Gas Turbine Compressor Flashcards
Highe compression ration»_space;more thermal efficient
35:1
Compression ratio
Is the ratio of compressor output to compressor inlet pressure
Types of compressor
~axial flow compressor
~centrifugal compressor
Centrifigual compressor compression ratio
With one centrifugal»_space;4,5:1
2 stages»_space; theoretically 20.25 :1 But in reality 12:1
Cannot aerodynamically stall
Is too noisy and is not enough as new axial compressors
Axial flow compressor
Rotors are always before the stator and the stator makes a divergence angle to slow down the speed and increase the static pressure and temperature
Compression ratio»_space; 1,1 :1 to 1,2:1 (10% to 20%)
~across rotor velocity,pressure and temp increases
~across the stator the velocity reduces and pressure ,temperature increase
Across the multiple stages velocity remains constant,but pressure and temperature increases
Convergent air annulas from the front part to the rear part in the compression stage
Compressor stall
Blade stall:
~damage
~ice
~extreme incidence angles
Symptoms of compressor stall are: ~high gas temperature ~reduce thrust ~rumbling or banging from the compressor ~fluctuating RPM and fuel flow
Compressor surge
~a very severe stall compressor output pressure falls below combustion pressure,gases flow forward through the compressor
~in an extreme case flames may be seen exiting intake
~over fuelling can cause a surge by creating excessive pressure in the combustor (mostly eliminated my electronic modern fuel control units)
Stall alleviation
~variable inlet guide vanes (VIGV) adjust their angle to ensure that air directed onto the first stage .
~on some engines variable stator vanes (VSVs) do the same thing for each stage
Handling bleed or inter stage bleed or transient bleed
To expel air if in excess
Stall alleviation - bleed valves
~inter stage valves vent pressure during the start to improve axial flow across the compressor (know as handling bleed).
These reduces the load on the compressor bringng it closer to the working line during engine start.
Generally ,valves are open when eng switched off and gradually close,to become fully closed at ground idle speed
MULITPLE SPOOL
~allow each compressor to run at its optimal speed
~reduce the need for complex air control system to prevent stall and surge
Compressor blades
Rotor blades are fitted loosely so that they take up a least stress position during rotation
Blades are held in three ways :
~mechanically»_space;the dovetail
~centrifugally»
~aerodynamically»air pressure will hold the blade in a stable positon
centrifugal compressor benefits
~is cheaper,less prone to surge and damage,shorter and reasonably efficient
But has low compression ration 4,4:1 compraed to at least 35:1` for anaxial flow
~for given mass flow it requires a larger frontal area
~it less efficient than axial comprewssor
Axial
~is very efficent
~has high compression ratio
~ is vuknerable to surge