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Ch 1: Engineering materials


 Dr. Zuhailawati Hussain
        EBB 224
   Design of Materials
      Engineering

                              1
Metal / Metallic materials
• Classifications & Specifications of Metallic Materials
• Major characteristics of metallic materials are
  crystallinity, conductivity to heat and electricity and
  relatively high strength & toughness.
• Classification: systematic arrangement or division of
  materials into group on the basis of some common
  characteristic
• Generally classified as ferrous and nonferrous
        Ferrous materials-iron as the base metal,
        • range from plain carbon (>98% Fe) to high
            alloy steel (<50% alloying elements)
        Nonferrous materials consist of the rest of the
        metals and alloys
            Eg. Aluminum, magnesium, titanium & their  2
            alloys
• Within each group of alloy, classification can be
  made according
    (a) chemical composition, e.g. carbon content or
    alloys content in steels;
    (b) finished method, e.g. hot rolled or cold
    rolled;
    (c) product form, e.g. bar, plate, sheet, tubing,
    structural shape;
    (d) method of production, e.g. cast, wrought
    alloys.




                                                  3
Designation: identification of each class by a
number, letter, symbol, name or a combination.
Normally based on chemical composition or
mechanical properties.
 Example : Table 2.1 designation systems for steel
System used by AISI & SAE: 4, or 5 digits which
designate the alloy composition.
• 1st two digits indicate Alloy system
• Last two or three digits nominal carbon content
   in hundredths of a percent




                                              4
5
In most eng. application, selection of metallic is usually
based on the following considerations:
1) Product shape: a) sheet, strip, plate, (b) bar, rod, wire,
   (c) tubes, (d) forging (e) casting
2) Mechanical properties-tensile, fatigue, hardness,
   creep,impact test
3) Physical & chemical properties-specific gravity, thermal
   & electrical conductivity, thermal expansion
4) Metallurgical consideration-anisotrophy of properties,
   hardenability of steel, grain size & consistency of
   properties
5) Processing castability-castability, formability,
   machinability
6) Sales appeal-color, luster
7) Cost & availability

                                                        6
Design and selection for metals
  One of the major issues for structural components
  is deflection under service load.
      A function of the applied forces and geometry,
      and also stiffness of material.
      Stiffness of material is difficult to change,
      either shape or the material has to be changed
      if order to achieve a large change in the
      stiffness of a component.




                                                7
• Load carrying capacity of component can be related
  to the yield strength, fatigue strength or creep
  strength depending on loading & service condition.
      All are structure sensitive.
     Changed by changing chemical composition of the
     alloy, method and condition of manufacturing, as
     well as heat treatment
     Increasing the strength cause metal ductility &
     toughness to decrease which affects the
     performance of component.




                                                  8
Electrical & thermal conductivities
     Thermal conductivity, K
     •   Is measure of the rate at which heat is
         transferred through a material
    Al & Cu- Manufacture of component where
    electrical conductivity is primary requirement
• Corrosion resistance & specific gravity limits
  the materials.




                                                   9
Manufacturing consideration
  Majority of metallic components are wrought or cast
  Wrought m/str:
  • usually stronger and more ductile than cast.
  • Available in many shapes & size tolerance
  Hot worked products:
  • Tolerance are wider thus difficult for automatic
     machining
  • Poor surface quality, esp. in sheet/wire drawing
  Cold worked product:
  Narrow tolerance
  Residual stress cause unpredictable size change during
  machining

                                                   10
Weldability – a function of material composition.
So structure involve welding of the components
need to consider. Also for other joining means.
Machinability:
• Important if large amounts of material have
  to be removed
• improvement by heat treatment or alloying
  elements
Economic aspects:
   material able to perform function at lowest
  cost
  Plain carbon steel & cast iron are the least
                                            11
  expensive
Design for polymer
• Classifications of Polymers
• Polymer – low density, good thermal & electrical
  insulation, high resistance to most chemicals and
  ability to take colours and opacities.
• But unreinforced bulk polymer are mechanically
  weaker, lower elastic moduli & high thermal
  expansion coefficients.
• Improvement           Reinforced variety of fibrous
  materials        Composites (PMC).




