AMT 287 Exam 1 Pt 2

0.0(0)
studied byStudied by 1 person
learnLearn
examPractice Test
spaced repetitionSpaced Repetition
heart puzzleMatch
flashcardsFlashcards
Card Sorting

1/325

flashcard set

Earn XP

Description and Tags

Aviation

Study Analytics
Name
Mastery
Learn
Test
Matching
Spaced

No study sessions yet.

326 Terms

1
New cards
Neglecting drag, how much power is needed to cause a 2500 pound airplane to climb at 1000 R2/mig

2
New cards
Express your answer in ft-lbs/min, watts and HP.
2500 lb * 1000 ft\= 2,500,000 ft-lb/min
3
New cards
(1 HP/33,000 ft-lb/min) * (2,500,000 ft-lb/min) \= 75.76 HP

4
New cards
(746 watts/ 1 HP)*(75.7 HP) \= 56,515.115 watts

5
New cards
Three minutes after take-off how much potential energy will the aircraft of Question \#1 possess (neglet remaining fuel in the tanks)?
2,500 lb * 1000 ft.min * 3 min \= 7,500,000 ft-lb
6
New cards
PE \= 7,500,000 ft-lb

7
New cards
solid, liquid, gas, plasma
states of matter
8
New cards
gasses fill their containers completely and liquids do not; gasses are highly compressible and liquids are not compressible
difference between gasses and liquids
9
New cards
fluid
a substance which changes its shape easily and takes the shape of the container
10
New cards
Show the value of temperature of the standard day atmosphere at sea level in four different units of measure.
1) 59˚ F
11
New cards
2) 15˚ C

12
New cards
3) 298.18 ˚K

13
New cards
4) 518.67˚ R

14
New cards
3rd class lever
What kind of a lever is your forearm?
15
New cards
3rd Class lever
What kind of a lever is a hydraulic wobble pump handle?
16
New cards
Inertia is the resistance offered by a body to the motion whereas momentum is the tendency of a body to continue moving.
What are the differences between inertia and momentum?
17
New cards
air
principal fluid for propulsion
18
New cards
thrust
the force which propels the aircraft
19
New cards
thrust horsepower (THP)
calculated by multiplying thrust by by aircraft speed (in MPH) divided by by 375 mi-lbs per hr or 325 kt-lbs per hr
20
New cards
How much thrust is being used by an atreraft that is using 100 THP to go 100 MPH?
X(100mph)/375 \= 100 THP
21
New cards
X\= 375 lbs of thrust

22
New cards
How much more or less thrust than the airplane of Question \#5 is another aircraft using that is using 100 THP, just like the airplane of Question \#5, but is going 90 KTS?
X(103.6)/375 \= 100 THP
23
New cards
X\=632.0 lbs of thrust

