Questions and Answers
What contributed to the decreased use of non-metallic materials in early aviation?
Which of the following is an advantage of composite materials over metallic structures?
What is a primary goal when designing structures with composite materials?
How do composite structures differ from metallic structures in terms of design?
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Which materials are significant for the strength of composites?
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In what part of an aircraft are composite materials commonly utilized?
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What is one of the characteristics that composites need a different approach for compared to metals?
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Which factor is essential for the performance of composite materials in aircraft?
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What is the main benefit of using a mixture of resin and flox instead of pure resin?
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How does temperature affect the pot life and gel time of resin?
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What does maturing time refer to in resin curing?
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What is a primary advantage of using pre-measured resin packages?
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What should you do with time-expired polyester resin systems?
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What happens if you dispose of uncured polyester resin or epoxy in general waste bins?
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What is the relationship between the mix ratio and the strength of the final composite?
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What key feature do disposable cartridges for epoxy offer?
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Which factor does NOT influence the hardening time of a resin?
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What is shelf life in relation to resin products?
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What is the main function of the matrix material in a composite structure?
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Which of the following reinforcing fibres is known for its high tensile strength and flexibility?
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What is a disadvantage of using aramid fibres in composite materials?
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What is the primary advantage of carbon fibre composites over other materials?
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In which temperature range do ceramic fibres retain most of their strength?
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Which component structure can help to prevent galvanic corrosion when using carbon fibres?
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Which fibre orientation term describes the threads that run the length of the fabric?
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What characteristic of fibreglass makes it less preferable compared to other composite fibres?
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What is the purpose of fibre science in composite materials?
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What is the main purpose of identifying the warp direction in fabric?
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Which fibre orientation provides strength primarily in a single direction?
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Which of the following statements regarding fibreglass is correct?
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What is typically used to enhance the benefits of fibreglass in contemporary applications?
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Which type of resin offers high strength and light weight in structural composites?
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What characteristic distinguishes satin weave from plain weave?
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Which composite fibre is considered to be the strongest in terms of tensile strength?
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Why is the orientation of fabric important in composite materials?
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What is the angle of the bias orientation in fabric?
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Which fabric weave is commonly used in advanced composite aircraft construction?
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What material surrounds the fibre in a composite to reinforce it?
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What happens to thermosetting resins after they are cured?
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In bidirectional fabrics, which direction typically has greater strength?
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What characteristic defines the plain weave fabric style?
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Which thermoplastic is noted for its transparency and lightweight properties?
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What does the selvage edge of a fabric do?
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What type of matrix material was commonly used with fiberglass in early composite applications?
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What effect does manipulating fabric along the bias provide?
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What is the main advantage of polyester resins when used with fibreglass composites?
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What type of resin system is most commonly used in newer aircraft composites?
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What is the primary reason for refrigerating film adhesives?
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Which aspect is NOT a disadvantage of using pre-preg materials?
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What is a key characteristic of epoxy resin systems?
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Why should accelerators never be mixed directly with catalysts in polyester resin?
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What is the function of fillers in resin systems?
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What happens if pre-preg fabrics are left at room temperature for too long?
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Which filler is NOT mentioned as commonly used in composite construction?
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What is the main purpose of using adhesive foams?
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What is the effect of using polyester resin in a thicker layer compared to a thinner layer?
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What is not a correct usage of epoxy resins?
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Which of the following statements is true about micro balloons?
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How are the components of a typical epoxy resin system measured?
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Study Notes
Overview of Composite Materials in Aircraft Construction
- Non-metallic materials were significant in early aviation, but aluminium dominance reduced their usage.
- Recent advancements, primarily from space technology, have revived interest in non-metallic materials for aircraft components including fuselages and wings.
- Composite structures combine multiple materials to achieve superior strength compared to individual components.
Advantages of Composite Structures
- Composites offer excellent elastic properties, customizable strength and stiffness, and improved damage tolerance.
- High strength-to-weight ratio aims to minimize overall weight, crucial for aircraft design.
- Allows creation of complex, aerodynamic shapes that reduce drag and improve range.
Main Components of Composite Materials
- Composed of reinforcing material (fibres), matrix material (bonding), and optional core material (shape).
- The composite derives strength from the combination and arrangement of these elements.
