15.12 Air Systems (Level 1, 2 Questions) Flashcards

(46 cards)

1
Q

Why is cooling provided to internal combustion engines?
A. To reduce noise
B. Due to intense heat generated during combustion
C. To improve airflow

A

B. Due to intense heat generated during combustion

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2
Q

Without cooling air, what could the internal engine temperature reach?
A. 1150°C
B. 800°C
C. 2200°C

A

C. 2200°C

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3
Q

With cooling air, what is the maintained internal engine temperature range?
A. 400–600°C
B. 800–1150°C
C. 1500–1800°C

A

B. 800–1150°C

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4
Q

Where is the hottest section of the turbine engine?
A. Around the turbines
B. Near the air intake
C. Around the fan case

A

A. Around the turbines

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5
Q

What function does secondary air perform?
A. Powers the fan
B. Increases fuel flow
C. Cools the combustion chamber liners

A

C. Cools the combustion chamber liners

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6
Q

What moves over the surfaces of the combustion chamber liners for cooling?
A. Oil
B. Thin fast-moving film of air
C. Water vapor

A

B. Thin fast-moving film of air

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7
Q

What type of cooling do some engines use for bearings?
A. Water and oil
B. Air and oil
C. Steam and air

A

B. Air and oil

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8
Q

Where is internal cooling air bled from?
A. Fan blades
B. Turbine shaft
C. Compressor section

A

C. Compressor section

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9
Q

How is air vented to or from the engine removed?
A. Manually
B. Using exhaust stream assistance
C. Through the fan intake

A

B. Using exhaust stream assistance

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10
Q

What isolates the primary zones of turbine engines?
A. Electrical panels
B. Plastic dividers
C. Fireproof bulkhead or seals

A

C. Fireproof bulkhead or seals

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11
Q

Which is not a primary engine zone?
A. Fan case compartment
B. Cargo hold
C. Core engine compartment

A

B. Cargo hold

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12
Q

How is Zone 1 vented?
A. Using exhaust stream
B. With ram air through an inlet and vented through right fan cowling
C. Through the turbine exhaust

A

B. With ram air through an inlet and vented through right fan cowling

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13
Q

How is Zone 2 cooled and vented?
A. Cooled by ram air and vented to the intake
B. Cooled by core air and vented downward
C. Cooled by fan air and exhausted into fan stream

A

C. Cooled by fan air and exhausted into fan stream

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14
Q

What does Zone 3 contain?
A. Wing flaps
B. Fuel and oil lines
C. Passenger seats

A

B. Fuel and oil lines

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15
Q

Which engine sections use cooling air?
A. Only the fan
B. Only the combustion chamber
C. Compressor, combustion, and turbine sections

A

C. Compressor, combustion, and turbine sections

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16
Q

What can ice do to a turbine engine compressor?
A. Increase airflow
B. Disrupt the compressor and reduce engine efficiency
C. Improve fuel efficiency

A

B. Disrupt the compressor and reduce engine efficiency

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17
Q

What serious damage can ice cause if it breaks off?
A. It can crack the fuselage
B. It can freeze the cockpit windows
C. It can damage engine blades

A

C. It can damage engine blades

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18
Q

What is generally fitted to engine inlets to prevent ice formation?
A. Dehumidifier system
B. Anti-ice system
C. Fire suppression system

A

B. Anti-ice system

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19
Q

At what temperature can ice form in the inlet due to high inlet velocities?
A. 20°C
B. 15°C
C. 5°C

20
Q

Why can ice form in the inlet at 5°C?
A. Due to cold fuel temperature
B. Because of the chilling effect of high inlet velocities
C. From high exhaust pressure

A

B. Because of the chilling effect of high inlet velocities

21
Q

How can anti-icing systems be controlled?
A. Only manually
B. Only automatically
C. Automatically or manually

A

C. Automatically or manually

22
Q

What part of the engine inlet does the anti-ice system heat?
A. Inner casing
B. Fan blades
C. Lip of the inlet

