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Composite Materials Fundamental questions

Composite Materials Fundamental questions. How do composite materials differ from other engineering materials? What are the constituent materials, and how do their properties compare? How do the properties of the composite depend on the type, amount and arrangement of the constituents?

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Composite Materials Fundamental questions

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  1. Composite MaterialsFundamental questions • How do composite materials differ from other engineering materials? • What are the constituent materials, and how do their properties compare? • How do the properties of the composite depend on the type, amount and arrangement of the constituents? • How are composite products made, and why does manufacture affect quality?

  2. Fibres have better stiffness and strength compared to bulk materials • Atomic or molecular alignment(carbon, aramid) • Removal of flaws and cracks (glass) • Strain hardening (metals)

  3. Most reinforcing fibres are brittle (elastic to failure) Hollaway (ed), Handbook of Polymer Composites for Engineers

  4. Types of Natural Fibre • Bast fibres (flax, hemp, jute, kenaf…)- wood core surrounded by stem containing cellulose filaments • Leaf fibres (sisal, banana, palm) • Seed fibres (cotton, coconut (coir), kapok)

  5. TNO Centre for Lightweight Structures

  6. Advantagesof Natural Fibres High specific properties (low density). A renewable resource; production requires relatively little energy Crops are sink for CO2, returning oxygen to atmosphere. Low investment and low cost production. Low tooling wear. Better working conditions, no skin irritation. Thermal recycling possible. Good thermal and acoustic insulating properties.

  7. Disadvantagesof Natural Fibres Low strength, especially impact strength. Variable quality (e.g. weather dependent). Moisture absorption, which causes swelling of the fibres. Limited maximum processing temperature. Lower durability (potential for improvement through fibre treatments). Poor fire resistance. Price fluctuation (harvest results or agricultural politics). Irregular fibre lengths (spinning is required to obtain continuous yarns).

  8. Structures cannot be made from fibres alone - the high properties of fibres are not realisable in practice A matrix is required to: • hold reinforcement in correct orientation • protect fibres from damage • transfer loads into and between fibres

  9. COMPOSITES - A FORMAL DEFINITION(Hull, 1981) 1. Consist of two or more physically distinct and mechanically separable parts.

  10. Polymer matrix composite combinations Matrix epoxypolyimidepolyesterthermoplastics (PA, PS, PEEK…) Fibre E-glassS-glasscarbon (graphitearamid (eg Kevlar)boron

  11. Ceramic matrix composite combinations Matrix SiCaluminaglass-ceramicSiN Fibre SiCaluminaSiN

  12. Metal matrix composite combinations Matrix aluminiummagnesiumtitaniumcopper Fibre boronBorsiccarbon (graphite)SiCalumina (Al2O3)

  13. Composite property might be only 10% of the fibre property:

  14. Some typical polymer composite properties

  15. Concrete - hard particles (gravel) + cement (ceramic/ceramic composite). Properties determined by particle size distribution, quantity and matrix formulation Additives and fillers in polymers: carbon black (conductivity, wear/heat resistance) aluminium trihydride (fire retardancy) glass or polymer microspheres (density reduction) chalk (cost reduction) Cutting tool materials and abrasives (alumina, SiC, BN bonded by glass or polymer matrix; diamond/metal matrix) Electrical contacts (silver/tungsten for conductivity and wear resistance) Cast aluminium with SiC particles Examples of particulate composites

  16. COMPOSITES - A FORMAL DEFINITION(Hull, 1981) 1. Consist of two or more physically distinct and mechanically separable parts. 2. Constituents can be combined in a controlled way to achieve optimum properties.

  17. Examples of natural composites

  18. COMPOSITES - A FORMAL DEFINITION(Hull, 1981) 1. Consist of two or more physically distinct and mechanically separable parts. 2. Constituents can be combined in a controlled way to achieve optimum properties. 3. Properties are superior, and possibly unique, compared those of the individual components

  19. Addition of properties: GLASS + POLYESTER = GRP (strength) (chemical resistance) (strength and chemical resistance) Unique properties: GLASS + POLYESTER = GRP (brittle) (brittle) (tough!)

  20. Aerospace, defence, F1… Highly stressed Glass, carbon, aramid fibres Honeycomb cores Epoxy, bismaleimide… Prepregs Vacuum bag/oven/autoclave Highly tested and qualified materials Marine, building… Lightly stressed Glass (random and woven) Foam cores Polyester, vinylester… Wet resins Hand lay up, room temperature cure Limited range of lower performance materials ADVANCED COMPOSITES vs REINFORCED PLASTICS

  21. Why are composites used in engineering? • Weight saving (high specific properties) • Corrosion resistance • Fatigue properties • Manufacturing advantages:- reduced parts count- novel geometries- low cost tooling • Design freedoms- continuous property spectrum- anisotropic properties

  22. Anisotropic properties - fibres can be aligned in load directions to make the most efficient use of the material

  23. The ability to vary fibre content and orientation results in a spectrum of available properties

  24. Why aren’t composites used more in engineering? • High cost of raw materials • Lack of design standards • Few ‘mass production’ processes available • Properties of laminated composites:- low through-thickness strength- low interlaminar shear strength • No ‘off the shelf’ properties - performance depends on quality of manufacture

  25. There are no ‘off the shelf’ properties with composites. Both the structure and the material are made at the same time. Material quality depends on quality of manufacture.

  26. Poor quality - low fibre content, high void content Good quality - high fibre content, ‘zero’ void content

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