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Gas Turbine Compressors Flashcards | StudBud
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Gas Turbine Compressors
Gas Turbine Compressors
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Aircraft gas turbine compressor review.
Flashcards
21 cards
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Practice quiz
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Questions
21
Answers
1
The aft turbine drives the N1 compressor in a dual spool engine.
False
True
2
Which component in a compressor adds kinetic energy to the air passing through the engine?
Fan
Nozzle
Rotors
Stators
3
The speed of the low-pressure compressor does what as the aircraft goes up in altitude?
Stalls
Slows down
Speeds up
Remains constant
4
The low-pressure compressor in a dual-spool engine is designated as N1
False
True
5
Single-stage, single sided & single-stage dual sided, & two stage, single sided are types of?
centrifugal compressors
axial flow compressors
combination compressors
rotary compressors
6
The inlet guide vanes are directly behind the last stage of compression
False
True
7
The inlet guide vanes direct the airflow into the compressor at the most desirable angle
False
True
8
What type of overall shape is the gas path passage in an axial flow compressor?
Concentric
Divergent
Oblong
Convergent
9
What causes a compressor stall in a gas turbine engine?
my mom told me not to play with you anymore
too lean a mixture in the turbine section
excessive fuel flow on start up
there is an imbalance between the air flow supply and the airflow demand
10
How are compressor blades normally fit into the compressor disk?
Bolted in place
Press fit
Dove-tail slot
Structural adhesive
11
Compression ratio is found by comparing the compressor discharge pressure and inlet pressure.
False
True
12
The stators in an axial flow compressor diffuse the air to change velocity energy into pressure energy.
False
True
13
What are two functions of a compressor in a gas turbine engine?
supplies bleed air to cool the internal hot section
Increases air velocity
Increases the pressure of the air mass
Decreases air mass
14
What are some advantages of the axial flow compressor?
Light weight
High pressure rise per stage
Higher pressure ratio
Smaller frontal area
15
What two factors determine the angle of attack of the compressor blades in a gas turbine engine?
The ram recovery velocity quotient
The rotational speed of the rotor blades
Inlet stagnation density
The velocity of the air entering the engine
16
Select all that apply to shaft configurations in gas turbines.
Dual-spool
Single-spool
Variable-spool
Triple-spool
17
What are the two basic types of compressors used on gas turbine engines?
Combined compressors
Centrifugal compressors
Axial flow compressors.
Radial compressors
18
What are the three major components in a centrifugal compressor?
Diffuser
Air Seperator
Impeller
Manifold
19
The diffuser is a convergent duct.
False
True
20
What's the difference between an orange?
Mind your own business
The workers control of factories in the urban prolitariat
The lugubrious variability of turgid thought makes enlightenment moribund
Ten cents if a deep fried cat fell off a ten story building
21
What are the two main elements of an axial-flow compressor?
Rotor & Stator
Spinner & Guide vanes
Rotor & Nozzle
Impeller & Diffuser