Aircraft Systems Flashcards

(22 cards)

1
Q

Function of fuel primer

A

used to draw duel from the tanks to vaporize fuel directly into the cylinders prior to starting the engine

avoid overpriming (cause fire)

Lock primer to precent excessively rich fuel-air mixture

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2
Q

Why are fuel tanks vented

A

To maintain atmospheric pressure inside the tank

allows fuel to expand with increases in temp without damaging the tank

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3
Q

Running a fuel tank completely dry may do what

A

May allow air to enter the fuel system and cause vapor lock - makes it difficult to restart engine

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4
Q

Ice formation in the aircraft fuel system results from

A

the presence of water in the fuel system

strain the sump during check

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5
Q

The exhaust systems serve as a heat source for

A

the cabin and carburetor

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6
Q

Risks of operating an aircraft with a defective exhaust heating system

A

CO poisoning, decreased engine performance, and increased potential for fire

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7
Q

Electrical energy stored in a battery provides a source of electrical power for

A

Starting the engine and a limited supply of electrical power for use in the event the alternator fails

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8
Q

How does an alternator work

A

Converts mechanical energy (the prop/engine) into electrical energy

powers electrical equipment and battery

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9
Q

4 stroke process

A
  1. Intake stroke
  2. Compression Stroke
  3. Power Stroke
  4. Exhaust Stroke
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10
Q

Intake Stroke

A

piston starts the downward travel. When this happens the intake valve opens and the fuel-air mixture is drawn into the cylinder.

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11
Q

Compression Stroke

A

Intake Valve closes and the piston starts moving back to the top of the cylinder

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12
Q

Power stroke

A

Fuel-air mixture is ignited - causes pressure increase in the cylinder and forces the pitston down and creates the power that turns the crankshaft

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13
Q

Exhaust stroke

A

Used to purge the cylinder of burned gases

begins when the exhaust valve opens and piston starts to move toward cylinder head again

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14
Q

Reason for twisted propeller blades

A

Difference in the actual speed of the various portions of the blade

tip travels faster than the base

the twist creates a uniform lift

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15
Q

Pros of fixed pitch prop

A

Low-weight, simple, low cost

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16
Q

Cons of fixed pitch prop

A

Fixed pitch achieves the best efficiency only at a given combination of airpseed and rpm

Fixed pitch is not optimal for cruise nor climb so performance suffers

17
Q

Throttle controls the

A

fuel-air flow to the engine

18
Q

As altitude changes the position of the throttle must be ____ to maintain ____

A

changed to maintain same rpm

as altitude is increased the throttle must be opened further to indicate the same rpm as a lower altitude.

19
Q

A constant-speed propeller is more efficient than other propellers because

A

it allows the selection of the most efficient engine rpm for the given conditions

20
Q

What does the induction system do

A

Brings air from the outside, mixes it with fuel, and delivers the fuel-air mixture to the cylinder where combustion occurs

21
Q

Two types of induction systems are common in small aircraft

A
  1. Carburetor system
  2. Fuel injection system