Powerplant (Propellers) pt. 1 ⭐️
問題一覧
1
Governor flyweights.
2
make the location of cracks readily apparent.
3
remain in the full LOW PITCH position.
4
position the propeller hub on the splined shaft.
5
Aerodynamic twisting force.
6
filing with a riffle file.
7
maintain the RPM, increase the blade angle, and maintain a low angle of attack.
8
Inspect the bolts for tightness after the first flight and again after the first 25 hours of flying.
9
High pitch directly to feather position.
10
Solder
11
change engine horsepower to thrust.
12
Rheostat
13
correct blade contouring and angle setting.
14
Measuring blade angle.
15
Centrifugal force acting on the counterweights.
16
is smallest at the tip.
17
very fine sandpaper
18
Centrifugal force
19
The plane of rotation
20
feathered or in the most critical pitch configuration.
21
To control engine RPM and reduce vibration.
22
Thrust-bending force.
23
Vertical
24
Fresh water
25
Cold straightening only.
26
reduce the pitch angle.
27
Relative airstream
28
increase, engine manifold pressure will increase, and engine RPM will decrease.
29
A major repair
30
the positions of the tips of the propeller blades relative to each other.
31
the propeller can be installed in only one position.
32
eliminate the drag created by a wind milling propeller when an engine fails in flight.
33
To limit the maximum engine speed during takeoff.
34
hub centerline
35
By changing the load tension against the flyweights ¡n the governor.
36
an appropriately rated repair station or the manufacturer.
37
washing off with solvent.
38
antifriction and plasticity characteristics of grease.
39
is used to produce zero or negative thrust.
40
Torque-bending force
41
propeller governors
42
Transverse cracks of any size.
43
Compression of the speeder spring is changed.
44
eliminate stress concentration points.
45
the pitch-changing oil.
46
In the counterweight assembly
47
reduced to conform with the shortened blade.
48
fatigue failure.
49
By magnetic particle inspection.
50
By allowing oil to escape from the propeller hub thus driving the blades to a increased blade angle.
51
LOW PITCH, high RPM position.
52
High RPM
53
oil pressure
54
direct oil from the engine oil system to the propeller cylinder.
55
adjusting the phase angle between the propellers on an aircraft’s engines.
56
feeling the sequence of boot heating and have an assistant observe the loadmeter indications.
57
To support the propeller on the balance knives.
58
parallel to the length of the blade.
59
chord of the blade
60
By centrifugal force.
Airlaw (PCAR, AFCAR, Airframe check & Publications) (2)
Airlaw (PCAR, AFCAR, Airframe check & Publications) (2)
Marga · 47問 · 1年前Airlaw (PCAR, AFCAR, Airframe check & Publications) (2)
Airlaw (PCAR, AFCAR, Airframe check & Publications) (2)
47問 • 1年前Reciprocating Engines pt.1 ⭐️
Reciprocating Engines pt.1 ⭐️
Marga · 50問 · 1年前Reciprocating Engines pt.1 ⭐️
Reciprocating Engines pt.1 ⭐️
50問 • 1年前Reciprocating Engines pt.2 ⭐️
Reciprocating Engines pt.2 ⭐️
Marga · 57問 · 1年前Reciprocating Engines pt.2 ⭐️
Reciprocating Engines pt.2 ⭐️
57問 • 1年前Induction and Airflow System
Induction and Airflow System
Marga · 42問 · 1年前Induction and Airflow System
Induction and Airflow System
42問 • 1年前Engine Instrument System
Engine Instrument System
Marga · 54問 · 1年前Engine Instrument System
Engine Instrument System
54問 • 1年前Fuel Metering System
Fuel Metering System
Marga · 45問 · 1年前Fuel Metering System
Fuel Metering System
45問 • 1年前Ignition starting system pt. 1 ⭐️
Ignition starting system pt. 1 ⭐️