A

C. Lip of the inlet

23
Q

Where does the heated air exit after warming the lip?
A. Through the wing
B. Through a grill on the nose cowl
C. Through the exhaust nozzle

A

B. Through a grill on the nose cowl

24
Q

What are the subsystems of internal engine cooling divided into?
A. Compressor, combustion chamber, fuel tank
B. Compressor, combustion chamber, turbine disc, NGV and blade, accessory section
C. Exhaust nozzle, fan case, intake duct

A

B. Compressor, combustion chamber, turbine disc, NGV and blade, accessory section

25
What is the typical temperature at the rear stages of the compressor? A. 100–200°C B. 200–300°C C. 350–400°C
C. 350–400°C
26
Where does compressor cooling air come from? A. Combustion chamber B. Intermediate compressor stage C. Exhaust nozzle
B. Intermediate compressor stage
27
What is the combustion chamber made of? A. A solid cylinder B. An outer casing with a perforated inner liner C. A steel block with drilled holes
B. An outer casing with a perforated inner liner
28
What percentage of air enters the combustion liner as primary air? A. 20–30% B. 50–60% C. 70–80%
A. 20–30%
29
What is the role of secondary airflow in the combustion chamber? A. Increases combustion speed B. Heats the liner C. Prevents flames from contacting the liner
C. Prevents flames from contacting the liner
30
What does cooling air in the combustor create on the liner? A. Vibration B. A thermal barrier film C. A solid carbon layer
B. A thermal barrier film
31
Why is turbine cooling key to engine performance? A. To slow down fuel usage B. To increase exhaust noise C. It allows operation 300–400°C above metal alloy limits
C. It allows operation 300–400°C above metal alloy limits
32
What method is commonly used for turbine disc cooling? A. Coolant fluid B. Engine bleed air C. Ice packs
B. Engine bleed air
33
How are Nozzle Guide Vanes (NGV) and turbine blades cooled? A. Fuel mist B. Water injection C. Compressor air
C. Compressor air
34
Why might engine accessories need their own cooling system? A. They are far from the engine B. They produce considerable heat C. They require high pressure
B. They produce considerable heat
35
What is used to cool oil-cooled generators? A. Radiators B. Water jackets C. Air-cooled oil cooler
C. Air-cooled oil cooler
36
What is LP compressor bleed air used for in the engine? A. Fuel injection B. Cooling the turbine blades C. Sealing the engine bearing chambers
C. Sealing the engine bearing chambers
37
What does the pressurised air act on in the bearing chambers? A. Turbine blades and stators B. Air seals and oil seals C. Fan blades and rotors
B. Air seals and oil seals
38
What is the purpose of the pressurised air acting on the seals? A. To increase fuel efficiency B. To provide thrust C. To prevent oil from escaping the bearing chamber
C. To prevent oil from escaping the bearing chamber
39
Where does the air that enters the bearing compartments eventually go? A. Into the combustion chamber B. Vents overboard through the hollow rotor shaft C. Into the turbine casing
B. Vents overboard through the hollow rotor shaft
40
What is a secondary function of the compressor? A. Reducing engine weight B. Supplying air to aircraft systems C. Increasing fuel pressure
B. Supplying air to aircraft systems
41
From which part of the compressor is air often bled? A. Middle pressure stage B. First stage C. Final or highest pressure stage
C. Final or highest pressure stage
42
What are the areas below the engine cowlings divided into? A. Intake and exhaust compartments B. Fan and core compartments C. Compressor and turbine compartments
B. Fan and core compartments
43
What does the external cooling system prevent from building up? A. Fuel in the combustor B. Flammable vapours in engine compartments C. Carbon in exhaust ducts
B. Flammable vapours in engine compartments
44
What separates the fan and core compartments? A. Exhaust ducts B. Heat exchangers C. Bulkheads and seals
C. Bulkheads and seals
45
When is there only positive ventilation of the core compartment? A. When the engine is off B. During maintenance C. When the engine operates
C. When the engine operates
46
What can happen after engine shutdown due to uneven expansion? A. Fan blade crack B. Compressor surge C. Bowed rotor
C. Bowed rotor