Rotor Blade Construction Quiz
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Questions and Answers

What protects the leading edge of wooden rotor blades from abrasion?

  • Aluminum tip cap
  • Aluminum pockets
  • Stainless steel cap (correct)
  • Fiberglass cloth
  • What is a distinct advantage of metal rotor blades?

  • They are lighter than wood blades
  • They are more resistant to moisture damage
  • They have better quality control during construction (correct)
  • They are less expensive to manufacture
  • What is the purpose of the aluminum pockets on metal rotor blades?

  • To attach the blade to the rotor head
  • To protect the blade from abrasion
  • To improve the blade's aerodynamic profile (correct)
  • To provide additional strength to the blade
  • What is a disadvantage of wooden rotor blades?

    <p>They are susceptible to moisture damage (C)</p> Signup and view all the answers

    What type of construction is common to all rotor blades?

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

    What is the purpose of the steel cuff on metal rotor blades?

    <p>To attach the blade to the rotor head (D)</p> Signup and view all the answers

    What is the main reason why most wooden rotor blades are in matched pairs?

    <p>To ensure that the blades are identical in shape and weight (D)</p> Signup and view all the answers

    What type of material is used to cover the exterior surface of a fiberglass rotor blade?

    <p>Resin impregnated fiberglass cloth (A)</p> Signup and view all the answers

    What is the location of the blade tip?

    <p>Furthest from the center of rotation (A)</p> Signup and view all the answers

    What is the purpose of the blade tip cap?

    <p>To provide a means for attaching balance weights (A)</p> Signup and view all the answers

    What is the leading edge of the blade?

    <p>The part of the blade that meets the air first (D)</p> Signup and view all the answers

    Why is the leading edge of the blade thicker than the trailing edge?

    <p>To improve the aerodynamic performance of the blade (D)</p> Signup and view all the answers

    Why is the leading edge of the blade covered with a hard cap or coating?

    <p>To protect the blade from erosion caused by sand and dust (A)</p> Signup and view all the answers

    What is the span of a rotor blade?

    <p>The distance from the root to the tip of the blade (C)</p> Signup and view all the answers

    Why is the span line important to blade repairers?

    <p>It helps them to locate and classify damage to the blade (A)</p> Signup and view all the answers

    What is a primary advantage of using a uniform planform for rotor blades?

    <p>It simplifies the manufacturing process. (C)</p> Signup and view all the answers

    What does a uniform blade design reduce in terms of production?

    <p>The number of unique stamping dies needed. (C)</p> Signup and view all the answers

    How does a tapered planform blade differ in performance compared to a uniform planform?

    <p>It achieves a more uniform lift distribution. (C)</p> Signup and view all the answers

    What is a characteristic of most rotor blades in terms of twist?

    <p>They are twisted negatively from root to tip. (B)</p> Signup and view all the answers

    Which material is commonly used for the skin of rotor blades?

    <p>Aluminum (B)</p> Signup and view all the answers

    What is the function of the blade root in a rotor blade?

    <p>It provides attachment to the rotor head. (C)</p> Signup and view all the answers

    Why are tapered planform blades not commonly used by manufacturers?

    <p>They are more complicated and costly to manufacture. (D)</p> Signup and view all the answers

    What consequence arises if the blade angle remains constant along its length?

    <p>Uneven lift distribution across the blade. (B)</p> Signup and view all the answers

    What is the faying surface in bonding?

    <p>The surface area where two objects are bonded together (B)</p> Signup and view all the answers

    Why do manufacturers avoid drilling holes in load-carrying parts of the blade?

    <p>Holes weaken the strength of the bond (A)</p> Signup and view all the answers

    What type of weights are placed into the leading edge of a blade for mass balance?

    <p>Mass balance weights (B)</p> Signup and view all the answers

    What happens when weights in the blade are adjusted?

    <p>It alters the center of gravity (B)</p> Signup and view all the answers

    What is a potential consequence of careless use of cleaning solvents on bonded joints?

    <p>Dissolves bonded joints (B)</p> Signup and view all the answers

    Which weight type is typically located at the tip of the blade?

    <p>Spanwise weights (D)</p> Signup and view all the answers

    What does adding spanwise weight to a blade do to the center of gravity?

    <p>Moves it outward (C)</p> Signup and view all the answers

    When is a repairer allowed to move weights in helicopter blades?

    <p>Only with specific manufacturer guidance (D)</p> Signup and view all the answers

    What effect does subtracting weight have on the center of gravity?

    <p>Moves it inward (C)</p> Signup and view all the answers

    What negative consequences can arise from blades failing to track correctly?

