Rotor Blade Designs and Construction

Choose a study mode

Play Quiz
Study Flashcards
Spaced Repetition
Chat to Lesson

Podcast

Play an AI-generated podcast conversation about this lesson

Questions and Answers

Which inspection method is primarily used for composite rotor blades?

  • Ultrasonic testing
  • Tap testing (correct)
  • Dye penetrant testing
  • Visual inspection

Where are additional double plates typically found on a rotor blade?

  • At the leading edge
  • At the trailing edge
  • At the root of the tip (correct)
  • At the center of span

What is the primary purpose of spanwise balance weights on a rotor blade?

  • To increase blade strength
  • To achieve balance along the blade's length (correct)
  • To control blade tracking
  • To adjust blade pitch

If a helicopter has a weight added to the leading edge of a blade, how would it affect the plane of rotation?

<p>It would make the helicopter fly lower (C)</p> Signup and view all the answers

Where are trim tabs typically located on a rotor blade?

<p>At the trailing edge, 75% of the span (C)</p> Signup and view all the answers

Which control is typically rigged first on a helicopter?

<p>Collective (C)</p> Signup and view all the answers

Where is the servo flap located on a rotor blade?

<p>Trailing edge, about 75% of span (A)</p> Signup and view all the answers

What is a benefit of using main servo flaps?

<p>They reduce the need for hydraulics (C)</p> Signup and view all the answers

What is a key characteristic of an asymmetrical rotor blade?

<p>Higher camber on one side (A)</p> Signup and view all the answers

Why are symmetrical rotor blades more commonly used than asymmetrical ones?

<p>They have a more stable aerodynamic characteristic (A)</p> Signup and view all the answers

What is a uniform planform in rotor blade design?

<p>When the leading and trailing edges are parallel to each other (D)</p> Signup and view all the answers

Why are uniform rotor blades preferred by manufacturers over tapered ones?

<p>They are more cost-effective to produce. (A)</p> Signup and view all the answers

What does a negative twist in a rotor blade achieve?

<p>Produces a higher angle of attack at the root. (A)</p> Signup and view all the answers

Which construction method is favored for rotor blades due to its strength and absence of drilled holes?

<p>Bonded construction (C)</p> Signup and view all the answers

What is a result of adding weight forward on a rotor blade?

<p>It will cause the blade to fly lower in its plane of rotation. (D)</p> Signup and view all the answers

What common feature is present on all leading edges of rotor blades?

<p>A stainless steel capping. (B)</p> Signup and view all the answers

Flashcards

Tap Testing

A primary inspection method for composite rotor blades, using tapping to detect damage.

Double Plates

Additional plates located at the root of the tip of a rotor blade, increasing structural strength without adding weight.

Spanwise Balance Weights

Weights located along the length of the rotor blade to balance its weight distribution.

Chordwise Mass Balance Weights

Weights placed along the width of the rotor blade, usually closer to the leading edge, to balance the blade during rotation.

Signup and view all the flashcards

Tracking Weights

Weights located on the leading and trailing edges of the rotor blade near its span, used for controlling the helicopter's pitch attitude.

Signup and view all the flashcards

Trim Tab

A small airfoil located on the trailing edge of a rotor blade, primarily used to adjust the helicopter's pitch.

Signup and view all the flashcards

Hydraulic System Depressurization

A procedure to ensure all hydraulic pressure is removed from the system before rigging a helicopter.

Signup and view all the flashcards

Collective Pitch Control Rigging

The first control to be rigged on a helicopter, used to adjust the pitch of the main rotor blades.

Signup and view all the flashcards

Symmetrical Rotor Blade

A rotor blade design where both sides have the same curvature, resulting in consistent aerodynamic characteristics.

Signup and view all the flashcards

Asymmetrical Rotor Blade

A rotor blade design where one side has a greater curvature (camber) than the other, providing more lift for the same surface area.

Signup and view all the flashcards

Uniform Planform

A rotor blade design where the leading and trailing edges run parallel to each other, resulting in a uniform chord length.

Signup and view all the flashcards

Tapered Planform

A rotor blade design where the leading and trailing edge converge towards the tip, resulting in a decreasing chord length.

Signup and view all the flashcards

Negative Twist

A technique to adjust the angle of attack (AOA) along the rotor blade, creating a more even lift distribution.

Signup and view all the flashcards

Bonded Construction

A method of constructing rotor blades where layers of material are bonded together, creating a strong and durable structure.

Signup and view all the flashcards

Single Pocket

A rotor blade design where the skin wraps completely around the spar, creating a single cavity.

Signup and view all the flashcards

Multi Pocket

A rotor blade design where the skin is divided into multiple sections, creating separate compartments.

Signup and view all the flashcards

Study Notes

Rotor Blade Designs

  • Symmetrical blades have better aerodynamic pitch characteristics.
  • Asymmetrical blades create more lift for the same surface area, with higher camber on one side.
  • Asymmetrical blade edges are swept 3 degrees upwards to improve stability.
  • Symmetrical blades are more common due to asymmetrical designs' instability.
  • Rotor blades exist in parallel (uniform) and tapered forms.
  • Uniform blades have parallel leading and trailing edges, creating more lift due to chord length.
  • Tapered blades converge towards the edges, creating more uniform lift.
  • Manufacturers favor uniform blades for cost-effectiveness due to simpler rib manufacturing.
  • Tapered blades require different ribs for varying chord lengths.

Rotor Blade Construction

  • Bonded construction is stronger than other methods and eliminates drilling holes.
  • Single-pocket construction makes building quicker due to a single skin.
  • Multi-pocket construction is more repairable but more expensive to manufacture.
  • Blade damage in single-pocket construction can lead to complete replacement.
  • Trim balance weights are used to fine-tune blade flight characteristics.
  • Forward weight shift lowers the blade, while aft shift raises it in flight.

Rotor Blade Materials and Inspection

  • Rotor blade leading edges often have stainless steel caps for erosion protection.
  • Composite, metal, and wood are used in rotor blade manufacturing.
  • Tap testing is a key inspection method for composite blades.
  • Additional structural plates at the blade root improve strength without adding weight.

Helicopter Control Systems

  • Spanwise and chordwise balance weights optimize rotor blade performance.
  • Tracking weights improve rotor blade positioning.
  • Trim tabs adjust pitch for optimal flight.
  • Hydraulic systems control flight adjustments (collective, throttle).
  • Collective is usually rigged first and connected to throttle.
  • Servo flaps reduce reliance on hydraulic systems.
  • Servo flaps are located at the trailing edge with infinite lifespan.
  • Servo flaps enhance helicopter maneuverability and efficiency.

Studying That Suits You

Use AI to generate personalized quizzes and flashcards to suit your learning preferences.

Quiz Team

Related Documents

Week 3 Rotor Wing Review PDF

More Like This

Rotor Blade Design Overview
16 questions
Rotor Blade Design Overview
23 questions
Rotor Blade Design Overview
24 questions
Rotor Blade Design Overview
23 questions
Use Quizgecko on...
Browser
Browser