Joining of Composites

Embed Size (px)

Citation preview

  • 7/28/2019 Joining of Composites

    1/44

    JOININGOFCOMPOSITEMATERIALS

    AND TYPESOFADHESIVES

    LTFYE ETN2008286011

  • 7/28/2019 Joining of Composites

    2/44

  • 7/28/2019 Joining of Composites

    3/44

    http://www.youtube.com/watch?v=HOjy_bRyUh0

    http://www.youtube.com/watch?v=HOjy_bRyUh0http://www.youtube.com/watch?v=HOjy_bRyUh0http://www.youtube.com/watch?v=HOjy_bRyUh0http://www.youtube.com/watch?v=HOjy_bRyUh0http://www.youtube.com/watch?v=HOjy_bRyUh0http://www.youtube.com/watch?v=HOjy_bRyUh0http://www.youtube.com/watch?v=HOjy_bRyUh0http://www.youtube.com/watch?v=HOjy_bRyUh0
  • 7/28/2019 Joining of Composites

    4/44

  • 7/28/2019 Joining of Composites

    5/44

  • 7/28/2019 Joining of Composites

    6/44

  • 7/28/2019 Joining of Composites

    7/44

  • 7/28/2019 Joining of Composites

    8/44

  • 7/28/2019 Joining of Composites

    9/44

  • 7/28/2019 Joining of Composites

    10/44

    Adhesion is defined as the adhesive force acting betweenthe adhesive and the surface ofthe material. This force is the result of the mechanicalinterlocking between adhesiveand the material surface roughness (mechanical

    adhesion) as well as the physical and/orchemical interaction between the adhesive and thematerial (specific adhesion).Cohesion is the strength of the adhesive itself. This is a result

    of the mechanicalentangling and interlocking of the adhesive moleculesand their physical and/orchemical affinity for each other

  • 7/28/2019 Joining of Composites

    11/44

  • 7/28/2019 Joining of Composites

    12/44

  • 7/28/2019 Joining of Composites

    13/44

  • 7/28/2019 Joining of Composites

    14/44

  • 7/28/2019 Joining of Composites

    15/44

    This theory explains adhesive attraction forces in terms ofelectrostatic effects at an interface.This is based on the phenomenon of a electrical double

    layer formed at the junction of twomaterials. At any boundary an electrical double layer isproduced and the consequentcoulombic attraction might account for the adhesionand resistance to separation.

  • 7/28/2019 Joining of Composites

    16/44

    In this theory adhesion is attributed tointermolecular entanglements at the interface.

    This is applied to the union of high polymers. The

    fundamental concept is that adhesion

    arises through the interdiffusion of theadherend and the adhesive. It is based upon

    the chain

    nature of the structure with the consequent

    flexibility and the ability of the chains to

    undergo

    Brownian movements on a sub-molecular

    scale.

  • 7/28/2019 Joining of Composites

    17/44

    When the adhesive is applied in solution

    (most probably) and if the adherend is

    sensibly soluable in the solvent the substrate

    molecules will also diffuse to an appreciable

    extent into the adhesive layer. Overall the

    clean-cut boundary between the adherend

    and the adhesive disappears and is replacedby a

    layer representing a gradual transition from

    one polymer to the other. A major difference

    inthis theory is that it implies a three dimensional

    volume process rather than a two

    dimensional surface process.

  • 7/28/2019 Joining of Composites

    18/44

    Adhesive joints are composite systems

    whose strength depends on both the

    geometrical

    design and loading type as well as on theschematically illustrated individual strengths

    of the components to be joint, the adhesive

    and the interface layer.

    As in every composite system consisting ofdifferent members, the overall strength is

    limited by the weakest member

  • 7/28/2019 Joining of Composites

    19/44

  • 7/28/2019 Joining of Composites

    20/44

    The intermolecular bonds (secondary valency

    bonds) act between the adhesive

    molecules as well as between adhesive and

    the surfaces of the joining parts and are thusrelevant for the cohesion and adhesion

    strength

  • 7/28/2019 Joining of Composites

    21/44

  • 7/28/2019 Joining of Composites

    22/44

    Numerous adhesives contain polar molecule

    groups (dipoles) which have a strong

    polarising action on the metallic joining parts,

    the latter being non-polar in themselves.The dipole forces can operate effectively

