HELICOPTERS Flashcards

1
Q

The rotor wings, or rotor blades, are attached to the __________.

A

Mast

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2
Q

Major components of modern helicopters.

A

Airframe
Fuselage
Landing Gear
Powerplant
Transmission
Main Rotor System
Tail Rotor System

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3
Q

Transfers power directly to the main and tail rotor systems.

A

Transmission

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4
Q

Provides the aerodynamic forces necessary to fly.

A

Main Rotor System

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5
Q

An anti-torque component that keeps the helicopter from turning due to torque.

A

Tail Rotor System

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6
Q

Newton’s third law of motion states…

A

…“To every action, there is an equal and opposite reaction.”

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7
Q

When a helicopter is hovering, it has a tendency to…

A

…drift laterally to the right caused by the lateral thrust supplied by the rotor.

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8
Q

The pilot may prevent lateral drift by tilting the…

A

…main rotor to the left, which counteracts the tail rotor thrust to the right.

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9
Q

The rotor system produces…

A

…centrifugal and centripetal force.

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10
Q

Has a propensity to make rotating bodies move away from the center of rotation.

A

Centrifugal Force

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11
Q

__________ counteracts __________ by keeping rotating bodies a certain radius from the center of rotation.

A

Centripetal Force
Centrifugal Force

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12
Q

The Coriolis Effect is also known as…

A

…the law of conservation of angular momentum.

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13
Q

The Coriolis Effect states…

A

…that an object will have the same velocity of momentum unless acted upon by an external force.

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14
Q

__________ accelerates as a rotating body moves closer to he axis of rotation.

A

Angular Momentum

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15
Q

As rotator blades move around their axis of rotation…

A

…there is a slight change in diameter due to the blades flapping.

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16
Q

The changes in diameter due to the blades flapping creates a small __________ resulting in __________.

A

acceleration and deceleration of the rotational velocity

fluctuations in lift

17
Q

The phenomenon in which force applied to a rotating object is manifested 90 degrees later in the direction of rotation.

A

Gyroscopic Precession

18
Q

Controls used to handle a helicopter.

A

Collective Pitch Control
Cyclic Pitch Control
Anti-Torque Pedals
Throttle Control

19
Q

Used to change the pitch angle of the main rotor blades simultaneously.

A

Collective Pitch Control

20
Q

As the pitch angle of the blade increases, __________ drag occurs.

A

More

21
Q

As the pitch angle of the blade decreases, __________ drag occurs.

A

Less

22
Q

__________ blade speed helps generate lift.

A

Faster

23
Q

Used to fly the helicopter forward, backward, left, and right.

A

Cyclic Pitch Control

24
Q

Used to change the pitch of the tail rotor blades, increasing or decreasing tail rotor thrust in a desired direction.

A

Anti-Torque Pedals

25
Q

Used to control the power of the engine and ensures that the rotational speed of the rotor blades is in a desired range.

A

Throttle Control

26
Q

Ty

A

Ty