24
New cards
13.0 lbs less than Q \#5

25
New cards
The advantages of a hydraulic valve filter or tappets is that it automatically keep the value at 0, trapping the oil in the pressure chamber. Then, a predetermined leakage occurs between the plunger and cylinder, compensating for any expansion or contraction in the valve train.
What are the advantages of a hydraulic lifter?
26
New cards
cylinder head and cylinder barrel
parts in a typical cylinder assembly
27
New cards
cylinder head
provides a place for the combustion of the fuel/air mixture and gives the cylinder more heat conductivity for adequate cooling; made out of aluminum alloy
28
New cards
cylinder barrel
holds the piston; must be light and withstand high temperatures; made out of steel alloy
29
New cards
nitriding
steel of the cylinder barrel soaks up nitrogen for the gas which forms iron nitrides on the exposed surface
30
New cards
piston
act as a moving wall within the combustion chamber; draws in (down) and compresses (up) fuel/air mixture
31
New cards
dynamic damper
a pendulum fastened to the crankshaft that reduces vibration during engine operation
32
New cards
Chemical energy into heat energy into mechanical energy.
What three energy forms does the reciprocating engine utilize or convert?
33
New cards
ft-lb per min/33,000 or ft-lb per sec/550
Horsepower (HP)
34
New cards
brake horsepower (BHP)
work per revolution
35
New cards
On a short field takeoff, what can the pilot do to reduce FHP and thus increase BHP and THP?
Pull the alternator field circuit breaker, or open the alternator switch, and let the battery handle the electrical system until you've cleared.
36
New cards
reduce friction, act as a cushion in between metal parts, absorb heat, reduces abrasive wear, and cleans the engine
functions of lubricating oil
37
New cards
The oil selected must be light enough to circulate freely but heavy enough to provide the proper oil film at various temperatures.
Why is viscosity important when selecting a lubricant?
38
New cards
What is the relationship between aviation grade numbers and SAE numbers for lubricating oil?
The Society of Automotive Engineers (SAE) rates and divides the oils into specific groups that go hand-in-hand in aviation grade numbers.
39
New cards
Under what conditions would a dry sump system be advantageous, over a wet sump?
A dry sump would be better for radial engines because oil can't be carried inside the engine itself and wet sump systems are self-contained unit.
40
New cards
Some advantages of wet sump lubrication systems is that it is a complete system that requires no external parts, no second pump is required, and it can be operated in colder temperatures.
What are the advantages of a wet sump system, compared to the dry sump?
41
New cards
Displacement pump and mechanical positive.
What type of pump is the engine oil pump?
42
New cards
bypass valve
allows oil flow if the oil filter becomes plugged
43
New cards
relief valve
creates pressure in the system to compensate for wear on bearings or thinning out oil
44
New cards
The cylinder walls are lubricated by oil sprayed from the crankshaft and crankpin bearings.
How are the cylinder walls lubricated in a typical opposed aircraft engine?
45
New cards
The cowlings are designed to force air over the cylinder cooling fins.
How does the cowling contribute to engine cooling?
46
New cards
augmenter tube
provides additional cooling, especially for low speed, high power conditions
47
New cards
How does opening cowl flaps affect engine cooling? Cabin cooling?
For engine cooling, cowl flaps (when opened) increase cooling airflow over the engine and through the oil cooler. For cabin cooling, hot and cold airflow is reduced due to air pressure inside and in front of the cowling when cowl flaps are open.
48
New cards
Rotational velocity
w \= 2pi(rpm)/60s \= unit ft/s
49
New cards
ft/s x 0.592 KTS \= unit KTS

50
New cards
KTS x 0.0015 Ma \= unit Ma

51
New cards
tan \= forward velocity/linear velocity

52
New cards
tan-1 to get degrees

53
New cards
near the tip to provide equal thrust along the propeller blade
where is the lowest blade angle!
54
New cards
With a fixed RPM, does propeller blade angle of attack increase or decrease as airspeed increases?
The angle of attack decreases while the blade angle increases.
55
New cards
centrifugal twisting force
force that tends to twist the blade to decrease propeller angle
56
New cards
Aerodynamic twisting force
force that tends to twist the blade to increase propeller blade angle
57
New cards
1) propeller position for hand starting

2) intake/exhaust valve opening minimized

3) less attractive for birds to perch on
What are the advantages of leaving the propeller in the 10/4 o clock position?
58
New cards
static balancing
propeller suspended by a drawstring
59
New cards
dynamic balancing
an electrical machine with vibration analysis of the aircraft
60
New cards
ground-adjustable propeller
operates as a fixed-pitch propeller; only can be changed on ground
61
New cards
two position propeller
permits a change of blade pitch while the prop is rotating
62
New cards
What components in the governor oppose the force of the speeder spring?
The flight weight and the pilot valve.
63
New cards
centrifugal force
force used to feather a propeller
64
New cards
carburetor venturi
provides the low pressure at the discharge nozzle of a float carburetor
65
New cards
Main metering jet
limits the maximum amount of fuel which can flow from the float bowl for any given pressure differential
66
New cards
1) to improve fuel vaporization

