as a jet nozzle which has better heat transfer
What is film cooling
There’s further cooling improvement, cooling air is blown into the hot gas flow via small drill holes in turbine aerofoil. The gas stream deflects airflow and makes a film
Advantage and disadvantages of film cooling?
- It’s the most effective method because it uses minimal cooling air
- This cooling method is very expensive because small drill holes are difficult to make