Controls Flashcards

1
Q

Elevator pitches around the

A

Lateral axis

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2
Q

Rudder yaws around

A

Normal axis

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3
Q

Ailerons roll around

A

The longitudinal axis

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4
Q

Problems with controls at high speeds

A

Large control surfaces produces high control forces

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5
Q

How speed effects controls

A

Larger control movements at high speed are physically hard for the pilot than at slow speed

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6
Q

7 Types of aerodynamic balances

A
Modify forces on the control surface
Inset hinge 
Horn balance 
Internal balance 
Balance tab 
Anti balance tab
Servo tab 
Spring tab
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7
Q

Inset hinge

A

Hinge moment distance is reduced
Reduced feel
Reduced work on the control column
Max distance from the fwd hinge is 25%

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8
Q

Horn balance

A

Reduces the amount of force on the surface
Make the controls lighter and more effective
Forces hold the control in place

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9
Q

Internal balance

A

Sealed internal gap
Pressure differential causes an assist with the hinge moment
Reduces control column forces

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10
Q

Balance tab

A

Manual balance
Deflects in the opposite direction
Not very efficient due to going in the opposite direction
Make control surfaces lighter
Reduces the load felt at the control column
Reduces control effectiveness

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11
Q

Anti balance tab

A

Makes control surfaces heavier
The tab moves with the control surface
Improves efficiency
Less possibility of over stressing at higher speeds

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12
Q

Servo tab

A

Pilot is connected to the tab itself
Move and it creates an aerodynamic force which moves the tab in the opposite direction
Control authority decreases at slow speeds
Very effective at high speeds
Not very effective at slow speeds with small aerodynamic forces being produced

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13
Q

Spring tab

A

Acts like a servo tab at high speed

Acts like a balance tab at slow speeds

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14
Q

Mass balancing

A

Adding masses ahead of the hinge line to reduce flutter

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15
Q

Power assisted controls

A

Still some natural feel but mostly powered

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16
Q

Fully powered controls and how to avoid the risks

A

No feedback
Artificial feel is required
Provide all the power to move control surfaces

Q feel system generates artificial forces in proportion to dynamic pressure

17
Q

AoA in a roll

A

Downgoing is greater

Up going is reduced

18
Q

Aerodynamic damping in the roll

A

The up going wing is producing more CL which is creating more Di which is forcing the a/c to yaw in the opposite direction

Longer wings increase this

19
Q

Variable incidence tailplane

A
Whole a/c tailplane moves 
Common on jet a/c
Creates a large pitching moment 
Greater aileron authority 
Leading edge down, pitch up 
Leading edge up, pitch down
20
Q

High T tail

A
Improves L/D ratio 
Stays out of downwash 
Ground effect reduces
Heavier structural requirements on the tail 
Could go into the deep stall
21
Q

Rate controls

A

Ailerons

22
Q

Displacement controls

A

Rudder

Elevator

23
Q

Frise ailerons

A

Reduces adverse aileron yaw

Increases parasite drag on the downgoing wing to counteract the induced drag on upgoing

24
Q

Differential ailerons

A

Upgoing aileron deflects less than the downgoing and produces more drag to counteract the adverse aileron yaw

25
Q

Secondary effects of the rudder, aileron and elevator

A

Rudder - roll
Aileron - sideslip the yaw
Elevator - none

26
Q

Using a servo tab and during the flight the elevator jams, what happens the pitch control

A

Pitch control sense is reversed due to the controls being attached to the tab

27
Q

When trimmed fo 0 stick force, what causes less drag

A

Horizontal trimmable stabiliser than a trim tab

28
Q

On a trim tab runway what causes less control difficulty

A

Trim tab runway compared to a horizontal trimmable

29
Q

Stabiliser trim and flutter

A

Less sensitive to it

Flutter is also dependant upon IAS

30
Q

Difference between trim tab and servo tab

A

Trim tab reduces stick force to 0

Servo tab reduces stick force