Flight Controls (S1) Flashcards

1
Q

What are the requirements of the rotor head

A

Provide attachment point for rotor blades
Transmit drive from engine to the rotor blades
Allow blade freedom of movement
Allow a control interface to change the pitch
Support the blades

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2
Q

What are the main types of rotor head

A

Fully articulated
Semi rigid
Rigid

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3
Q

What additions can be present on a rotor head

A

Lifting eye
Flapping restrainer
Droop restrainer

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4
Q

What is a drag damper used for

A

To reduce the rate of dragging and absorb shock loads

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5
Q

What type of drag dampers are there

A

Elastomeric
Hydraulic

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6
Q

What is the purpose of the tie bar

A

To absorb centrifugal loads generated by rotating blades

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7
Q

What 3 attachments does the MRBS have

A

Pitch bearings
Tie bar
Damper support

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8
Q

What does the tie bar do and how does it work

A

Connects the sleeve to the rotor head, is made using miles of wound wire around 2 bushes, wound at an angle to offset the aerodynamic affects on pitch

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9
Q

What is the purpose of the rotor blades

A

Produce a force greater than the weight of the aircraft to provide thrust

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10
Q

How can blade lift be evenly distributed

A

Wash-out
Tapered blades

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11
Q

What can be used to balance blades

A

Weights

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12
Q

What is used to aid the instalment of blade pins

A

Bullet adaptors that help get past any misalignments without damaging the pin

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13
Q

What is a bonding lead and its purpose

A

A cable completing the electrical path from the rotor head to the blade to reduce damage to aircraft during lightning strikes, to prevent static buildup and reduce electric shock hazard

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14
Q

What are trim tabs

A

Small device fitted to the trailing edge to balance the blade aerodynamically. Done by manufacturers

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15
Q

What does a static wick do

A

Discharges static electricity

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16
Q

What is the lift load path

A

MRB
Rotor head
Rotor mast
Gearbox casting
Gearbox supports
Airframe mountings

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17
Q

What methods ore there of negating vibration

A

Mass/spring main rotor head vibration absorber (MRHVA)
Bifilar vibration absorber
Active vibration cancellation

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18
Q

What are the 3 types of tail rotor

A

Free (Lynx, Apache)
Shrouded (Gazelle)
NOTAR

19
Q

What are the disadvantages of shrouded tail rotors

A

Increase in weight
Increase in power requirement
Increase in drag
Higher costs

20
Q

What are the 5 main parts of a tail rotor blade

A

Spar
Root end
Skin
Erosion shield
Blade tip

21
Q

What should be checked for during rotor blade maintenance

A

Dents, cracks, distortions
Attachments
Bearing wear
Damage to tips and tabs
Balancing

22
Q

What 2 systems are used to alter MRB pitch

A

Swash plate system
Spider system

23
Q

What is geometric lock

A

Where cables and rods aren’t correctly adjusted and can cause controls to become locked after they get caught on each other

24
Q

What 2 measures are there to make sure control rods are correctly tightened

A

Witness hole
Witness line

25
What is used to change rod inputs to cables or vice versa
Quadrant
26
What are control stops
Adjustable or fixed stops that restrict the movement of the control inputs, to prevent geometric locking and prevent dangerous inputs
27
What type of cable is used on cable control systems
Preformed cable Kink resistant and will not unravel
28
What are turnbuckles
Used to join and adjust the length of wire control systems.
29
How are turnbuckles secured
Wire locking Provided locking clips
30
What types or turnbuckles are there
Tension Barrel
31
What is a swaged end
Clamping and forming the end of a cable to secure it
32
What are fairleads
Restrainers along a cable system to limit the amount of movement of the cable during vibrations
33
How can left hand threads be identified
Notches in the nut Grooves
34
What is an interlink assembly
Linked controls to deal with collective, cyclic or yaw inputs that keep the aircraft level
35
How can constant rotor speed be maintained
Automatic fuel supply changes to the engine made by a computer to change the output from the engine
36
What is rigging
The truing and checking the system to ensure the flying controls operate correctly
37
What are rigging pins
Pins used to hold control systems into a predefined position for tests to be carried out (neutral position)
38
What are the 2 parts of an independent inspection
Correct assembly check Functional systems check
39
When is rigging carried out
At specific intervals laid down by AMM After disturbing any part of the control system
40
What are the design requirements of rotor blades
Have good lift:drag ratio Maximum lift required Minimise pitching moments
41
What are the 3 areas of a blade
Root Centre Tip
42
What are doubler plates
Plates at the blade root, increase the strength of the blade in critical area
43
How can rotor blades be identified
Colour coding