Rotary Flashcards

1
Q

Define rotor mast

A

Supports and drives the main rotors

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2
Q

Define rotor disc

A

Area projected by the rotor travel

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3
Q

Outline Shaft axis

A

Axis through the rotor mast, which about the rotors are ALLOWED to rotate

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4
Q

Outline axis of rotation

A

The imaginary line about which the rotars actually rotate

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5
Q

Plane of rotation

A

Plane at right angles to the axis of rotation

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6
Q

Tip path plane

A

Imaginary circular plane outline from the rotor tips during travel

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7
Q

Define blade coning

A

Upward flex of the rotor blades due to pitch and lift increased and centrifugal force is applied

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8
Q

Define cone angle

A

Angle between blades span wise axis and the plane of rotation.

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9
Q

Purpose of a transmission system

A

To transfer power from engine to the main rotors, tail rotor and other accessories

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10
Q

Purpose of mgb

A

Reduce the engines high RPM low torque to high torque low RPM for rotors

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11
Q

Components of a tail rotor drive system

A

MGB, drive shafts, tail rotor gearbox, and tail rotor

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12
Q

Main components of a transmission system (4)

A

MGB
TR Drive system
Clutch
Freewheel

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13
Q

4 forces acting on helicopter in hover

A

Directly upwards forces, thrust and lift, equal to the directly downward forces, drag and weight.

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14
Q

Forces in forward flight (2)

A

Total resultant thrust

Total resultant drag

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15
Q

Outline ground effect

A

When helicopter is hovering within 1 rotor diameter from the ground, it stops induced airflow through disc and the loft vector increases and less power is needed

Also reduces blade tip vortices

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16
Q

Define recirculation

A

When the same air passes through the disc, which is more turbulent and reduces production of lift.

17
Q

Outline gyroscope precession

A

An input on a rotating mass, will have an output manifest 90 degrees in the direction of rotation. “Lag effect”

18
Q

Define disymmetry of lift

A

Advancing blade travels faster in relation to the realitive air flow. And the retreating blade travels slower. Blades will flap to equality to reduce this.

19
Q

How is retreating blade stall perceived when evident

A

Roll
Pitch up
Vibrations

20
Q

Outline coriolis effect

A

Acceleration and deceleration as the rotor blades flap. When the centre of mass of a rotor blade moves towards the centre of rotation the blade will speed up.

21
Q

Purpose of tail rotor [2]

A

Counter main rotor torque

Alter fuselage heading

22
Q

Define translating tendency

A

When helicopter drifts from the thrust cuased by tail rotor to counter the rotors toqure.

To stop this. Manufacturers mount mast at a tilt

23
Q

Translational lift

A

When helicopter moves forward at about 16 to 24knts it will move out of its downward and into clean air. This gives a boost in lift

24
Q

4 defects of rotor blades

A

Delamination
Cracking
Erosion
Impact damage