    <p>Causes vibrations and damages parts (D)</p> Signup and view all the answers

    How can tracking weights be used to retain blade track?

    <p>By adding or shifting weights in front of and behind the feathering axis (A)</p> Signup and view all the answers

    What is a cheaper method to align rotor blades to the same plane of rotation?

    <p>Using trim tabs on the trailing edge (D)</p> Signup and view all the answers

    What is the function of a trim tab during tracking operations?

    <p>It adjusts the blade's flight altitude in the plane of rotation (A)</p> Signup and view all the answers

    Where is the trim tab typically located on a rotor blade?

    <p>Near the tip of the blade (B)</p> Signup and view all the answers

    What is one reason for adding tracking weights to helicopter blades?

    <p>To maintain a consistent tip path plane (C)</p> Signup and view all the answers

    What must happen for all rotor blades to fly in the same plane of rotation?

    <p>The trim tabs need to be adjusted correctly (C)</p> Signup and view all the answers

    What is the purpose of painting the bottom of the rotor blade black?

    <p>To prevent glare from reflecting into crew compartments (C)</p> Signup and view all the answers

    What is the purpose of blade stations?

    <p>To indicate the position of the blades relative to the mast (A)</p> Signup and view all the answers

    What is the main advantage of a single-pocket or fairing blade?

    <p>It is easier to manufacture than a multiple-pocket blade (A)</p> Signup and view all the answers

    What is the main advantage of a multiple-pocket or fairing blade?

    <p>It is easier to repair in the event of damage (C)</p> Signup and view all the answers

    What is the purpose of the internal structural components in a rotor blade?

    <p>To provide structural support for the blade skin (B)</p> Signup and view all the answers

    What is bonding in the context of rotor blade construction?

    <p>A method of joining two or more parts together using an adhesive (C)</p> Signup and view all the answers

    Which type of rotor blade is typically used on large helicopters?

    <p>Multiple-pocket or fairing blade (B)</p> Signup and view all the answers

    Study Notes

    Rotary Wing Aerodynamics

    • AVIA-1035 course
    • Focuses on rotor blade aerodynamics

    Rotor Blades

    • Design and construction vary between manufacturers, but all aim for efficiency and cost-effectiveness.
    • Helicopter design dictates specific requirements for rotor blades, influencing their design.

    Rotor Blade Design

    • Most blades are symmetrical airfoils to create a stable aerodynamic pitch.
    • Stability is ensured when the center of gravity, center of pressure, and feathering axis are aligned.
    • The constant alignment of these forces across blade pitch changes yields flight stability.

    Asymmetrical Airfoils

    • Asymmetrical airfoils are becoming more common
    • This design is capable of producing greater lift compared to symmetrical airfoils.
    • Aerodynamic stability achieved with a 3° upward angle on the trailing edge.
    • This design counteracts excessive center of pressure shifts

    Rotor Blade Materials

    • Common materials include aluminum, steel, brass, and fiberglass.
    • Initial blades often used wood, still used in some applications.
    • Metal blades were used next, followed by composite designs incorporating multiple materials.
    • Composite blades are the most recent design.

    Wooden Rotor Blades

    • First production blades employed laminated wood from various species (birch, spruce, pine, balsa).
    • A steel core was placed within the wood laminations near the leading edge for reinforcement.
    • A resin-impregnated fiberglass cloth covers the exterior surfaces.

    Wooden Blade Details

    • Two-thirds of the outboard leading edge covered with stainless steel caps for abrasion prevention.
    • Blade pairs are often a matching set for construction consistency; a single blade is not easily substituted.
    • Moisture affects wood blades; this can be mitigated by a brief helicopter run-up.

    Metal Rotor Blades (Aluminum)

    • Have been used for over 40 years.
    • Construction varies considerably among manufacturers and over time.
    • Typical blades use an extruded hollow aluminum spar forming the leading edge.
    • Quality control during construction is an advantage.

    Metal Blades - Design Details

    • Single blades can be replaced without a matched set.
    • Aluminum pockets bonded to the trailing edge help with streamlining.
    • An aluminum tip cap is fastened using screws, enhancing assembly efficiency.
    • Metal blades have a limited lifespan due to flight stresses.

    Rotor Blades - Diagrams

    • Diagrams (Figures 3-6, 3-7, 3-8, 3-9, 3-10, 3-11, 3-12, 3-13, 3-14, 3-15, 3-16, 3-17. 3-18, 3-19, 3-20, 3-21, 3-22, 3-23, and 3-24) depict blade components and construction features.

