Lesson 5 Flashcards

(50 cards)

1
Q

What are the basic requirements of controls?

A

Not too light
Not too heavy
Control forces should vary with IAS
No lag - controls should be responsive
Harmonised - similar for pitch/roll

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2
Q

What is the
axis of rotation
control
primary effect
secondary effect
of

aileron

A

axis of rotation:
Longitudinal

control:
Lateral

primary effect:
Roll

secondary effect:
Yaw

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3
Q

What is the
axis of rotation
control
primary effect
secondary effect
of

elevator

A

axis of rotation:
Lateral

control:
Longitudinal

primary effect:
Pitch

secondary effect:
(speed)

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4
Q

What is the
axis of rotation
control
primary effect
secondary effect
of

rudder

A

axis of rotation:
Normal

control:
Directional

primary effect:
Yaw

secondary effect:
Roll

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5
Q

Suggest some combined controls (3)

A

Ruddervator
Elevon
Taileron

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6
Q

What type of controls have a mechanical connection between the control column and control surfaces.

A

Conventional -
full feedback to pilot

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7
Q

What type of controls have a mechanical link and are augmented?

A

Partially powered controls -
Pilot still gets feedback

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8
Q

What type of controls does not have any mechanical connection to the control surface?

A

Fully powered controls -
No pilot feedback

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9
Q

What can be used in an aircraft with fully powered controls to reduce the chances of the pilot demanding too much control deflection and overstressing the aircraft? (3)

A

Springs
Bobweight
Fly-by-wire

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10
Q

Name types of aerodynamic balance
(1x hinge)
(2x balance)
(4x tab)

A

Inset hinge
Horn balance
Internal balance
Balance tab
Anti-balance tab
Servo tab
Spring tab

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11
Q

Which aerodynamic balance will move the position of the hinge (usually aft) and what does it do to the forces?

A

Inset hinge

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12
Q

Which aerodynamic balance sticks out ahead of the control surface, forward of the hinge?

A

Horn balance

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13
Q

Which balance has an internal chamber which can be split into two by a flexible seal?

How does this work?

A

Internal balance

Two halves of the camber are exposed to the static pressure on the upper/lower surfaces.

As the control surface is deflected then the static pressures will change, creating a pressure gradient and helps the pilot, making the aircraft controls lighter.

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14
Q

Which balance is similar to a trim tab but moves with the same control but in the opposite direction?

A

Balance tab (not the same as a trim tab)
The balance tab moves in the opposite way to the control surface

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15
Q

Which balance is works the opposite to the ‘balance tab’? It moves in the same direction as the control surface.

A

Anti-balance tab

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16
Q

Which balance system can be use in the case of hydraulic failure?

A

Servo tab

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17
Q

What balance system acts like a servo tab at higher speeds and a regular control surface at lower speeds.

A

Spring tab

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18
Q

Name a balance that is NOT aerodynamic.

A

Mass balance

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19
Q

Control flutter would be dampened (or prevented) by which type of balance

A

Mass balance

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20
Q

Fly-by-wire normal law:
What does forward/aft on the sidestick command?

A

g-force

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21
Q

Fly-by-wire normal law:
What does left/right on the sidestick command?

22
Q

What are the two forms of protection?

A

Soft - can be overridden
Hard - can’t be overridden

23
Q

In alternate law, what does side stick command?

A

Same as ‘Normal law’

24
Q

In direct law, what does side stick command?

A

Now a direct relationship with the control surfaces.

25
What protections do you have in 'normal law'
Hard and Soft
26
What protections do you have in 'alternate law'?
Soft only
27
What protections do you have in 'Direct law'?
None
28
When talking about FBW law, what do failures cause?
A degradation to a lower law.
29
When you manoeuvre an aircraft, what will resist this?
Aerodynamic damping
30
What would effect the strength of aerodynamic damping?
Wingspan - longer is stronger damping Density - weaker in low density
31
When we draw a RAF line, the angle is used for AoA. What does the length represent
TAS
32
Describe a fries aileron
To fix adverse aileron yaw when the aileron is going up, the leading edge points down into the airflow creating drag on the downwind wing
33
What are the 4 ways you can prevent adverse aileron roll
Differential ailerons Frise ailerons Roll spoilers Coupled controls
34
What are the two configurations that can be used for trimming?
Elevator and trim tab Trimmable horizontal stabiliser
35
Why may you want to trim the aircraft with the nose up?
Climb Slower forward CG
36
Trim tab moves in same/opposite direction to elevator?
Opposite
37
Which direction does the trim tab move in when you rotate the trim wheel for nose down?
Nose down = trim tab up
38
Which direction does the trim tab move in when you rotate the trim wheel for nose up?
Nose up = trim tab down
39
When you trim the aircraft, the physical control column does what?
Stays in the trimmed position.
40
What drag is introduced with the use of the trim tab?
trim drag
41
Name 3 disadvantages of using elevator trim tabs.
Creates trim drag Reduces elevator effectiveness Can run out of elevator authority (so limit CG range)
42
When using trim tabs there is a risk of running out of elevator authority. How do we guard against this?
Use CG limits
43
Where is a THS hinged
centrally
44
At what stage can you not feel when the aircraft is in/out of trim?
Before takeoff
45
What's the name of the angle between the Relative Air Flow (RAF) and the longitudinal axis? (clear when operating the rudder)
Beta angle
46
Is weight or lift greater in a climb?
Lift is less than weight in a climb
47
If lift is greater than weight then how can an aircraft still climb?
Thrust
48
How man 'g' is the load factor in a climb?
Load factor in a climb is less than 1g
49
Equation: Lift, weight, gamma
Lift = weight COS$gamma;
50