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    Kalpakjian SchmidManufacturing Engineering and Technology 2001 Prentice-Hall Page 7-1

    CHAPTER 9

    Composite Materials: Structure, GeneralProperties, and Applications

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    Kalpakjian SchmidManufacturing Engineering and Technology 2001 Prentice-Hall Page 7-2

    Application of Advanced Composite Materials

    Figure 9.1Application ofadvancedcompositematerials in

    Boeing 757-200commercialaircraft. Source:BoeingCommercialAirplaneCompany.

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    Kalpakjian SchmidManufacturing Engineering and Technology 2001 Prentice-Hall Page 7-3

    Methods of Reinforcing Plastics

    Figure 9.2 Schematicillustration of methodsof reinforcing plastics

    (matrix) with (a)particles, and (b) shortor long fibers orflakes. The four layersof continuous fibers inillustration (c) areassembled into a

    laminate structure.

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    Kalpakjian SchmidManufacturing Engineering and Technology 2001 Prentice-Hall Page 7-4

    Types and General Characteristics ofComposite Materials

    TABLE 9.1

    Material Characteristics

    Fibers

    Glass High strength, low stiffness, high density; lowest cost; E (calcium aluminoborosilicate) and S(magnesia-aluminosilicate) types commonly used.

    Graphite Available as high-modulus or high-strength; low cost; less dense than glass.

    Boron High strength and stiffness; highest density; highest cost; has tungsten filament at its center.Aramids (Kevlar) Highest strength-to-weight ratio of all fibers; high cost.

    Other fibers Nylon, silicon carbide, silicon nitride, aluminum oxide, boron carbide, boron nitride, tantalum

    carbide, steel, tungsten, molybdenum.

    Matrix materialsThermosets Epoxy and polyester, with the former most commonly used; others are phenolics,

    fluorocarbons, polyethersulfone, silicon, and polyimides.Thermoplastics Polyetheretherketone; tougher than thermosets but lower resistance to temperature.

    Metals Aluminum, aluminum-lithium, magnesium, and titanium; fibers are graphite, aluminum oxide,

    silicon carbide, and boron.

    Ceramics Silicon carbide, silicon nitride, aluminum oxide, and mullite; fibers are various ceramics.

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    Kalpakjian SchmidManufacturing Engineering and Technology 2001 Prentice-Hall Page 7-5

    Strength and Stiffness of Reinforced Plastics

    Figure 9.3 Specific tensile strength (tensile strength-to-density ratio) and specific tensile modulus(modulus of elasticity-to-density ratio) for various fibers used in reinforced plastics. Note the widerange of specific strengths and stiffnesses available.

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    Kalpakjian SchmidManufacturing Engineering and Technology 2001 Prentice-Hall Page 7-6

    Typical Properties of Reinforcing Fibers

    TABLE 9.2

    Type

    Tensile

    strength

    (MPa)

    Elastic

    modulus

    (GPa)

    Density

    ( kg/m3) Relative cost

    Boron 3500 380 2600 Highest

    Carbon

    High strength 3000 275 1900 Low

    High modulus 2000 415 1900 Low

    GlassE type 3500 73 2480 Lowest

    S type 4600 85 2540 Lowest

    Kevlar

    29 2800 62 1440 High

    49 2800 117 1440 High

    Note: These properties vary significantly depending on the material and method of preparation.

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    Kalpakjian SchmidManufacturing Engineering and Technology 2001 Prentice-Hall Page 7-7

    Fiber Reinforcing

    Figure 9.4 (a) Cross-section of a tennis racket, showing graphite and aramid (Kevlar) reinforcing fibers. Source:J. Dvorak, Mercury Marine Corporation, and F. Garrett, Wilson Sporting Goods Co. (b) Cross-section of boron

    fiber-reinforced composite material.

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    Kalpakjian SchmidManufacturing Engineering and Technology 2001 Prentice-Hall Page 7-8

    Effect of Fiber Type on Fiber-Reinforced Nylon

    Figure 9.5 The effectof type of fiber onvarious properties offiber-reinforced nylon(6,6). Source: NASA.

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    Kalpakjian SchmidManufacturing Engineering and Technology 2001 Prentice-Hall Page 7-9

    Fracture Surfaces of Fiber-Reinforced EpoxyComposites

    (a) (b)

    Figure 9.6 (a) Fracture surface of glass-fiber reinforced epoxy composite. The fibers are10 m (400 in.) in diameter and have random orientation. (b) Fracture surface of agraphite-fiber reinforced epoxy composite. The fibers, 9 m-11 m in diameter, are inbundles and are all aligned in the same direction. Source: L. J. Broutman.

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    Kalpakjian SchmidManufacturing Engineering and Technology 2001 Prentice-Hall Page 7-10

    Tensile Strength of Glass-Reinforced Polyester

    Figure 9.7 The tensile strengthof glass-reinforced polyester as afunction of fiber content andfiber direction in the matrix.Source: R. M. Ogorkiewicz, TheEngineering Properties ofPlastics. Oxford: Oxford

    University Press, 1977.

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    Kalpakjian SchmidManufacturing Engineering and Technology 2001 Prentice-Hall Page 7-11

    Example of Advanced Materials Construction

    Figure 9.8 Cross-section of acomposite sailboard, an exampleof advanced materialsconstruction. Source: K.Easterling, Tomorrows Materials

    (2d ed.), p. 133. Institute ofMetals, 1990.

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    Kalpakjian SchmidManufacturing Engineering and Technology 2001 Prentice-Hall Page 7-12

    Metal-Matrix Composite Materials andApplications

    TABLE 9.3

    Fiber Matrix Applications

    Graphite Aluminum

    Magnesium

    Lead

    Copper

    Satellite, missile, and helicopter structures

    Space and satellite structures

    Storage-battery plates

    Electrical contacts and bearings

    Boron AluminumMagnesium

    Titanium

    Compressor blades and structural supportsAntenna structures

    Jet-engine fan blades

    Alumina AluminumLead

    Magnesium

    Superconductor restraints in fission power reactorsStorage-battery plates

    Helicopter transmission structures

    Silicon carbide Aluminum, titanium

    Superalloy (cobalt-base)

    High-temperature structures

    High-temperature engine components

    Molybdenum, tungsten Superalloy High-temperature engine components