問題一覧
1
The fan rotational speed of a dual axial compressor forward fan engine is the same as the
low-pressure compressor
2
What turbine engine section provides for proper mixing of the fuel and air?
Combustion sections
3
In a gas turbine engine, combustion occurs at a constant
pressure
4
In the dual axial-flow or twin spool compressor system, the first stage turbine drives the
N2 compressor
5
The turbine section of a jet engine
drives the compressor section
6
What is the function of the stator vane assembly at the discharge end of a typical axial-flow compressor?
To straighten airflow to eliminate turbulence
7
Where is the highest gas pressure in a turbojet engine?
In the entrance of the burner section
8
An exhaust cone placed aft of the turbine in a jet engine will cause the pressure in the first part of the exhaust duct to
increase and the velocity to decrease
9
A turbine engine compressor which contains vanes or both sides of the impeller is a
double entry centrifugal compressor
10
Some engine manufacturers of twin spool gas turbine engines identify turbine discharge pressure in their maintenance manuals as
Pt7
11
Main bearing oil seals used with turbine engines are usually what type(s)?
Labyrinth and/or carbon rubbing
12
What are the two basic elements of the turbine section in a turbine engine?
stator and rotor
13
The function of the exhaust cone assembly of a turbine engine is to
straighten and collect the exhaust gases into a solid exhaust jet
14
What are the two functional elements in a centrifugal compressor?
Impeller and diffuser
15
An advantage of the axial-flow compressor is its
high peak efficiency
16
What is one purpose of the stator blades in the compressor section of a turbine engine?
Control the direction of the airflow
17
What is the purpose of the diffuser section in a turbine engine
To increase pressure and reduce velocity
18
How does a dual axial-flow compressor improve the efficiency of a turbojet engine?
Higher compression ratios can be obtained
19
Three types of turbine blades are
impulse, reaction, and impulse-reaction
20
Which statements are true regarding aircraft engine propulsion? 1. An engine driven propeller impar ts a relatively small amount of acceleration to a large mass of air. 2. Turbojet and turbofan engines impart a rela- tively large amount of acceleration to a smaller mass of air. 3. In modern turboprop engines, nearly 50 percent of the exhaust gas energy is extracted by turbines to drive the propeller and compressor with the rest providing exhaust thrust.
1 and 2
21
Which turbine engine cormpressor offers the greatest advantages for both starting flexibility and improved high-altitude performance?
Split-spool, axial-flow
22
Reduced blade vibration and improved airflow characteristics in gas turbines are brought about by
shrouded turbine rotor blades
23
In which type of turbine engine combustion chamber is the case and liner removed and installed as one unit during routine maintenance?
Can
24
The Diffuser section of a jet engine is located between
the compressor section and the burner section
25
Between each row of rotating blades in a turbine engine compressor, there is a row of stationary blades which act to diffuse the air. These stationary blades are called
stators
26
The two types of centrifugal compressor impellers are
single entry and double entry
27
Which two elements make up the axial-flow compressor assembly?
Rotor and stator
28
An advantage of the centrifugal-flow compressor is its high
pressure rise per stage
29
The highest heat-to-metal contact in a jet engine is the
turbine inlet guide vanes
30
A weak fuel to air mixture along with normal airflow through a turbine engine may result in
a lean die-out
31
What is used in turbine engines to aid in stabilization of compressor airflow during low thrust engine operation?
Variable guide vanes and/or compressor bleed valves.
32
In an axial-Tlow Compressor, one purpose of the stator vanes at the discharge end of the compressor is to,
straighten the airflow and eliminate turbulence
33
A purpose of the shroud on the turbine blades of an axial-flow engine is to
reduce vibration
34
In a dual axial-flow compressor, the first stage turbine drives
N2 compressor
35
What is the primary advantage of an axial-flow compressor over a centrifugal Compressor?
Greater pressure ratio
36
The purpose of a bleed valve, located in the beginning stages of the compressor, in an aircraft gas turbine engine is to
vent some of the air overboard to prevent a compressor stall
37
Ina turbine engine with a dual-spool compressor, the low speed compressor
seeks its own best operating speed
38
What is the function of the inlet guide vane assembly on an axial-flow compressor?
Directs the air into the first stage rotor blades at the proper angle.
39
The stator vanes in an axial-flow compressor
convert velocity energy into pressure energy
40
A gas turbine engine comprises which three main sections?
Turbine, compressor, and combustion
41
What type of turbine blade is most commonly used in aircraft jet engines?
Impulse-reaction
42
What is the primary factor which controls the pressure ratio of an axial-fiow compressor?
Number of stages in compressor
43
What is meant by a double entry centrifugal compressor?
A compressor with vanes on both sides of the impeller.
44
A high surge of current is required when a DC electric motor is first started. As the speed of the motor increases,
the counter EMF builds up and opposes the applied EME, thus reducing the current flow through the armature.
45
Electric motors are often classified according to the method of connecting the field coils and armature. Aircraft engine starter motors are generally of which type?
Series
46
A certain direct current series motor mounted within an aircraft draws more amperes during start than when it is running under its rated load. The most logical conciusion that may be drawn is
the condition is normal for this type of motor
47
What type of electric motor is generally used with 2 direct-cranking engine starter?
