Dale Crane Q's Flashcards

1
Q

Two variables in the angle of attack of a propeller are:

A
  1. engine RPM (rotational speed)
  2. Forward velocity (speed of aircraft)
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2
Q

The curved surface of a propeller blade is the ______

(back or face)

A

back

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3
Q

The pitch angle and the angle of attack of a propeller blade _______ the same.

(are or are not)

A

are not

(would only be the same if no forward velocity)

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4
Q

Propeller blade stations are measured in inches from the _______ (hub or tip)

A

hub

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5
Q

The actual distance a propeller advances in one revolution in theair is the _________ pitch

(effective or geometric)

A

effective

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6
Q

The difference between the geometric and effective pitch of a propeller is called _____

A

slip

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7
Q

Five factors that affect the amount of thrust produced by a propeller blade are:

A
  1. Airfoil shape
  2. Air density
  3. Angle of Attack
  4. Velocity of airflow
  5. Area of airfoil
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8
Q

Two things that change on a propeller blade from the root to the tip are:

A
  1. Blade pitch angle
  2. Cross section of the blade
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9
Q

Increasing the engine RPM with the forward speed remaining constant _________ the angle of attack

(increases or decreases)

A

increases

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10
Q

Five forces acting on a propeller turning at a high speed are:

A
  1. Centrifugal force
  2. Thrust bending force
  3. Torque bending force
  4. Aerodynamic twisting force
  5. Centrifugal twisting force
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11
Q

The greatest force acting on a propeller is _______ force

A

centrifugal

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12
Q

The force that tries to bend a propeller blade forward is the _____ bending force

A

thrust

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13
Q

The force that tries to bend a propeller blade in its plane of rotation is the ___________ force

A

Torque bending force

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14
Q

Aerodynamic twisting force (ATF) tries to _______ the blade angle

(increase or decrease)

A

increase

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15
Q

Centrifugal twisting force (CTF) tries to ______ the blade angle

(increase or decrease)

A

decrease

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16
Q

The twisting force that has the greater effect on propeller operation is _______ (ATF or CTF)

A

CTF

17
Q

A fixed-pitch climb propeller has a ______ pitch angle than a cruise propeller

(higher or lower)

A

lower

18
Q

Centrifugal force acting on the counterweights on a two-position-pitch propeller rotate the blades toward _______ pitch

(high or low)

A

high

19
Q

The basic difference between a two-position controllable-pitch propeller and a constant-speed propeller is in the control.

In a constant-speed propeller, a ______ replaces the two position valve

A

governor

20
Q

Multiengine airplanes were made appreciably safer than their single-engine counterpart by the development of the ______ propeller

A

feathering

21
Q

The blade pitch angle when a propeller is feathered is near _______ degrees

A

90

(88 degrees)

22
Q

A reversible propeller is a constant-speed propeller whose ______ (low or high) pitch stops can be released so the blades can be moved to an angle that produces thrust in the reverse direction

A

low

23
Q

The wood used for most commercially made wood propellers is ______

A

Birch

24
Q

Modern metal propellers are forged from high-strength ________ alloy, and after being ground to their finished dimensions and pitch, they are ______ to protect them from corrosion

A

aluminium

anodized

25
Q

The two types of propellers that are found on almost all modern airplanes are:

  1. ________
  2. ________
A
  1. Fixed pitch
  2. Constant speed
26
Q

The pitch on all modern constant-speed propellers is changed ________ (electrically or hydraulically)

A

hydraulically

(oil)