Controls Flashcards

1
Q

What type of controls are ailerons

A

Rate controls

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2
Q

What is the formula for the hinge moment (feel)

A

Hinge moment = f x d

D= distance from centre of pressure of control surface to the hinge

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3
Q

What does a insert hinge do

A

The hinge connecting the control surface is inset slightly closer to the centre of pressure to reduce the force

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4
Q

What is the max Inset for a hinge

A

25% from the leading edge > trailing edge

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5
Q

What is a horn balance

A

Adds area of surface infront of hinge

When elevator is deflected a part deflects in the opposite direction to reduce the force required

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6
Q

What % inset is the horn balance limited to

A

25% of the chord

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7
Q

What is a balance tab

A

Deflects in the opposite direction of the control surface to make movements lighter but less effective

You move control surface which is then linked to the tab

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8
Q

What is a anti- balance tab

A

Works against you

You move control which deflects tab to make controls heavier

Less likely to overstress aircraft

Retaining control feel at low speed

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9
Q

What is a servo tab

A

You move the tab (not the control surface)

Makes controls lighter

High speeds = makes controls lighter

Slow speed = small force produced by tab = controllability issues

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10
Q

What is a spring tab

A

Like a servo tab but with a spring

At slow speeds whole control surface moves as not enough force to stretch spring

High speeds = spring stretches to do the same job as servo tab

Solves the problem of low speed control issues

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11
Q

Is a mass balance a aerodynamic balance

A

NO!!!!!

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12
Q

What are the different types of mass balances

A

Mass in the horn balance

Mass on boom attached to control surface

Arc shaped mass forward of control surface

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13
Q

How do mass balances work

A

Moving the cg of the control surface forward meaning it has a lower inertia (wants to move less)

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14
Q

What is the difference between a elevator and a stabilator

A

Elevator is a camber changing device

Stabilator is a angle of attack changing device

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15
Q

When is the greatest risks during s fin stall

A

Counteracting asymmetric power on a Engine failure on multi engine aircraft

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16
Q

What direction does the raf need to come from to produce a positive angle on the rudder

A

Raf from the right = positive

17
Q

If ailerons are rate control what is rudder and elevator

A

Displacement

18
Q

What causes aerodynamic damping

A

Higher AOA on down going wing = more lift

Lower AOA on up going wing = less lift

19
Q

If you roll right what was do you yaw

A

Left

20
Q

What are frise ailerons

A

Down going wing = aileron up = leading edge of aileron protrudes below = drag = helps counter adverse aileron yaw

21
Q

What are differential ailerons

A

down going wing aileron deflects more than up going going = more drag = helps reduce aileron yaw

22
Q

How do large aircraft control adverse aileron yaw

A

Frise ailerons

Spoilers

Control coupling

23
Q

What would happen if the outboard ailerons were used at high speed on a large jet

A

Wing twist = adverse aileron yaw

24
Q

How do spoilers help stop adverse aileron yaw

A

Down going wing = spoilers up a bit to create more drag

25
Q

What are the advantages of spoilers as roll control

A

Don’t suffer from flutter

Leave tailing edge free for flaps

Cause no twisting moment

26
Q

What is a flaperon

A

Aileron can drop slightly to give the effect of s flap

27
Q

What is control coupling

A

Where a mixer unit interconnects the inputs from the control column and the rudder peddle

28
Q

What are the advantages of a trimmable horizontal stabiliser

A

More aerodynamically effective (less drag)

Enables equal pitch up and down control about any trimmed position

Control over a greater cg range

Less sensitive to flutter

29
Q

What may help a Jamed stabiliser

A

Reducing speed might help by reducing the size of the out of trim force but will also reduce effectiveness