Direct current, series-wound motor
48
(Refer to Powerplant figure 5 on page 8-11.) The type of system depictea is capable of operating with
either battery or external power
49
When the starter switch to the aircraft gas turbıne engine starter-generator is energized and the engine fails to rotate, one of the probable causes would be the
starter solenoid is defective
50
What are two types of AC motors that are used to produce a relatively high torque?
Three-phase induction and capacitor start
51
Which of the following aircraft circuits does NOT contain a fuse/circuit breaker?
Starter circuit
52
As a general rule, starter brushes are replaced when they are approximately
one-haft their original length
53
When using an elecric starter motor, the current flow through it
is highest at the start of motor rotation
54
The purpose of ari under current relay in a starter-generator system is to
disconnect power from the starter-generator and ignition when sufficient engine speed is reached.
55
In a typical starter-generatot system, under which of the following starting circumstances may it be necessary to use the start stop switch?
Hung start
56
When using an electric starter motor, current usage
is highest at the start of motor rotation
57
The primary advantage of pneumatic (air turbine) starters over comparable electric starters for turbine engines is
high power-to-weight ratio
58
Inspection of pneumatic starters by maintenance technicians usually includes checking the
oil level and magnetic drain plug condition
59
Pneumatic starters are usually designed with what types of airflow impingemnent systems?
Radial inward fiow turbinc and axial-flow turbine.
60
A clicking sound heard at en gine coast-down in a pneumatic starter incorporating a sprag clutch ratchet assembly is an indication of
the pawls re-contacting and riding on the ratchet gear.
61
Air turbine starters are generally designed so that reduction gear distress or damage may be detected by
inspection of a magnetic chip detector
62
Airflow to the pneumatics starter from a ground unit is normally prevented from causing starter overspeed during engine start by
activation of a flyweight cutout switch
63
What is used to polish commutators or slip rings?
Very fine sandpaper
64
A satety feature usually employed in pneumatie arters that is used if the clutch does not release from the engine drive at the proper time during start is the
drive shaft shear point
65
A safety feature usually employed in pneumatic starters that is used to prevent the starter from reaching burst speed if inlet air does not terminate on schedule is the
stator nozzle design that chokes airflow and stabilizes turbine wheel speed
66
In the event a pneumatic start valve will not operate and the manual override must be used, the starter T handle must be closed at scheduled starter drop out because
the starter will overspeed at a given N2
67
One of the best indicators of reciprocating engine combustion chamber problems is
sparkplug condition
68
When a magneto is disassembled, keepers are usually placed across the poles of the rotating magneto reduce the loss of magnetism. These keepers are usually made of
cobalt steel
69
If the ignition switch is moved from BOTH to either LEFT or RIGHT during an engine round check, normal operation is usually indicated by a
slight drop in RPM
70
What tool is generally used to measure the crarkshaft rotation in degrees?
Timing disk
71
The greatest density of flux lines in the magnetic circuit of a rotating magnet-type magneto occurs when the magnet is in what position?
Full alignment with the field shor faces
72
Magneto breaker point opening relative to the position of the rotating magnet and distributor rotor (internal timing) can be set most accurately
during assembly of the magneto before installation on the engine.
73
The E-gap angle is usually de fined as the number of degrees between the neutral position of the rotating magnet and the position
where the contact points open
74
When timing a. magneto internaly, the aiignment of the timing marks indicates that the
magnets are in the E-gap position
75
When internally timing a magneto, the breaker points begin to open when thu rotating magnet is
a few degrees past the neutral position
76
What is the purpose of a safety gap in some magnetos?
To discharge the secondary coil’s voltage if an open occurs in the secondary circuit
77
When timing a magneto internally, the alignment of the timing marks indicates that the
magnets are in the E-gap position
78
When internally timing a magneto, the breaker points begin to open when the rotating magnet is
a few degrees past the neutral position
79
Why are bigh-tension ignition cables frequently routed from the distributors to the spark plugs in flexible metallic conduits?
To reduce the effect of the high-frequency electromagnetic waves emanated during operation.
80
What will be the results of increasing the gap of the breaker points in a magneto?
Advance the spark and decrease its intensity.
81
What is the radial location of the two north poles of a four-pole rotating magnet in a high-tension magneto?
180° apart.
82
When a "Shower of Sparks" ignition system is activated at an engine start, a spark plug fires
only while both the retard and advance breaker points are open.
83
Magneto timing drift is caused by erosion of the breaker points and
wear of the cam followers
84
What is the electrical location of the primary capacitor in a high-tension magneto?
In parallel with the breaker points
85
When the switch is off in a battery ignition system the primary circuit is
opened
86
As an aircraft engine's speed is increased, the voltage induced in the primary coil of the magneto
increase
87
In an aircraft ignition system, one of the functions of the capacitor is to
facilitate a more rapid collapse of the mag- netic field in the primary coil.
88
What components make up the magnetic system of a magneto?
Rotating magnet, the pole shoes, the pole shoe extensions, and the coil core.
89
Capacitance after firing in most modern spark plugs is reduced by the use of
a built-in resistor in each plug
90
How many secondary coils are required in a lowtension ignition system on an 18-cylinder engine?
36
91
A magneto ignition switch is connected
parallel to the breaker points
92
The spark is produced in a magneto ignition system when the breaker points are
beginning to open