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
Q

What is used to change rod inputs to cables or vice versa

26
Q

What are control stops

A

Adjustable or fixed stops that restrict the movement of the control inputs, to prevent geometric locking and prevent dangerous inputs

27
Q

What type of cable is used on cable control systems

A

Preformed cable
Kink resistant and will not unravel

28
Q

What are turnbuckles

A

Used to join and adjust the length of wire control systems.

29
Q

How are turnbuckles secured

A

Wire locking
Provided locking clips

30
Q

What types or turnbuckles are there

A

Tension
Barrel

31
Q

What is a swaged end

A

Clamping and forming the end of a cable to secure it

32
Q

What are fairleads

A

Restrainers along a cable system to limit the amount of movement of the cable during vibrations

33
Q

How can left hand threads be identified

A

Notches in the nut
Grooves

34
Q

What is an interlink assembly

A

Linked controls to deal with collective, cyclic or yaw inputs that keep the aircraft level

35
Q

How can constant rotor speed be maintained

A

Automatic fuel supply changes to the engine made by a computer to change the output from the engine

36
Q

What is rigging

A

The truing and checking the system to ensure the flying controls operate correctly

37
Q

What are rigging pins

A

Pins used to hold control systems into a predefined position for tests to be carried out (neutral position)

38
Q

What are the 2 parts of an independent inspection

A

Correct assembly check
Functional systems check

39
Q

When is rigging carried out

A

At specific intervals laid down by AMM
After disturbing any part of the control system

40
Q

What are the design requirements of rotor blades

A

Have good lift:drag ratio
Maximum lift required
Minimise pitching moments

41
Q

What are the 3 areas of a blade

A

Root
Centre
Tip

42
Q

What are doubler plates

A

Plates at the blade root, increase the strength of the blade in critical area

43
Q

How can rotor blades be identified

A

Colour coding