Day 11 Progress Check Flashcards

1
Q

How does an Engine Air-Inlet Vortex Destroyer solve the problem of suction vortices during ground operations?

A

Bleed air is used to destroy the jet stream

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2
Q

What is a disadvantage of acoustic linings?

A

Increased weight

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3
Q

What is the function of flaps in noise suppression?

A

Reduce exhaust area, increasing frequency

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4
Q

Why is the exhaust section of an aircraft engine vulnerable to cracking?

A

Repeated thermal cycling

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5
Q

What does a hot spot in the exhaust section of an engine indicate?

A

Faulty fuel nozzle

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6
Q

Where are acoustic linings located in an aircraft engine?

A

Between engine and cowling

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7
Q

What is the main solution to the problem of harmful Nitrogen Oxide (NOX) emissions in turbine engines?

A

Increased combustion efficiency

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8
Q

What is the primary motivation for the need for noise reduction in aircraft?

A

Operating near population centers

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9
Q

What component is responsible for converting acoustic energy into heat energy in the noise suppression system?

A

Acoustic linings

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10
Q

What is the purpose of noise suppressors in aircraft engines?

A

Augment the aircraft noise profile

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11
Q

How do low-frequency noises generated by jet efflux propagate compared to high-frequency noises?

A

Travel the farthest

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12
Q

How does the swirling motion in the TAPS combustor contribute to emission reduction?

A

Ensures a lean mixture of fuel and air

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13
Q

What does the Twin Annular, Pre-mixing Swirler (TAPS) combustor source air from?

A

High-pressure compressor

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14
Q

What is the purpose of the landing gear safety switch in the Engine Air-Inlet Vortex Destroyer?

A

Closes the valve on lift-off

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15
Q

How does the corrugated-type noise suppressor operate?

A

Breaking up the exhaust stream

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