    only if these molecule groups can approach

    to

    within about 0.1 mm of the surface of thejoining parts Theabove

    is only possible if the adhesive can wet the

    solid surfaces optimally

  • 7/28/2019 Joining of Composites

    23/44

  • 7/28/2019 Joining of Composites

    24/44

    Hydrogen bonds are a special form of

    intermolecular bonds. These are, for example,

    responsible for the relatively high cohesion

    strengths of PUR and PA adhesives

    Hydrogen bonds can also be formed between

    adhesives and solid surfaces when thelatter are oxidised or contain adsorbed

    hydrogen molecules.

  • 7/28/2019 Joining of Composites

    25/44

  • 7/28/2019 Joining of Composites

    26/44

    Adhesives can be classified into three main

    types given below. There are of course several

    products that are combinations of these threetypes but essentially all adhesives can be

    grouped into these categories.

  • 7/28/2019 Joining of Composites

    27/44

    Basically an adhesive of this type is supplied in a

    low molecular weight form and after

    application a polymerisation reaction is allowed

    to take place. This polymerisation can beachieved by:

  • 7/28/2019 Joining of Composites

    28/44

    Two component pack:

    Supply the produce as a two component pack, i.e.base plus hardener. Examples of this type

    are: Epoxy adhesives based on epichlorhydrin bisphenol.

    Cured with amines or polyamide. Phenolics adhesives i.e. a novalac type with

    hexamethylene tetramine. Unsaturated polyesters using an organic peroxide,

    i.e. M.E.K. peroxide and cobalt naphthenate. Polysulfide with lead dioxide or an isocyanate.

    Polyurethanes with isocyanate. Silicone polymers utilising a metal salt of' an organic

    acid, e.g. lead octoate. Reactive acrylics - rely on peroxides or amines.

  • 7/28/2019 Joining of Composites

    29/44

    Moisture:

    Polymerisation can be achieved by relying onmoisture either on the surface of the adherend

    or in the atmosphere to effect a cross-linkingmechanism on some other "natural" component.

    In this case the adhesive is supplied as a singlecomponent. Examples are:

    Polyurethane containing an isocyanate group. Cyanoacrylates. These are the instant bond

    adhesives. Silicones containing an acetyle group. These are

    the common R.T.V. silicones which

    with moisture releases acetic acid causing a cross-linking of the paste to an elastomer. Anaerobic which rely on absence of oxygen.

  • 7/28/2019 Joining of Composites

    30/44

    Heat:

    The final method of curing a chemical reactive type isby utilising heat to polymerise the

    adhesive components. Examples are: Expoxies with the catalyst incorporated in the

    adhesive in a latent form, e.g. dicyandiamide which will require a temperature of

    175o C to effect a cure.

    Phenolics of the resole type. Polyvinyl acetates which are based on polyvinyl

    alcohol reacted with an aldehyde. The conversion is normally about 80% and on heating

    after application the crosslinking

    is completed. Urethanes incorporating a blocked isocyanate. The

    free isocyanate groups are all

    reacted with a temporary blocking agent such asphenol which is stable up to 150oC.

  • 7/28/2019 Joining of Composites

    31/44

    Basically the adhesives in this class are thermoplasticin nature which means they are heatedto a sufficient temperature where they will flow andwet the substrates and then set and

    develop the bulk strength on cooling. The ideal HotMelt adhesive is a solid up to atemperature of 80o C (as a minimum) but will thenmelt sharply to give a low viscosity fluidthat is easily applied and capable of wetting the

    adherend followed by rapid setting uponcooling. They normally contain a base high molecularweight polymer together with tackifying resins andviscosity depressants.

  • 7/28/2019 Joining of Composites

    32/44

    Examples of polymers that are used as the base for Hot Meltadhesives are:

    Ethylene vinyl acetate - a polyethylene chain containing thehighly polar acetate

    group. Ethylene-ethyl acrylate which has an ethyl acrylic grouping.

    Ionomers - derived from ethylene acrylic acid copolymers butincluding a metal

    cation or some of the pendant carboxyl groups. The metal cation isfree to cross-link

    with the anionic side groups similar to a thermosetting resin but thereaction is

    thermally reversible.