                                                 12
Advantages : ease of manufacturing & versatility.
  • Can manufacture into complicated shapes in one
     step with little need for further processing or
     surface treatment.
  • Versatility : ability to produce accurate
     component, with excellent surface finish and
     attractive color, at low cost and high speed
• Application: automotive, electrical & electronic
  products, household appliance, toys, container,
  packaging, textiles
• Basic manufacturing processes for polymer parts
  are extrusion, molding, casting and forming of
  sheet.
                                                13
Thermoset & thermoplastic
  • Differ in the degree of their inter-molecular
     bonding
  • Thermoplastic-litle cross bonding between
     polymer, soften when heated & harden when
     cooled
  • Thermoset-strong intermolecular bonding which
     prevents fully cured materials from softening
     when heated
• Rubber are similar to plastic in structure and the
  difference is largely based on the degree of
  extensibility or stretching.

                                               14
Design consideration for polymer
  Structural part/When the parts is to carry load
    •Should remember the strength and stiffness
    of plastics vary with temperature.
    •Troom data cannot be used in design calculation if
    the part will be used at other temp.
  Long term properties cannot be predicted from
 short term prop. Eg. Creep behavior
  Engineering plastics are britle (notched impact
 strength < 5.4 J/cm)
     Avoid stress raiser
                                                  15
Design for ceramics
• Classification of Ceramic Materials
• Ceramics – inorganic compounds of one or more metals
  with a nonmetallic element. Eg Al2O3, SiC, Si2N3.
     Crystal structure of ceramic are complex
     • They accommodate more than one element of
        widely different atomic size.
     The interatomic forces generally alternate
     between ionic & covalent which leave few free
     electrons
     • usually heat & electrical insulators.
     Strong ionic & covalent bonds give high hardness,
     stiffness & stability (thermal & hostile env.).

                                                 16
Structure:
(1) Amorphous or glass-short range order, (2)
 crystalline (long range order) & (3) crystalline
 material bonded by glassy matrix.
 Clasiification:
 • Whitewares, glass, refractories, structural clay
    products & enamels.
 Characteristics:
    Hard & brittleness,
    low mechanical & thermal shock
    High melting points
    Thermal conductivities between metal & polymer

                                              17
Design consideration for ceramics
  Britle, low mechanical & thermal shock-need special
  consideration
  Ratio between tensile strength, modulus of rupture &
  compressive strength ~ 1:2:10. In design, load ceramic
  parts in compression & avoid tensile loading
  Sensitive to stress concentration
  • Avoid stress raiser during design.
  Dimensional change take place during drying and firing,
  should be consider
  Large flat surface can cause wrapping
  Large changes in thickness of product can lead to
  nonuniform drying and cracking.
  Dimensional tolerances should be generous to avoid
  machining
                                                   18
Design for composite

Introduction
   A composite material can be broadly defined as
   an assembly two or more chemically distinct
   material, having distinct interface between them
   and acting to produce desired set of properties
   • Composites – MMC, PMC & CMC.
   The composite constituent divided into two
   • Matrix
   • Structural constituent / reinforcement



                                                19
Properties / behavior depends on properties, size
& distribution, volume fraction & shape of the
constituents, & the nature and strength of bond
between constituents.
Mostly developed to improve mechanical
properties i.e strength, stiffness, creep
resistance & toughness.
Three type of composite
   (1) Dispersion-strengthened,
   (2) Reinforcement – continuous & discontinuous
   (3) Laminated (consist more than 2 layers
   bonded together).
                                             20
21
Designing with composite
  A composite materials usually are more expensive on
  a cost.
  Used when weight saving is possible when the
  relevant specific property (property/density) of the
  composite is better than conventional material
  • E.g. specific strength (strength/density), specific
     elastic modulus ( elastic modulus/density)
  Efficient use of composite can be achieved by
  tailoring the material for the application
     E.g., to achieve max. strength in one direction in a
     fibrous composite, the fibers should be well
     aligned in that direction
                                                   22
If composite is subjected to tensile loading,
     important design criterion is the tensile
     strength in the loading direction
     Under compression loading, failure by buckling
     become important
• Fatigue behavior:
     Steel- show an endurance limit or a stress
     below which fatigue does not occur
     Composite-fatigue at low stress level because
     fibrous composites may have many crack, which
     can be growing simultaneously and propagate
     through the matrix

