Chapter 7: Aircraft Systems Flashcards

1
Q

Name 2 primary reciprocating engine designs.

A

spark ignition and compression ignition

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2
Q

Why do opposed-type engines have higher power-to-weight ratios ?

A

1) comparatively small, lightweight crankcase. 2) cylinder arrangement reduces the engines frontal area and allows streamlined installation that minimizes drag.

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3
Q

Why do two-stroke engines typically have higher power-to-weight ratios than four-stroke engines ?

A

there is a power stroke on each revolution of crankshaft.

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4
Q

Name the main parts of spark ignition reciprocating engine.

A

cylinders (valves, plugs, pistons), crankcase (crankshaft and connection rods), accessory housing (magnetos).

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5
Q

Why is a propeller twisted ?

A

To produce uniform thrust. Blade travels less near hub than tip.

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6
Q

Why is a fixed-pitch propeller used ?

A

Low-weight, simplicity, and low cost

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7
Q

List 2 types of fixed-pitch propellers.

A

Climb and Cruise.

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8
Q

Describe characteristics of a climb propeller.

A

Has a lower pitch, therefor less drag resulting in higher RPM and more horsepower capability which increases performance during takeoffs and climbs but decreases performance during cruising flight.

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9
Q

Describe the characteristics of a cruise propeller.

A

Has a higher pitch, therefore more drag, resulting in lower RPM and less horsepower capability, which decreases performance during takeoffs and climbs but increases efficiency during cruising flight.

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10
Q

What instrument indicates engine power on a fixed-pitch propeller ?

A

Tachometer

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11
Q

Why might the tach show the correct power output as the altitude increases ?

A

Power output depends on air density. Less air reduces power. As altitude increases, the throttle must be opened to maintain RPM.

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12
Q

Describe the characteristics of a constant-speed propeller.

A

A controllable-pitch propeller whose pitch is automatically varied in flight by a governor maintaining constant rpm despite varying air loads.

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