Types of Reinforcing Fibres
- Fibreglass: Inexpensive, widely available with variable weaves; heavier and historically less strength but improvements in matrix technology enhance its utility.
- Aramid (Kevlar®): High tensile strength, lightweight, excellent toughness and vibration-damping; however, can stretch and is challenging to cut or drill.
- Carbon Fibre: Offers high compressive strength and stiffness; necessary to take precautions against galvanic corrosion when used with metals.
- Ceramic Fibre: Maintains strength at temperatures up to 1200 °C; used in high-temperature applications like space shuttle tiles.
Importance of Fibre Science
- Placement and orientation of fibres in composite materials are crucial for strength and performance.
- Customizing fibre direction in multiple layers aids in responding effectively to different stresses encountered during flight.
Fabric Orientation and Styles
- Warp: Represents threads running lengthwise, defining primary strength.
- Weft: Runs perpendicularly and interweaves with warp to create fabric strength.
- Bias: 45° angle orientation allows the fabric to assume contoured shapes.
- Types include unidirectional (fibres in one direction), bidirectional (fibres in two directions), and multi-directional (fibres in several directions).
Composite Fabric Weaves
- Plain Weave: Alternates warp and fill threads; stable and prevents yarn slippage.
- Satin Weave: Creates a smooth surface with longer warp floats; aesthetic but less stable.
- Twill Weave: Features a diagonal pattern offering good strength and flexibility across the fabric.
Composite Bonding and Matrix Systems
- Matrices transfer stress to fibres, significantly enhancing the material's structural integrity.
- Matrix types include thermoplastics (reformable with heat) and thermosetting resins (permanently solidified after curing).
Key Matrix Materials
- Polyester Resin: Early thermosetting system, primarily in non-structural applications; limited rigidity.
- Epoxy Resin: Known for high adhesion, strength, and chemical resistance; crucial for modern aircraft composites.
Adhesives and Pre-impregnated Materials
- Adhesives may be film-based or foaming, simplifying bonding processes.
- Pre-impregnated fabrics (pre-pregs) ensure proper resin saturation and mitigate mixing issues, but require strict storage conditions and have limited shelf life.
Role of Fillers and Terminology
- Fillers alter resin viscosity and enhance ease of application without compromising overall structural integrity.
- Important terms include shelf life, the duration a product remains effective; proper knowledge ensures optimal material performance and safety.### Storage and Shelf Life
- Temperature influences the shelf life of resins; proper storage conditions are crucial.
- Labels should provide detailed information regarding storage conditions and shelf life.
Pot Life and Gel Time
- Both pot life and gel time depend on catalyst activity, catalyst proportion, and ambient temperature.
- Increased air temperature reduces pot life and gel time for resins.
Hardening and Maturing Time
- Hardening time varies based on the size, thickness of the molding, and resin proportions.
- Maturing time is the period when the molding gains additional hardness, achieving maximum strength and stability eventually.
Mix Ratio
- Accurate mix ratios are critical; slight deviations can significantly affect composite strength.
- Manufacturers include mixing procedures with resin containers; these should be followed precisely.
- Pre-measured matrix packages simplify the mixing process and mitigate ratio error risks.
Packaging and Application
- Resin and catalyst in pre-packaged systems are stored separately and mixed upon use by breaking a partition.
- Thorough blending requires squeezing and kneading the package before dispensing.
- Disposable cartridges offer storage, mixing, and application convenience for two-component materials and can be customized in size.
- Proper mixing with epoxy cartridges involves breaking a seal and using a plunger for combination; specific mixing instructions are provided on labels.
Disposal Regulations
- Cured polyester resin and epoxy products must be disposed of following local regulations.
- Time-expired polyester resins are mixed with the appropriate catalyst before disposal.
- Unmixed uncured resins and catalyst-soaked rags should not be placed in general waste bins due to fire hazards.
- Consult local hazardous material agencies for proper disposal of large quantities of uncured products and catalysts.
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Description
Explore the role of composite materials in aircraft construction and how they've evolved from early aviation to today's advanced technologies. This quiz highlights the transition from traditional materials like aluminum to innovative non-metallic options that have emerged from the space program. Test your knowledge on the significance and application of these materials in modern aviation.