15.5 combustion section Flashcards
what are the following requirements the combustion chamber must fulfil
- it must permit safe ignition of the fuel-air mixture both on ground and in flight
- give stable combustion in all operating conditions of the engine
- combustion must also be complete
what are the two primary conditions necessary for correct and safe combustion
- the ratio of air and fuel must be correct
- the air velocity must be slow enough to make sure that the combustion is completed inside the combustion chamber
approximately how much of the airflow is from the compressor
20% to 30%
what are the three types of combustion chamber
can-type
can-annular
annular
what are the two main components on each combustion chamber
- the combustion chamber casing
- the flame tube found inside the casing
to complete combustion of a kerosene-air mixture, what ratio is needed
15 part air, 1 part fuel (15:1)
what does each combustion camber have in can-type camber
- air supply duct
2.fuel nozzle - flame tube
- casing
what are the advantages of can-type combustion chamber
- simple design
- very good structural strength
- they can be removed and replaced individually
what is the advantage of can-annual over multiple-can-type combustions chamber
they are smaller and lighter
what are the three major components of an annular combustion chamber
- the dome
- the inner liner
- the outer liner
what is the disadvantage of annular combustion chamber
they are expensive to make and removal is very difficult and time consuming
what does the combustion case consist of
- outer wall
- inner wall
- diffuser
what connects the inner liner with the outer liner on the flame tube
the dome
how is the flame tube connected to the combustion case
bolts
what is it called if there is too much fuel for the primary air in the combustion chamber
rich mixture
what does the combustion chamber casing do
it takes air pressure loads and protects the internal and external engine parts from hot combustion gases
what is the disadvantage of can-annual
the aerodynamic losses are quite high and the ignition from one flame tube to the others is very difficult
what does the secondary airflow form to help protect the liner from the intense heat of the combustion gases
a cooling film