Rotor System Flashcards

1
Q

the tail rotor rotates clockwise ( from left hand view) and generates “anti-torque” air flow to the right hand side. What is the result of this?

A

It forces the tail to the left naturally

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2
Q

what are the rotor blades constructed from?

A

foam cored fiberglass and carbon fiber skin

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3
Q

what is the purpose of the blade tips?

A

provide blade tip streamlining movement

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4
Q

what is the purpose of the 6 trim tabs?

A

provide dynamic blade tracking and balancing

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5
Q

what are the leading edges made from, and what is their purpose?

A

Stainless steel to provide erosion and abrasion protection

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6
Q

how are the blades attached to the rotor system?

A

they are mounted to spherical thrust bearings and the elastomeric frequency adapters in between the mounting bars

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7
Q

what is the purpose of the spherical thrust bearings?

A

Located at the center of the hub the spherical thrust bearings handle the centrifugal loads from the blades and also ‘twist’ to provide pitch rod change movement

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8
Q

what is the purpose of the elastomeric frequency adapters in between the mounting bars?

A

mounted at the ends of the center hub, the frequency adapters absorb fore and aft loads (lead/lag) on the head

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9
Q

what is the purpose of the droop rings?

A

provides support for the blades when the aircraft is static. Also supports the head during rotor slow down

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10
Q

In high wind conditions, what prevents excessive blade conning (upward flap)?

A

Anti-conning stops. Located at each attachment bar
At 181-202 RPM the fly weight moves the contact arm out of the way and the springs retract the stops as the rotor speed decreases

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11
Q

What controls tilt of the swashplate?

A

Cyclic inputs tilt of the swashplate

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12
Q

The rotor head is —— in the flapping axis and ——- in the lead/lag axis?

A

flexible

ridged

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13
Q

The assemblies that make up the rotor shaft assembly are?

A

the rotor shaft, swashplates, a conical housing, pitch change rods, and a blade droop restrainer ring.

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14
Q

What is installed in the rotor blade to counteract natural flapping?

A

An integral brass weight is installed inside the leading edge to counteract natural flapping frequencies that result from the light composite blades.

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15
Q

Why is there a grounding strap installed at the blade root?

A

To minimize radio and radar interference by equalizing static charges that may accumulate on the blade

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16
Q

Where is the main rotor brake installed?

A

Mounted on the MGB oil cooler fan shaft. The brake is a mechanically operated friction disk and brake caliper device

17
Q

What does the Tail Rotor system consist of?

A

The tail rotor head consists of a rotor hub, central plate, pitch change spider, and a fairing.

18
Q

How are the tail rotor blades constructed? This process helps prevent “skin debonding.”

A

Each blade is constructed of composite materials by means of a Resin Transfer Molding (RTM) process,
which creates a single material construction and eliminates skin debonding

19
Q

what creates centrifugal retention on the tail rotor blades?

A

Centrifugal retention of each blade is made by a tension torsion bar made of 38 individual tension thin stainless steel layers.

20
Q

How are the tail rotor blades arranged and why?

A

The blades are arranged around the rotor hub in

an uneven pattern to reduce the noise signature.