used to decrease the velocity of the air.

in the combustion chamber

exhaust smoke and carbon particles formed inside combustion chamber

a transpiration cooling.

to protect combustion chamber from melting

(45:1 – 130:1)

turbo-prop and turbo-shaft engines

two cans by igniter plugs then moved through interconnector tubes to the remaining cans

snout shape

A tubo-annular.

smaller and lighter

too much fuel for the primary air in the combustion chamber

the primary dilution zone is 15:1

is correct mixture ratio and air velocity must be slow enough

has a set of flame tubes with common outer casing

Removal difficult and time consuming

Better thermal load distribution for the turbine

air flow vortex and help air fuel mixing