    Phenoxies - similar chemical structure to epoxides.

    Polyamides of low to intermediate molecular weight based onthe unsaturated dibasic

    acids of vegetable origin. Polyesters (saturated).

    Vinyl resins such as polyvinyl acetate, polyvinyl butyral andpolyvinyl ethers - used

    in various special areas.

  • 7/28/2019 Joining of Composites

    33/44

    In adhesives of this class the adhesive polymers

    is essentially in its final form however,

    wetting of the adherend is achieved by

    dissolving or dispersing the polymers in asuitable

    solvent.

  • 7/28/2019 Joining of Composites

    34/44

    Solvent Based Systems:

    Rubber adhesives - usually based on an elastomerwhich is either natural or synthetic.

    The synthetic rubbers that are used in adhesives arepolychloroprene nitrile (a

    copolymer of butadiene and acrylonitrile) butyl (acopolymer of isobutylene and

    isoprene) and styrene butadiene rubber. Natural rubberis essential isoprene .

    Normally resins, usually phenol-fomaldehyde based, areincorporated.

    Phenolic or resorcinced formaldehyde resins dissolvedin a solvent.

    Vinyl resins such as polyvinyl acetate, polyvinyl

    chloride, polyvinyl ether etc. Acrylic resins based on methyl methacrylate, ethyl

    acrylate, acrylic acid etc. Miscellaneous resins such as cellulose acetate and

    polyamides.

  • 7/28/2019 Joining of Composites

    35/44

    Water Based Systems:

    There are very few polymers of sufficient

    molecular weight to be attractive as adhesivesthat

    will dissolve in water. However, dispersions oremulsions are very important. Examples are:

    Rubber latices - again either natural orsynthetic such as polychloroprene, nitrile or

    styrobutadiene rubber.

    Vinyl resins, where polyvinyl acetate

    emulsions are very widely used. Acrylic resins which offer some advantages

    over PVA types such as water and

    solvent resistance.

  • 7/28/2019 Joining of Composites

    36/44

  • 7/28/2019 Joining of Composites

    37/44

    Thermosetting plastics - The basic molecules cross-linkacross a number of free mainvalencies to a spatial molecule structure. This results inhigh strengths and rigidities.

    Thermoplastics have a linear molecular structure (string-like macromolecules). A largenumber of molecule strings are held together byphysical secondary valency bonds.Amorphous thermoplastics have a "cotton wool"

    structure. In semi-crystallinethermoplastics, parts of the microstructure depict adefinite structural arrangement sothat the attractive forces in these regions are more

    intensive than in the amorphous areas

  • 7/28/2019 Joining of Composites

    38/44

  • 7/28/2019 Joining of Composites

    39/44

    An adhesive bonded joint has many good

    properties. To make the most

    of these properties, it is important to think

    about adhesive bonding at

    the design stage.

  • 7/28/2019 Joining of Composites

    40/44

    Various materials can be joined Galvanic corrosion can be avoided Joint is permanent Makes structures stronger and more rigid Distributes load and stress more evenly in the joints Stress concentrations can be avoided. The adhesive seals and bonds and prevents

    crevice corrosion

    Low costs for finishing Good fatigue characteristics Dampens vibration Reduces weight and number of required

    components

  • 7/28/2019 Joining of Composites

    41/44

    Should not be handled directly after bonding High temperature results in reduced strength A bonded component is difficult to

    disassemble for repair and service Pre-treatment of the surface before bonding

    is essential for structural bonding and to obtain satisfactory quality in

    corrosive environments It is necessary to ensure that the adhesive

    completely covers the surface Potential health, environmental, and safety

    issues

  • 7/28/2019 Joining of Composites

    42/44

  • 7/28/2019 Joining of Composites

    43/44

    1. Influence of time on process properties 2. Pretreatment of joining parts surfaces 3. Limited form stability 4. Process parameters must be held within very narrow range;low tolerance 5. Change of properties of joint with time (ageing of adhesive layer etc.) 6. Complicated control of process 7. Low peeling strength, creep sensitive

    8. Low adhesive layer strength must e compensated by large joining area 9. Repair possibilities limited 10.Complicated strength calculation

