turbine engines Flashcards

1
Q

explain the main difference and advantage of a turbofan over a turbojet engine

A

a turbofan engine uses a fan to bypass some air around the engine core and to provide thrust. the advantage is that this provides additional thrust without increasing fuel flow

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2
Q

name the major components of a gas turbine engine

A

air inlet
compressor section
combustion section
turbine section
exhaust section
gearbox
accessory section

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3
Q

what determines the amount of airflow through a turbine engine?

A

the forward speed of the aircraft, compressor speed, and air density

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4
Q

name the two types of compressors commonly used in turbine engines

A

axial and centrifugal flow

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5
Q

name two different methods for attaching turbine engine rotor blades to the rotor disks

A

dovetail
root
bulb
fir-tree

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6
Q

what are the different types of combustion chambers used in turbine engines

A

can
annular
can-annular
reverse flow annular

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7
Q

what is a split compressor system

A

also called dual or twin spool compressors. these are connected to the turbine section with two rotor shafts, one inside the other

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8
Q

what prevents the combustion chambers from burning

A

cooling air along the inside of the liner

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9
Q

what is the purpose of the interconnecting tubes attached between the can-type combustion chambers

A

for flame propagation during engine start

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10
Q

what functions do axial flow turbine nozzles perfom

A

they direct the mass airflow to drive the turbine rotor at a specific angle

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11
Q

how is thermal stress relieved on a turbine disc

A

by directing bleed air onto the face of the disk, or by grooves being cut in the disk

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12
Q

what are carbon seals used for in turbine engines

A

they are used as oil seals for the rotor shaft bearings

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13
Q

what is shaft horsepower

A

it is an indication of the torque developed by a turboprop or turboshaft engine

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14
Q

when a turbofan or turbojet engine is shut down what should the mechanic listed for during coast-down

A

any rubbing sound or other unusual noises from the engine

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15
Q

what are the desired effects of turbine engine of turbine engine compressor field cleaning

A

removal of contaminant deposits from interior engine surfaces and improved engine performance

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16
Q

what methods are commonly used to accomplish turbine engine compressor field cleaning

A

fluid wash and abrasive grit blast

17
Q

what type of compressor blade damage may be found when inspecting compressor blades

A

dents
galling
pitting
cracks
scratches
burrs
burns
gouges

18
Q

what is used to mark both hot and cold section parts for repair

A

layout dye, commercial felt tip marker, or chalk

19
Q

what is the effect of relative humidity on a turbojet or turbofan power

A

negligible, no effect

20
Q

what may be the indications if a turbojet or turbofan engine is out of trim

A

the engine has high exhaust gas temperature at the target engine pressure ration for takeoff power

21
Q

what would the possible cause be for a turbojet or turbofan engine having high exhaust gas temperature, low RPM, and high fuel flow at all engine pressure ratio settings

A

possible turbine damage or loss of turbine efficiency