Chapter 18 - Control Flashcards

1
Q

Basic requirements are
Forces?

Feel?

Responsive?

Movement and Harmony?

A

The forces on the controls must not be too heavy or light.

You must be able to sense airspeed through the controls- must be proportional to aerodynamic force.

No delay in response

Controls must not require excessive small or large input, fwd + aft, should be the same as left + right to harmonise.

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2
Q

Aileron is changing the aerodynamic force which is a what control?

A

rate

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3
Q

Rudder and elevator are a deflection effect which is a what control

A

displacement ( which changes the direction of the total reaction)

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4
Q

Hinge moments give us feel how

A

aerodynamic force x distance

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5
Q

Which aerodynamic balance gives a heavier feel

A

Anti balance tab

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6
Q

What does inset hinge do?

A

reduces the moment by reducing the distance. Max 25%

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7
Q

Horn balance does what?

A

Add area to the control surface in front of the hinge line

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8
Q

Trim Tab

A

Holds the control surface in the desired position by deflecting the opposite way

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9
Q

Internal Balance

A

Uses differential pressures to reduce forces

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10
Q

Balance Tab

A

Pilot moves the control surface - the balance tab then moves in the opposite direction to help reduce the forces

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11
Q

Servo tab

A

Pilot deflects the servo tab, not very good at low speeds and loses control authority

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12
Q

The spring tab

A

At low speeds = balance tab

At high speeds = Servo tab

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13
Q

Mass balance is for what and is put where

A

To stop flutter and in front of the hinge line

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14
Q

Power assisted controls have natural feedback?

A

Yes

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15
Q

Aerodynamic dampering is a resistance to roll why?

A

Because the down going wing will have an increased AOA

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16
Q

What is the difference between elevator and complete moving tail plane

A

Elevator is camber changing device

Moving tail plane changes the AOA

17
Q

What are the advantages of THS

A

Can deal with greater CofG changes
No loss of control authority
More efficient because less drag with no trim tabs

18
Q

When does fin stall come into effect

A

In cross winds

19
Q

Secondary effect of roll is

A

yaw

20
Q

Secondary effect of yaw is

A

roll

21
Q

secondary effect of pitch is

A

Doesn’t have one

22
Q

Adverse Aileron Yaw is

A

In a roll When the up going wing produces more lift and more induced drag causing the aircraft to yaw towards the up going wing.