Non-Metallic Aircraft Materials Overview
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Questions and Answers

What is a key characteristic of whiskers in terms of their dimensions?

  • They are shorter than they are wide.
  • They are equal in length and width.
  • They have no specific dimensions.
  • They are longer than they are wide. (correct)
  • Which material is listed as a thermosetting material used in aircraft manufacturing?

  • Fiberglass
  • Reinforced plastic (correct)
  • Aluminum
  • Carbon fiber
  • What distinguishes sandwich structures from solid laminates?

  • Sandwich structures have more layers.
  • Sandwich structures are used for insulation.
  • Sandwich structures contain a core. (correct)
  • Sandwich structures are heavier.
  • What property of reinforced plastic contributes to its utility in aircraft?

    <p>Resistance to mildew and rot.</p> Signup and view all the answers

    How is a solid laminate constructed?

    <p>By wet laminating three or more layers of resin impregnated cloths.</p> Signup and view all the answers

    In what order are the materials listed from least to most commonly used?

    <p>Reinforced plastic, whiskers, fibers.</p> Signup and view all the answers

    What is one advantage of using sandwich-type laminates?

    <p>They provide equal strength with less weight.</p> Signup and view all the answers

    Which of the following is NOT a feature of reinforced plastic?

    <p>Resistance to fire.</p> Signup and view all the answers

    What is the primary benefit of using bidirectional fabrics in aerospace structures?

    <p>They reduce the overall weight of the structure.</p> Signup and view all the answers

    How are unidirectional prepreg tapes created?

    <p>By impregnating raw dry strands with thermosetting resins.</p> Signup and view all the answers

    What characterizes rovings in composite materials?

    <p>All filaments are aligned in the same direction and are not twisted.</p> Signup and view all the answers

    What process is commonly used to create bidirectional fabrics?

    <p>Solution or hot melt resin impregnation.</p> Signup and view all the answers

    What is a characteristic of a plain weave fabric?

    <p>Fibers alternate over and under each intersecting strand.</p> Signup and view all the answers

    What is the function of warp clocks in composite fabrication?

    <p>To show the fiber directions.</p> Signup and view all the answers

    Which fiber form is characterized by having high strength in one direction but minimal strength across fibers?

    <p>Unidirectional tape.</p> Signup and view all the answers

    What distinguishes a satin weave from a plain weave?

    <p>It allows for greater flexibility in fiber orientation.</p> Signup and view all the answers

    What is the primary advantage of advanced composite materials in aerospace applications?

    <p>High strength and low weight</p> Signup and view all the answers

    Which type of sealant requires mixing a base compound and an accelerator?

    <p>Two-part sealant</p> Signup and view all the answers

    What is the primary purpose of using laminated structures in composite materials?

    <p>To enhance strength and stiffness</p> Signup and view all the answers

    What modification can be made to one-part sealants before use?

    <p>Adjust consistency with a thinner</p> Signup and view all the answers

    Which component is typically found in advanced composites to improve their properties?

    <p>Fibrous materials</p> Signup and view all the answers

    In which areas of aircraft are advanced composite materials primarily applied?

    <p>Fairings, spoilers, and flight controls</p> Signup and view all the answers

    What is commonly a characteristic of two-part sealants compared to one-part sealants?

    <p>They require careful measuring for mixing</p> Signup and view all the answers

    Why is specialized knowledge required for repairing modern composite structures?

    <p>They require specific tools and techniques</p> Signup and view all the answers

    What is a primary characteristic of Thiokol, or polysulfide rubber?

    <p>Excellent resistance to deterioration</p> Signup and view all the answers

    Which of the following synthetic rubbers is known for excellent heat stability and flexibility?

    <p>Silicone rubbers</p> Signup and view all the answers

    What is a limitation of silicone rubbers when used in aviation applications?

    <p>Adverse reaction to aromatic and nonaromatic gasoline</p> Signup and view all the answers

    What is Silastic primarily used for in aircraft?

    <p>Insulation of electrical equipment</p> Signup and view all the answers

    In which application are sealing compounds primarily used?

    <p>Preventing weather-related corrosion</p> Signup and view all the answers

    Which of the following properties does NOT characterize Thiokol?

    <p>High elasticity</p> Signup and view all the answers

    What temperature range can silicone rubbers withstand?

    <p>-150°F to 600°F</p> Signup and view all the answers

    What is a significant disadvantage of using silicone rubbers in certain fuel systems?

    <p>Reactivity to certain types of gasoline</p> Signup and view all the answers

    What is a primary disadvantage of using Kevlar fibers in applications?

    <p>Weakness in compression</p> Signup and view all the answers

    Which type of fiberglass is known for its structural strength?

    <p>S-glass</p> Signup and view all the answers

    What is a characteristic of nonwoven fabrics compared to woven fabrics?

    <p>Fibers are held in place by stitching</p> Signup and view all the answers

    What application is fiberglass commonly used in?

    <p>Secondary aircraft structures</p> Signup and view all the answers

    Which fiber type is specifically designed for lightning protection?

    <p>Lightning Protection Fibers</p> Signup and view all the answers

    What is a typical use for Carbon/Graphite fibers?

    <p>High-performance sporting goods</p> Signup and view all the answers

    What is a weakness associated with aramid fibers such as Kevlar?

    <p>High hygroscopy</p> Signup and view all the answers

    Which statement is true regarding the fabric properties of knitted or stitched fabrics?

