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two categories for accessories driven by the turbine
driven by bleed air
driven mechanically
dual-axial compressor engines have three separate bleed air system
high pressure
low pressure
interstage bleed-air
high and low pressure systems are used to drive
aircraft and engine components or accessories
interstage bleed valves are required
to ensure compressor stability
on dual/split spool axial compressors, low pressure bleed air is
extracted between the low pressure and high pressure spools
dual-axial compressor engines have two accessory drive gear boxes connected to
the low pressure compressor and the other to the high pressure compressor
starter system purpose
accelerate the engine until the turbine is producing enough power to continue engine acceleration by itself
starting cycle
as the compressor has been accelerated enough, ignition is actiavted and then the fuel is added
different abnormal starts
hot start
hung start
false start
wet start
hot start
exceeding the maximum allowable temperature for the turbine section during start
hung start
temperature within the turbine section continues to rise, and the compressor stabilizes below normal
false start
compressor rpm stabilizes below normal, and turbine temperature remains within limits
wet start
fuel-air mixture does not light off initially, but has the capability to eventually ignite
most dangerous abnormal start
wet start
two different types of starters
DC electric motor
air turbine starter
what type of ignition system is normally used for gas turbine engines
high energy capacitor-type ignition system
why is the high energy capacitor-type ignition system used
provides both high voltage and an exceptionally hot spark, which affords an excellent chance of igniting the fuel-air mixture at reasonably high altitudes
how many ignitor plugs is a gas turbine engine provided with
2
annular gap plug
protrudes slightly into the combustion chambers liner to provide effective spark
constrained-gap plug
the spark does not closely follow the face of the plug and jumps in an arc which carries beyond the face of the chamber liner
two types of ignitor plugs used
annular gap
constrained-gap