    Fiberglass/Composite Rotor Blades

    • Fiberglass is a primary material for construction.
    • The spar can be made of fiberglass or metal.
    • Roving material impregnated with epoxy resin is wound around a foam core.
    • Fiberglass cloth makes up the blade skins, providing rigidity and protection.

    Rotor/Blade Reinforcement/Additions

    • Root reinforcement plates are added to fiberglass blades.
    • Trail edge foam filler and additional roving strips to the trailing edge reinforce stability.
    • Fiber coverings that add fairing and streamline the blade.
    • The leading edge of the fiberglass blade is protected by a stainless steel strip.
    • Balancing weights are added to the blade tip during manufacturing.

    Rotor Blade - Aluminum Hollow Spar Design

    • Featured in Figure 3-7, highlighting structural details.

    Rotor Blade - Composite Roving Design

    • Depicted in Figure 3-7, showing the blade root details.

    Rotor Blade - Other Details

    • Additional protection with rubber erosion strips bonded to the underside of the blade.
    • Steel socket for attaching the blade to the rotor head.
    • Stainless steel tip caps fastened to the spar and tip pocket.
    • Internal grounding strips for static electricity transfer to the aircraft.

    Blade Nomenclature

    • The planform is the blade shape viewed from above.
    • Uniform planforms are common for easier construction.
    • Tapered planforms give better lift throughout the blade.

    Rotor Blade - Span and Span Line

    • Span is the distance from root to tip, a crucial measurement.
    • Span line is an imaginary line that runs parallel to the blade from the root to the tip.
    • Damages are often reported relative to the location on the span line.

    Rotor Blade Defects

    • Defects parallel to the span line are less critical; the chordwise stress affects the entire blade.

    Chord and Chord Line

    • Blade width measured at the widest point, the chord.
    • Chord line an imaginary line from leading to trailing edge, perpendicular to the span line.
    • Used as a reference line for angular measurement.

    Spar Construction

    • Spar, the primary support structure, is often made of aluminum, steel or fiberglass.
    • Usually D-shaped, forming the airfoil leading edge.
    • Shape varies based on material and blade design fit.

    Blade Construction - Other Components

    • Internal structural components include ribs, I-beams, spanwise channels, and aluminum honeycomb foil for strength.

    Bonding

    • Bonding methods reduce hardware needs, which usually weaken the structural bond.
    • Bonding surfaces called faying surfaces.
    • This process is not susceptible to chemical damage or many cleaning solvents.

    Blade Construction - Single Pocket

    • Uses a single, continuous skin for top and bottom construction
    • Skin wraps across the entire span and chord from behind the spar.
    • Simple design minimizes the number of joining points (pockets) or fairings during bonding.

    Blade Construction - Multiple Pocket

    • Most large-rotor blades use multiple pockets or fairings behind the spar
    • Repairs only require replacing pockets or fairings instead of the entire blade, making repairs more efficient and cost-effective.

    Blade Balance

    • Three types of balancing weights (mass chordwise, spanwise, and tracking) are used to ensure proper balance and distribution.
    • Mass balance bars are bonded to the leading edge of the blade.
    • Balance ensures that the center of gravity is about 25% of the chord.
    • Manufacturer-specific methods, shapes, and locations for balance vary.

    Blade Movement Restriction

    • Usually, helicopter blade weights are fixed and not easily repositioned or adjusted.
    • Changing weights affect the center of gravity.
    • Spanwise weights affect the center of gravity to move outward or inward.

    Blade Construction & Efficiency

    • Rotating blades should track on the same level plane for efficiency and vibration-free operation.
    • Tracking deviations cause vibrations leading to damage and reduced comfort.
    • Air turbulence caused by blade rotation also reduces performance.

    Blade Construction - Trim Tabs

    • Trim tabs are used to fine-tune the blade's position in the plane of rotation.
    • Placement is typically at the blade tip for the necessary aerodynamic reaction.

    Tail Rotor Blades

    • Tail rotor blades are used for directional control in helicopters.
    • Metal blades are built similarly to the main rotor blades with aluminum extrusions, hollow extrusions, and sheet channels.
    • Fiberglass tail rotor blades use fiberglass sheets and solid titanium spars.

    Blade Preservation and Storage

    • Maintenance instructions for rotor blade handling, storage, inspections, and documentation.
    • Condemn blades with nonrepairable damage.
    • Tape blade holes and inspect for damage.
    • Clean the blade external surfaces.
    • Protect surface areas from erosion or corrosion.
    • Secure blades and containers after cleaning and repairs.
    • Document critical information such as NSN, model, and serial number.

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