2) to provide a more even mixture over a wide range of air flows

3) to decrease the size of the fuel metering force needed which decreases the amount of restriction necessary at the Venturi
functions of an air bleed on a float carburetor
67
New cards

1. fuel evaporation
2. decreasing air pressure in the venturi
Why are float carburetors more susceptible to icing?
68
New cards
When should carburetor heat be used on the ground (several answers)?
When engine starting in high or low temperatures and when shutting off the engine which prevents cold air from passing through
69
New cards
What is the purpose of the acceleration system on an aircraft carburetor?
temporarily enriches the mixture when the throttle is suddenly opening
70
New cards
Why is a power enrichment system also called an economizer system?
Because they allow the engine to operate with a relatively lean, economical mixture for all conditions besides full power
71
New cards
it will be leaned when the air bleed is restricted
Is the fuel-air mixture enriched or leaned when the main air bleed is restricted?
72
New cards
richen
Does application of carburetor heat richen or lean the mixture?
73
New cards
a) less dense air decreases the amount of oxygen getting into the cylinder, thus increasing the fuel/air ratio

74
New cards
b) higher air temperature will do a better job of vaporizing the fuel, thus increasing the fuel/air ratio

75
New cards

1. not susceptible to icing
2. even fuel/air mixture distribution
3. not critical at high density altitudes
4. not affected by gravity
advantages of the pressure carburetor over the float carburetor
76
New cards
less susceptible to icing, but can still have ice formations
disadvantages of the pressure carburetor
77
New cards
air pressure
What does the fuel flowmeter actually measure on the fuel injection systems discussed in this chapter?
78
New cards
air bleed
minimizes fuel bleeding in fuel injection systems
79
New cards
What are the functions of the spider?
1) distributes the fuel evenly to all of the cylinders
80
New cards
2) provides a positive shut off when the mixture control is placed in the idle cut off position

81
New cards
not susceptible to icing and has more power than carbureted systems
What are the advantages of a fuel injection system, as a fuel metering system?
82
New cards
possible vapor lock in the fuel lines make it difficult to start the engine
What are the disadvantages of a fuel injection system, as a fuel metering system?
83
New cards
True
T/F. An in-line engine usually has an even number of cylinders. This engine may be either liquid cooled, or air cooled and has only one crankshaft, either above or below the cylinders.
84
New cards
T/F. The opposed type of engine has two banks of cylinders opposite each

85
New cards
other with a crankshaft in the center. This type of engine may be liquid cooled or

86
New cards
air-cooled but the air-cooled version is used predominantly in aviation today.
True
87
New cards
T/F Radial engines consist of a row or rows of cylinders arranged radially about

88
New cards
a central crankcase. The number of cylinders comprising a row may be three, five

89
New cards
or seven or nine, but it is always and odd number.
True
90
New cards
compression rings
prevent the escape of gas past the piston during engine operation
91
New cards
oil control ring location
placed in grooves immediately below the compression rings and above the piston pin bore
92
New cards
oil control rings
regulate the thickness of oil film on the cylinder wall
93
New cards
oil scraper ring
usually has a beveled face and is installed in the groove on the bottom of the piston skirt
94
New cards
lower
intake valves operate at _____ temperatures than the exhaust valves
95
New cards
1/2
The camshaft always rotates at _____ the crankshaft speed in four stroke engines
96
New cards
plain, ball, roller
three types of bearings commonly found in engines
97
New cards
the speed of sound; decreases
when the propeller tips approach ____, the efficiency of the propeller _____ rapidly
98
New cards
tapered, splined, flanged
three major types of propeller shafts
99
New cards
single-throw, double-throw, four-throw, six-throw
four principle types of crankshafts
100
New cards
bearing
any surface that supports or is supported by another surface.