    <p>They can enhance interlaminar shear and toughness</p> Signup and view all the answers

    Study Notes

    Non-Metallic Aircraft Materials

    • Composite materials are strong and stiff, but they are heavy.
    • Laminated structures can be made with or without a core.
    • Sandwich structures have a core center, which makes them equally strong but lighter.

    Reinforced Plastic

    • Reinforced plastic is used in the manufacture of radomes, antenna covers, wingtips, and insulation for electrical equipment and fuel cells.
    • It has excellent dielectric characteristics, high strength-to-weight ratio, resistance to mildew, rust, and rot, and ease of fabrication.
    • It is formed from either solid laminates or sandwich-type laminates.
    • Solid laminates consist of three or more layers of resin-impregnated cloths "wet laminated" together to form a solid sheet facing or molded shape.
    • Sandwich-type laminates consist of two or more solid sheet facings or molded shapes enclosing a fiberglass honeycomb or foam-type core.

    Synthetic Rubber

    • Thiokol (polysulfide rubber) offers excellent resistance to deterioration and chemicals like petroleum and gasoline but has low physical properties, including tensile strength, elasticity, and tear abrasion resistance.
    • It is commonly used in oil hoses, tank linings for aromatic aviation gasolines, gaskets, and seals.
    • Silicone rubbers are made from silicon, oxygen, hydrogen, and carbon. They offer excellent heat stability and flexibility across a wide temperature range from -150°F to 600°F, making them ideal for gaskets and seals.
    • Silastic is a well-known silicone used to insulate electrical and electronic equipment due to its excellent dielectric properties across a wide temperature range. It remains flexible without cracking and is also used for gaskets and seals in specific oil systems.

    Sealing Compounds

    • Aircraft areas are sealed to withstand pressurization, prevent fuel leaks, block fumes, and protect against weather-related corrosion.
    • Sealants typically involve multiple ingredients, with some requiring mixing before use, while others are ready to apply straight from the package.
    • One-part sealants are pre-prepared by the manufacturer and ready to use, though their consistency can be adjusted with a manufacturer-recommended thinner if needed.
    • Two-part sealants require separate packaging of a base compound and an accelerator, which must be mixed in prescribed ratios, typically equal by weight, to ensure proper curing and material quality.

    Advanced Composite Materials

    • Advanced composite materials are increasingly used in aerospace structures for their weight savings compared to aluminum.
    • They have applications including fairings, spoilers, and flight controls developed since the 1960s.
    • Modern large aircraft feature composite fuselage and wing structures, which require specialized knowledge for repair.
    • Their primary advantages are high strength, low weight, and corrosion resistance.

    Laminated Structures

    • Composite materials combine distinct components to achieve superior structural properties, with individual materials remaining physically identifiable.
    • Advanced composites typically consist of fibrous materials embedded in a resin matrix, laminated with fibers oriented in alternating directions for enhanced strength and stiffness.
    • Plain weave fabric is a common type of fabric used in composite structures.

    Fiber Orientation

    • Quasi-isotropic layups use a combination of orientations to mimic isotropic properties.
    • Warp clocks are used to indicate fiber directions, with the default orientation assumed if the clock is not provided.

    Fiber Forms

    • Composite materials typically start with spooled unidirectional raw fibers, where individual fibers are called filaments, and bundles are known as tows, yarns, or rovings.
    • Fibers can be supplied as dry fiber requiring resin impregnation or as prepreg materials with pre-applied resin.
    • Rovings have all filaments in the same direction and are not twisted.
    • Unidirectional (Tape) prepreg tapes are commonly used in aerospace and are made by impregnating raw dry strands with hot melted thermosetting resins through heat and pressure. Tape products have high strength in the fiber direction and virtually no strength across the fibers.
    • Bidirectional (Fabric) fabrics offer greater flexibility for the layup of complex shapes compared to unidirectional tapes. They can be impregnated with resin through solution or hot melt processes. Tightly woven fabrics are usually the choice in aerospace structures to save weight, minimize resin void size, and maintain fiber orientation during the fabrication process.
    • Plain weave is a type of bidirectional fabric where each fiber alternates over and then under each intersecting strand.
    • Satin weave is a type of bidirectional fabric where fiber bundles traverse both in warp and fill directions, changing the over/under position less frequently.
    • Nonwoven (Knitted or Stitched) fabrics provide many benefits similar to unidirectional tapes, where fibers are held in place by stitching with fine yarns or threads rather than weaving. These fabrics offer versatile multi-ply orientations and may enhance interlaminar shear and toughness properties, although they may add some weight and slightly reduce ultimate reinforcement fiber properties.

    Types of Fiber

    • Fiberglass is used in secondary aircraft structures and helicopter rotor blades.
    • E-glass is used for electrical applications because it has high resistance to current flow.
    • S-glass is used for structural strength.
    • Kevlar® aramid fibers are yellow, lightweight, strong, and tough, making them ideal for impact-prone areas.
    • Kevlar® 49 has high stiffness.
    • Kevlar® 29 has lower stiffness.
    • Carbon/Graphite fibers both stem from graphene (hexagonal) layer networks in carbon.

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    AVI III Lesson 4-1 PDF

    Description

    This quiz covers various non-metallic materials used in aircraft construction, including composite materials, reinforced plastics, and synthetic rubber. Explore the properties and applications of these materials, focusing on their strength, weight, and fabrication characteristics. Test your knowledge on the benefits and uses of laminated and sandwich structures as well.

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