                                               23

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materials eng

  • 1. Ch 1: Engineering materials Dr. Zuhailawati Hussain EBB 224 Design of Materials Engineering 1
  • 2. Metal / Metallic materials • Classifications & Specifications of Metallic Materials • Major characteristics of metallic materials are crystallinity, conductivity to heat and electricity and relatively high strength & toughness. • Classification: systematic arrangement or division of materials into group on the basis of some common characteristic • Generally classified as ferrous and nonferrous Ferrous materials-iron as the base metal, • range from plain carbon (>98% Fe) to high alloy steel (<50% alloying elements) Nonferrous materials consist of the rest of the metals and alloys Eg. Aluminum, magnesium, titanium & their 2 alloys
  • 3. • Within each group of alloy, classification can be made according (a) chemical composition, e.g. carbon content or alloys content in steels; (b) finished method, e.g. hot rolled or cold rolled; (c) product form, e.g. bar, plate, sheet, tubing, structural shape; (d) method of production, e.g. cast, wrought alloys. 3
  • 4. Designation: identification of each class by a number, letter, symbol, name or a combination. Normally based on chemical composition or mechanical properties. Example : Table 2.1 designation systems for steel System used by AISI & SAE: 4, or 5 digits which designate the alloy composition. • 1st two digits indicate Alloy system • Last two or three digits nominal carbon content in hundredths of a percent 4
  • 5. 5
  • 6. In most eng. application, selection of metallic is usually based on the following considerations: 1) Product shape: a) sheet, strip, plate, (b) bar, rod, wire, (c) tubes, (d) forging (e) casting 2) Mechanical properties-tensile, fatigue, hardness, creep,impact test 3) Physical & chemical properties-specific gravity, thermal & electrical conductivity, thermal expansion 4) Metallurgical consideration-anisotrophy of properties, hardenability of steel, grain size & consistency of properties 5) Processing castability-castability, formability, machinability 6) Sales appeal-color, luster 7) Cost & availability 6
  • 7. Design and selection for metals One of the major issues for structural components is deflection under service load. A function of the applied forces and geometry, and also stiffness of material. Stiffness of material is difficult to change, either shape or the material has to be changed if order to achieve a large change in the stiffness of a component. 7
  • 8. • Load carrying capacity of component can be related to the yield strength, fatigue strength or creep strength depending on loading & service condition. All are structure sensitive. Changed by changing chemical composition of the alloy, method and condition of manufacturing, as well as heat treatment Increasing the strength cause metal ductility & toughness to decrease which affects the performance of component. 8
  • 9. Electrical & thermal conductivities Thermal conductivity, K • Is measure of the rate at which heat is transferred through a material Al & Cu- Manufacture of component where electrical conductivity is primary requirement • Corrosion resistance & specific gravity limits the materials. 9
  • 10. Manufacturing consideration Majority of metallic components are wrought or cast Wrought m/str: • usually stronger and more ductile than cast. • Available in many shapes & size tolerance Hot worked products: • Tolerance are wider thus difficult for automatic machining • Poor surface quality, esp. in sheet/wire drawing Cold worked product: Narrow tolerance Residual stress cause unpredictable size change during machining 10
  • 11. Weldability – a function of material composition. So structure involve welding of the components need to consider. Also for other joining means. Machinability: • Important if large amounts of material have to be removed • improvement by heat treatment or alloying elements Economic aspects: material able to perform function at lowest cost Plain carbon steel & cast iron are the least 11 expensive
  • 12. Design for polymer • Classifications of Polymers • Polymer – low density, good thermal & electrical insulation, high resistance to most chemicals and ability to take colours and opacities. • But unreinforced bulk polymer are mechanically weaker, lower elastic moduli & high thermal expansion coefficients. • Improvement Reinforced variety of fibrous materials Composites (PMC). 12