  • 7/28/2019 Joining of Composites

    44/44

    http://www.cozybuilders.org/Oshkosh_Presentations/AbarisCompositeBondingOshkosh2005.pdf

    http://www.alueurope.eu/talat/lectures/4701.pdf

    http://nzic.org.nz/ChemProcesses/polym

    ers/10H.pdf

    http://ebookbrowse.com/assembly-

    adhesive-bonding-pdf-d313133029

    http://www.cozybuilders.org/Oshkosh_Presentations/AbarisCompositeBondingOshkosh2005.pdfhttp://www.cozybuilders.org/Oshkosh_Presentations/AbarisCompositeBondingOshkosh2005.pdfhttp://www.cozybuilders.org/Oshkosh_Presentations/AbarisCompositeBondingOshkosh2005.pdfhttp://www.alueurope.eu/talat/lectures/4701.pdfhttp://www.alueurope.eu/talat/lectures/4701.pdfhttp://nzic.org.nz/ChemProcesses/polymers/10H.pdfhttp://nzic.org.nz/ChemProcesses/polymers/10H.pdfhttp://ebookbrowse.com/assembly-adhesive-bonding-pdf-d313133029http://ebookbrowse.com/assembly-adhesive-bonding-pdf-d313133029http://ebookbrowse.com/assembly-adhesive-bonding-pdf-d313133029http://ebookbrowse.com/assembly-adhesive-bonding-pdf-d313133029http://ebookbrowse.com/assembly-adhesive-bonding-pdf-d313133029http://ebookbrowse.com/assembly-adhesive-bonding-pdf-d313133029http://ebookbrowse.com/assembly-adhesive-bonding-pdf-d313133029http://ebookbrowse.com/assembly-adhesive-bonding-pdf-d313133029http://ebookbrowse.com/assembly-adhesive-bonding-pdf-d313133029http://ebookbrowse.com/assembly-adhesive-bonding-pdf-d313133029http://ebookbrowse.com/assembly-adhesive-bonding-pdf-d313133029http://nzic.org.nz/ChemProcesses/polymers/10H.pdfhttp://nzic.org.nz/ChemProcesses/polymers/10H.pdfhttp://www.alueurope.eu/talat/lectures/4701.pdfhttp://www.alueurope.eu/talat/lectures/4701.pdfhttp://www.alueurope.eu/talat/lectures/4701.pdfhttp://www.alueurope.eu/talat/lectures/4701.pdfhttp://www.alueurope.eu/talat/lectures/4701.pdfhttp://www.alueurope.eu/talat/lectures/4701.pdfhttp://www.alueurope.eu/talat/lectures/4701.pdfhttp://www.alueurope.eu/talat/lectures/4701.pdfhttp://www.alueurope.eu/talat/lectures/4701.pdfhttp://www.alueurope.eu/talat/lectures/4701.pdfhttp://www.alueurope.eu/talat/lectures/4701.pdfhttp://www.cozybuilders.org/Oshkosh_Presentations/AbarisCompositeBondingOshkosh2005.pdfhttp://www.cozybuilders.org/Oshkosh_Presentations/AbarisCompositeBondingOshkosh2005.pdfhttp://www.cozybuilders.org/Oshkosh_Presentations/AbarisCompositeBondingOshkosh2005.pdfhttp://www.cozybuilders.org/Oshkosh_Presentations/AbarisCompositeBondingOshkosh2005.pdfhttp://www.cozybuilders.org/Oshkosh_Presentations/AbarisCompositeBondingOshkosh2005.pdfhttp://www.cozybuilders.org/Oshkosh_Presentations/AbarisCompositeBondingOshkosh2005.pdfhttp://www.cozybuilders.org/Oshkosh_Presentations/AbarisCompositeBondingOshkosh2005.pdfhttp://www.cozybuilders.org/Oshkosh_Presentations/AbarisCompositeBondingOshkosh2005.pdfhttp://www.cozybuilders.org/Oshkosh_Presentations/AbarisCompositeBondingOshkosh2005.pdfhttp://www.cozybuilders.org/Oshkosh_Presentations/AbarisCompositeBondingOshkosh2005.pdfhttp://www.cozybuilders.org/Oshkosh_Presentations/AbarisCompositeBondingOshkosh2005.pdf