Reciprocating Engines pt.2 ⭐️
問題一覧
1
Decreased engine power at a constant RPM and manifold pressure.
2
The valves will open late and close early.
3
A mixture leaner than a manual lean mixture of .060
4
To enable the engine RPM to be increased with an accompanying increase in power and allow the propeller to remain at a lower, more efficient RPM.
5
Master rod bearing (radial engine)
6
Exhaust and intake
7
manifold pressure is reduced with the throttle control before the RPM is reduced with the propeller control.
8
Lower than normal static RPM, full throttle operation
9
nitriding.
10
The power impulses are spaced closer together.
11
Deep-groove ball
12
Low oil temperatures
13
push rod replacement
14
controlling air flow through the oil cooler
15
Lean mixture
16
To determine satisfactory performance
17
Critical altitude
18
turn the propeller by hand three to four revolutions in the normal direction of rotation to check for liquid lock.
19
.005 inch
20
both the piston and the small end of the connecting rod
21
water-mixed degreaser residues may cause engine oil contamination in the overhauled engine.
22
At the end of the exhaust stroke and the beginning of the intake stroke
23
Moveable counterweights serve to reduce the torsional vibrations in an aircraft reciprocating engine.
24
7:1
25
The valves will not seat positively during start and engine warm up
26
the cause should be identified and corrected before the aircraft is released for flight
27
intake, compression, ignition, power, exhaust.
28
373°
29
Cylinder compression check.
30
an excessively lean mixture.
31
excessively enriching the fuel/air mixture.
32
Use of fuel with too low an octane rating.
33
three
34
provide a better fit at operating temperatures
35
Reduced valve operating temperatures.
36
greater
37
some of the soap will become impregnated in the surface of the material and subsequently cause engine oil contamination and foaming.
38
245°
39
Timing disk
40
By placing the rings in the cylinder and measuring the end-gap with a feeler gauge.
41
During normal operation
42
cylinder volume with piston at bottom dead center and at top dead center
43
just after top center at the beginning of the power stroke.
44
leaking oil dilution valve
45
Oil starvation of bearings and other parts.
46
Reduce the manifold pressure, then the RPM.
47
Reduced valve overlap period.
48
backfiring into the induction system.
49
neither No. 1 nor No. 2 is true.
50
Top dead center
51
with a contour or radius gauge
52
brake horsepower
53
at maximum velocity 90° after TDC
54
low oil supply
55
To prevent valves from falling into the combustion chamber.
56
engines lubrication system is probably operating normally.
57
both No. 1 and No. 2 are true
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. 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
Decreased engine power at a constant RPM and manifold pressure.
2
The valves will open late and close early.
3
A mixture leaner than a manual lean mixture of .060
4
To enable the engine RPM to be increased with an accompanying increase in power and allow the propeller to remain at a lower, more efficient RPM.
5
Master rod bearing (radial engine)
6
Exhaust and intake
7
manifold pressure is reduced with the throttle control before the RPM is reduced with the propeller control.
8
Lower than normal static RPM, full throttle operation
9
nitriding.
10
The power impulses are spaced closer together.
11
Deep-groove ball
12
Low oil temperatures
13
push rod replacement
14
controlling air flow through the oil cooler
15
Lean mixture
16
To determine satisfactory performance
17
Critical altitude
18
turn the propeller by hand three to four revolutions in the normal direction of rotation to check for liquid lock.
19
.005 inch
20
both the piston and the small end of the connecting rod
21
water-mixed degreaser residues may cause engine oil contamination in the overhauled engine.
22
At the end of the exhaust stroke and the beginning of the intake stroke
23
Moveable counterweights serve to reduce the torsional vibrations in an aircraft reciprocating engine.
24
7:1
25
The valves will not seat positively during start and engine warm up
26
the cause should be identified and corrected before the aircraft is released for flight
27
intake, compression, ignition, power, exhaust.
28
373°
29
Cylinder compression check.
30
an excessively lean mixture.
31
excessively enriching the fuel/air mixture.
32
Use of fuel with too low an octane rating.
33
three
34
provide a better fit at operating temperatures
35
Reduced valve operating temperatures.
36
greater
37
some of the soap will become impregnated in the surface of the material and subsequently cause engine oil contamination and foaming.
38
245°
39
Timing disk
40
By placing the rings in the cylinder and measuring the end-gap with a feeler gauge.
41
During normal operation
42
cylinder volume with piston at bottom dead center and at top dead center
43
just after top center at the beginning of the power stroke.
44
leaking oil dilution valve
45
Oil starvation of bearings and other parts.
46
Reduce the manifold pressure, then the RPM.
47
Reduced valve overlap period.
48
backfiring into the induction system.
49
neither No. 1 nor No. 2 is true.
50
Top dead center
51
with a contour or radius gauge
52
brake horsepower
53
at maximum velocity 90° after TDC
54
low oil supply
55
To prevent valves from falling into the combustion chamber.
56
engines lubrication system is probably operating normally.
57
both No. 1 and No. 2 are true