  • 13. Advantages : ease of manufacturing & versatility. • Can manufacture into complicated shapes in one step with little need for further processing or surface treatment. • Versatility : ability to produce accurate component, with excellent surface finish and attractive color, at low cost and high speed • Application: automotive, electrical & electronic products, household appliance, toys, container, packaging, textiles • Basic manufacturing processes for polymer parts are extrusion, molding, casting and forming of sheet. 13
  • 14. Thermoset & thermoplastic • Differ in the degree of their inter-molecular bonding • Thermoplastic-litle cross bonding between polymer, soften when heated & harden when cooled • Thermoset-strong intermolecular bonding which prevents fully cured materials from softening when heated • Rubber are similar to plastic in structure and the difference is largely based on the degree of extensibility or stretching. 14
  • 15. Design consideration for polymer Structural part/When the parts is to carry load •Should remember the strength and stiffness of plastics vary with temperature. •Troom data cannot be used in design calculation if the part will be used at other temp. Long term properties cannot be predicted from short term prop. Eg. Creep behavior Engineering plastics are britle (notched impact strength < 5.4 J/cm) Avoid stress raiser 15
  • 16. Design for ceramics • Classification of Ceramic Materials • Ceramics – inorganic compounds of one or more metals with a nonmetallic element. Eg Al2O3, SiC, Si2N3. Crystal structure of ceramic are complex • They accommodate more than one element of widely different atomic size. The interatomic forces generally alternate between ionic & covalent which leave few free electrons • usually heat & electrical insulators. Strong ionic & covalent bonds give high hardness, stiffness & stability (thermal & hostile env.). 16
  • 17. Structure: (1) Amorphous or glass-short range order, (2) crystalline (long range order) & (3) crystalline material bonded by glassy matrix. Clasiification: • Whitewares, glass, refractories, structural clay products & enamels. Characteristics: Hard & brittleness, low mechanical & thermal shock High melting points Thermal conductivities between metal & polymer 17
  • 18. Design consideration for ceramics Britle, low mechanical & thermal shock-need special consideration Ratio between tensile strength, modulus of rupture & compressive strength ~ 1:2:10. In design, load ceramic parts in compression & avoid tensile loading Sensitive to stress concentration • Avoid stress raiser during design. Dimensional change take place during drying and firing, should be consider Large flat surface can cause wrapping Large changes in thickness of product can lead to nonuniform drying and cracking. Dimensional tolerances should be generous to avoid machining 18
  • 19. Design for composite Introduction A composite material can be broadly defined as an assembly two or more chemically distinct material, having distinct interface between them and acting to produce desired set of properties • Composites – MMC, PMC & CMC. The composite constituent divided into two • Matrix • Structural constituent / reinforcement 19
  • 20. Properties / behavior depends on properties, size & distribution, volume fraction & shape of the constituents, & the nature and strength of bond between constituents. Mostly developed to improve mechanical properties i.e strength, stiffness, creep resistance & toughness. Three type of composite (1) Dispersion-strengthened, (2) Reinforcement – continuous & discontinuous (3) Laminated (consist more than 2 layers bonded together). 20
  • 21. 21
  • 22. Designing with composite A composite materials usually are more expensive on a cost. Used when weight saving is possible when the relevant specific property (property/density) of the composite is better than conventional material • E.g. specific strength (strength/density), specific elastic modulus ( elastic modulus/density) Efficient use of composite can be achieved by tailoring the material for the application E.g., to achieve max. strength in one direction in a fibrous composite, the fibers should be well aligned in that direction 22
  • 23. If composite is subjected to tensile loading, important design criterion is the tensile strength in the loading direction Under compression loading, failure by buckling become important • Fatigue behavior: Steel- show an endurance limit or a stress below which fatigue does not occur Composite-fatigue at low stress level because fibrous composites may have many crack, which can be growing simultaneously and propagate through the matrix 23