unit 2 Flashcards
A jet engine derives its name from its design in that it uses
an exhaust-gas driven turbine wheel to drive its compressor
A turbo-supercharger is essentially a
high-capacity air pump
The two forces that air is subjected to after it is drawn into the guide vanes of centrifugal compressor are
rotational and centrifugal
A constructional feature of the centrifugal compressor is that the impeller
is forged as a single unit
The jet engine compressor that is cheaper to manufacture is the
centrifugal type, because of its fewer parts
Which is a constructional feature of an axial-flow compressor casing?
Split along the horizontal centerline
The percentage of combustion efficiency of a gas turbine is usually between
95 and 100
What is the most probable cause of flameout of a jet engine flying at 40,000 feet with a constant engine revolution per minute (rpm) of 50 percent?
the rpm is too low
The excess airflow that is not burned in the combustion section is used to
mix with and cool the burned gases
The inner and outer surfaces of an annular-type combustion chamber are formed by
interlocking stainless-steel bands
Fuel that accumulates after a failed start is
drained overboard by a drain system
The parts on a can-annular combustion section must be removed in a specific order because of the
combustion chamber crossover tubes
What is the most common type of fuel nozzle system?
Pressure-atomizing
Three types of turbine and van assemblies used in jet engines are impulse, reaction, and
reaction-impulse
The “fir tree” method of attaching turbine blades (buckets) to the turbine rotor disc is preferred because
of the temperature differential between the turbine rotor disc and the blades.