Marga · 50問 · 1年前Ignition starting system pt. 1 ⭐️
Ignition starting system pt. 1 ⭐️
50問 • 1年前Ignition starting system pt. 2 ⭐️
Ignition starting system pt. 2 ⭐️
Marga · 78問 · 1年前Ignition starting system pt. 2 ⭐️
Ignition starting system pt. 2 ⭐️
78問 • 1年前Turbine Engines pt. 1 ⭐️
Turbine Engines pt. 1 ⭐️
Marga · 60問 · 1年前Turbine Engines pt. 1 ⭐️
Turbine Engines pt. 1 ⭐️
60問 • 1年前Turbine Engines pt. 2 ⭐️
Turbine Engines pt. 2 ⭐️
Marga · 59問 · 1年前Turbine Engines pt. 2 ⭐️
Turbine Engines pt. 2 ⭐️
59問 • 1年前Powerplant (Propellers) pt. 2 ⭐️
Powerplant (Propellers) pt. 2 ⭐️
Marga · 57問 · 1年前Powerplant (Propellers) pt. 2 ⭐️
Powerplant (Propellers) pt. 2 ⭐️
57問 • 1年前Powerplant (Auxiliary power unit)
Powerplant (Auxiliary power unit)
Marga · 10問 · 1年前Powerplant (Auxiliary power unit)
Powerplant (Auxiliary power unit)
10問 • 1年前Engine Lubrication ⭐️
Engine Lubrication ⭐️
Marga · 93問 · 1年前Engine Lubrication ⭐️
Engine Lubrication ⭐️
93問 • 1年前Assembly and Rigging ⭐️
Assembly and Rigging ⭐️
Marga · 78問 · 1年前Assembly and Rigging ⭐️
Assembly and Rigging ⭐️
78問 • 1年前問題一覧
1
Governor flyweights.
2
make the location of cracks readily apparent.
3
remain in the full LOW PITCH position.
4
position the propeller hub on the splined shaft.
5
Aerodynamic twisting force.
6
filing with a riffle file.
7
maintain the RPM, increase the blade angle, and maintain a low angle of attack.
8
Inspect the bolts for tightness after the first flight and again after the first 25 hours of flying.
9
High pitch directly to feather position.
10
Solder
11
change engine horsepower to thrust.
12
Rheostat
13
correct blade contouring and angle setting.
14
Measuring blade angle.
15
Centrifugal force acting on the counterweights.
16
is smallest at the tip.
17
very fine sandpaper
18
Centrifugal force
19
The plane of rotation
20
feathered or in the most critical pitch configuration.
21
To control engine RPM and reduce vibration.
22
Thrust-bending force.
23
Vertical
24
Fresh water
25
Cold straightening only.
26
reduce the pitch angle.
27
Relative airstream
28
increase, engine manifold pressure will increase, and engine RPM will decrease.
29
A major repair
30
the positions of the tips of the propeller blades relative to each other.
31
the propeller can be installed in only one position.
32
eliminate the drag created by a wind milling propeller when an engine fails in flight.
33
To limit the maximum engine speed during takeoff.
34
hub centerline
35
By changing the load tension against the flyweights ¡n the governor.
36
an appropriately rated repair station or the manufacturer.
37
washing off with solvent.
38
antifriction and plasticity characteristics of grease.
39
is used to produce zero or negative thrust.
40
Torque-bending force
41
propeller governors
42
Transverse cracks of any size.
43
Compression of the speeder spring is changed.
44
eliminate stress concentration points.
45
the pitch-changing oil.
46
In the counterweight assembly
47
reduced to conform with the shortened blade.
48
fatigue failure.
49
By magnetic particle inspection.
50
By allowing oil to escape from the propeller hub thus driving the blades to a increased blade angle.
51
LOW PITCH, high RPM position.
52
High RPM
53
oil pressure
54
direct oil from the engine oil system to the propeller cylinder.
55
adjusting the phase angle between the propellers on an aircraft’s engines.
56
feeling the sequence of boot heating and have an assistant observe the loadmeter indications.
57
To support the propeller on the balance knives.
58
parallel to the length of the blade.
59
chord of the blade
60
By centrifugal force.