Engine Instrument System
問題一覧
1
Front of the compressor and the rear of the turbine
2
5
3
It requires no external power source
4
A current generated by the temperature difference between dissimilar metal hot and cold junctions
5
The voltage output of a thermocouple system is determined by the temperature difference between the two ends of the thermocouple
6
Synchronous motors
7
Three
8
One more fuel nozzles are clogged
9
Higher than normal fuel flow indication
10
Indicate absolute pressure in the intake manifold
11
Immediately aft of the last turbine stage
12
Bootstrapping
13
Only No. 1 is true
14
Prevailing atmospheric pressure
15
Are designed for a specific installation and may not be altered
16
Obtain the best mixture setting for fuel efficiency
17
Entering the engine
18
Frequency
19
Fuel/air ratio being burned in the cylinders
20
Diaphragm or bellows
21
Dividing turbine outlet total pressure by engine inlet total pressure
22
2, 4, 5, 8
23
Engine thrust being produced
24
The three-phase ac generator
25
Generally, an accurate trend forecast may be made after an engine’s first oil sample analysis
26
Fuel mass-flow
27
Turbine damage or loss of turbine efficiency
28
One indicates engine RPM and the other main rotor RPM
29
Both No. 1 and No.2 is true
30
Noticeable shift in EPR
31
An electrical signal
32
Both No. 1 & No. 2 are true
33
The maximum limit for high transients such as starting
34
Turbine inlet temperature
35
Fuel flow meter
36
Galvanometer
37
Engine pressure ratio indicator
38
Monitor engine RPM during starting and to indicate overspeed conditions
39
An increased fuel flow indication on the gauge
40
Moves off-scale on the zero side of the meter
41
Either wheatstone bridge or ratio meter circuit
42
Chromel-alumel
43
Tachometer
44
Frequency
45
1 and 2
46
Prevailing atmospheric pressure
47
Bourdon tube
48
Fuel pressure
49
Fuel nozzles
50
Turbine inlet temperature
51
The hot junction is located at the cylinder and the cold junction is located at the instrument
52
Using aircraft electrical system power
53
Percent of engine RPM
54
Mean effective cylinder pressure
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. 1 ⭐️
Powerplant (Propellers) pt. 1 ⭐️
Marga · 60問 · 1年前Powerplant (Propellers) pt. 1 ⭐️
Powerplant (Propellers) pt. 1 ⭐️
60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
Front of the compressor and the rear of the turbine
2
5
3
It requires no external power source
4
A current generated by the temperature difference between dissimilar metal hot and cold junctions
5
The voltage output of a thermocouple system is determined by the temperature difference between the two ends of the thermocouple
6
Synchronous motors
7
Three
8
One more fuel nozzles are clogged
9
Higher than normal fuel flow indication
10
Indicate absolute pressure in the intake manifold
11
Immediately aft of the last turbine stage
12
Bootstrapping
13
Only No. 1 is true
14
Prevailing atmospheric pressure
15
Are designed for a specific installation and may not be altered
16
Obtain the best mixture setting for fuel efficiency
17
Entering the engine
18
Frequency
19
Fuel/air ratio being burned in the cylinders
20
Diaphragm or bellows
21
Dividing turbine outlet total pressure by engine inlet total pressure
22
2, 4, 5, 8
23
Engine thrust being produced
24
The three-phase ac generator
25
Generally, an accurate trend forecast may be made after an engine’s first oil sample analysis
26
Fuel mass-flow
27
Turbine damage or loss of turbine efficiency
28
One indicates engine RPM and the other main rotor RPM
29
Both No. 1 and No.2 is true
30
Noticeable shift in EPR
31
An electrical signal
32
Both No. 1 & No. 2 are true
33
The maximum limit for high transients such as starting
34
Turbine inlet temperature
35
Fuel flow meter
36
Galvanometer
37
Engine pressure ratio indicator
38
Monitor engine RPM during starting and to indicate overspeed conditions
39
An increased fuel flow indication on the gauge
40
Moves off-scale on the zero side of the meter
41
Either wheatstone bridge or ratio meter circuit
42
Chromel-alumel
43
Tachometer
44
Frequency
45
1 and 2
46
Prevailing atmospheric pressure
47
Bourdon tube
48
Fuel pressure
49
Fuel nozzles
50
Turbine inlet temperature
51
The hot junction is located at the cylinder and the cold junction is located at the instrument
52
Using aircraft electrical system power
53
Percent of engine RPM
54
Mean effective cylinder pressure