AIRCRAFT PROPELLER (MIDTERM) 2 Flashcards

1
Q

Fixed-Pitch Propellers
Ground Adjustable Propellers
Variable Pitch Propellers
● Controllable Pitch Propellers
● Constant Speed Propellers

A
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2
Q

is an engine rpm sensing device with
a high pressure oil pump.

A

Propeller Governor

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3
Q

In a constant-speed propeller
system, the governor responds to a change in engine rpm
by directing oil under pressure to the propeller hydraulic
cylinder or by releasing oil from the hydraulic cylinder,
depending on system design.

A

Propeller Governor

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4
Q

The change in oil volume in
the hydraulic cylinder changes the blade angle and
maintains the engine rpm

A

Propeller Governor

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5
Q

FACTORS USED TO CHANGE ANGLE IN A
CONSTANT SPEED PROPELLER

A
  • Centrifugal Twisting Moment
  • Propeller Governor Oil
  • Propeller Blade Counterweight
  • Pneumatic pressure against the propeller
    piston
  • Springs
  • Aerodynamic twisting moment
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6
Q

a component of the
centrifugal force acting on a rotating blade that tends at all times to
move the blade into low pitch

A

Centrifugal twisting moment

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7
Q

on the propeller piston side of the
governor moves the blades to low pitch. This balances against the
propeller blade counterweights. The latter moves the blades
toward high pitch.

A

Propeller Governor Oil

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8
Q

always move the blades
toward high pitch

A

Propeller blade counterweights

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9
Q

pushes toward high pitch.

A

Pneumatic pressure against the propeller
piston

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10
Q

push in the direction of high pitch and
feather.

A

Springs

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11
Q

moves
the blades toward high pitch.

A

Aerodynamic twisting moment

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12
Q

The most powerful force is the _______ acting on the propeller
piston.

A

governor
oil Pressure

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13
Q

The engine driven single
acting propeller governor
(constant-speed control)
receives oil from the
engine’s lubrication system
and boosts that pressure to
that required to operate the
pitch changing mechanism

A

Governor mechanism

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14
Q

Key components

A
  • Flyweights
  • Speeder spring
  • Pilot valve
  • Governor Pump
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15
Q

These sense changes in engine speed.

A

Flyweights

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16
Q

Sets the desired RPM by balancing the
flyweight force.

A

Speeder spring

17
Q

Controls the flow of oil to and from the propeller
hub.

A

Pilot valve

18
Q

Increases oil pressure for blade pitch changes

A

Governor Pump

19
Q

When the engine is
operating at the rpm set
by the pilot using the
cockpit control, the
governor is operating

A

On speed

20
Q

When the engine is
operating above the rpm
set by the pilot using the
cockpit control or the
redline adjustment of the
governor, the governor is
operating in an over
speed condition

A

Overspeed

21
Q

When the engine is
operating below the rpm set
by the pilot using the cockpit
control, the governor is
operating in an under speed
condition

A

Underspeed

22
Q

Hartzell propellers can be classified by aluminum
hub (compact) and steel hub. Hartzell compact
aluminum propellers represent new concepts in
basic design. They combine low weight and
simplicity in design and rugged construction.

A
23
Q

In order to control the pitch of the blades, a hydraulic piston cylinder
element is mounted on the front of the hub spider.
The piston is attached to the blade clamps by means of a sliding rod
and fork system for non-feathering models and a link system for the
feathering models.
The piston is actuated in the forward direction by means of oil
pressure supplied by a governor, which overcomes the opposing force
created by the blade counterweights

A
24
Q

Feathering occurs because the summation
of internal propeller forces causes the oil to
drain out of the propeller until the feather
stop position is reached

A
25
Q

● Feathering is accomplished by releasing the governor oil pressure
from the piston assembly, allowing the counterweights and
feathering spring to feather the blades.
● This is done by pulling the condition lever (pitch control) back to
the limit of its travel, which opens up a port in the governor
allowing the oil from the propeller dome to drain back into the
engine.
● As the oil drains from the piston assembly, the actions of the blade
counterweights and feathering spring work to increase propeller
pitch.

A