11.9 Flight Controls Flashcards

1
Q

Primary control system operating methods

A
  • Cable operated system
  • boosted cable system
  • hydraulic power operated system
  • push pull rod system
  • fly by wire system
  • fly by light system
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2
Q

Trim?

A

Keeps flight controls in position

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3
Q

Artificial feel?

A

Makes controls proportional to loads so pilot doesnt over comtrol

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4
Q

In event of hydraulic system failure what is used

A

Servo tabs

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5
Q

Roll and yaw trimming

A

Trim tabs used for roll and yaw trimming

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6
Q

Pitch trimming

A

Trimmed by adjusting position of leading edge of horizontal stabiliser

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7
Q

Mach trim compensation?

A

Compensates the pitch down tendency at high speed

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8
Q

High lift devices?

A
  • Trailing edge flaps ( increase area and camber. Increase angle of attack)
  • Leading edge flaps (2 positions extended or retracted)
  • Slats (3 positions, fully extened , fully retracted of partially extended)
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9
Q

Spoiler and speed brake system

A
  • spoilers “spoil lift”
  • flight spoilers and ground spoilers
  • flight spoilers help ailersons in lateral movement
  • speed brake- work symmetrically during a brake
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10
Q

Artificial feel system

A
  • needed when hydraulic actuator used

* prevent over control from pilot

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11
Q

Stall protection system

A
  • system consists of warning, and prevention mechanism

* prevention lowers angle of attack

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12
Q

Rudder travel limiter

A
  • large aircraft need it

* protects tail from overload at high speed

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13
Q

Active stability systems

A

•provide stability during flight

…..yaw damper( prevents dutch roll )

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14
Q

Fly-by wire system

A

•uses electrical wires to connect flight control surfaces to cockpit

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15
Q

Fly-by light system

A
  • uses fibre optic cables rather than wires

* susceptible to EMI

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16
Q

Cable operated system

A
  • cables only

* used in light low speed aircraft

17
Q

Booster cable system

A
  • 1kg of force on control = 14kg of force
  • hydraulic actuator used
  • servi tabs used for manual control if hydraulic system fails
18
Q

2 flap hinging methods

A
  • Fixed hinge point

* flaps with rollers in tracks

19
Q

What happens in event of hydraulic failure

A

Servo tabs used

20
Q

Follow up control?

A

Used to close control valve of servo control unit when its reached its desired position

21
Q

When is trim tab used

A

Trim tab puts 0 load on control column, it allows for hands off and level flight

22
Q

Stall protection

A

Auto slat

23
Q

Biggest problem with fly by light system

A

EMI

24
Q

Where are krueger and droop flaps located

A

Leading edge

25
Q

Torque tubes?

A

Torsion load turned into linear motion