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POLYMER MATRIX COMPOSITES (PMC)
PERTEMUAN KE-9
Material Komposit
KLASIFIKASI KOMPOSIT BERDASARKAN MATRIKSNYA
Composite materials
Matrices
Polymer Matrix Composites (PMC)
Metal Matrix Composites MMC)
Ceramic Matrix Composites (CMC)
Thermoset Thermoplastic Rubber
What is a polymer?
Poly mer
many repeat unit
C C C C C C
HHHHHH
HHHHHH
Polyethylene (PE)
ClCl Cl
C C C C C C
HHH
HHHHHH
Polyvinyl chloride (PVC)
HH
HHH H
Polypropylene (PP)
C C C C C C
CH3
HH
CH3CH3H
repeat
unit
repeat
unit
repeat
unit
Examples of polymers:
A polymer is a large molecule (macromolecule) composed of repeating
structural units typically connected by covalent chemical bonds
Polymer Matrix Composite (PMC) is the material consisting of a
polymer (resin) matrix combined with a fibrous reinforcing dispersed
phase.
Polymer Matrix Composites are very popular due to their low cost
and simple fabrication methods.
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Polymer(Matrix) Composite (Matrix + Reinforcement)
Classification of Polymers
� Polimer Linear - Semua polimer yang molekulnya dalam
bentuk rantai.
� Polimer Termoplastik - Polimer linear atau bercabang di
mana rantai molekul tidak saling berhubungan satu sama
lain.
� Polimer Thermosetting - Polimer yang saling menyilang
untuk menghasilkan struktur jaringan dimensi tiga yang
kuat.
� Elastomer - Ini adalah polimer (termoplastik atau
termoset ringan) yang memiliki deformasi elastis > 200%.
Konfigurasi rantai Molekul:
a. Linearb. Branchedc. Crossed linkedd. Ladder
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• Bentuknya bermacam-macam : discontinuous, continuous atau
woven/tenun seperti pada pembuatan kain .
• Bahan utama fiber pada FRPs adalah gelas, karbon, dan Kevlar 49.
• Fiber yang tidak umum, seperti boron, SiC, Al2O3 dan baja.
• Glass (in particular E-glass) adalah bahan fiber yang paling umum
pada FRPs saat ini; penggunaannya untuk memperkuat plastik dari
sekitar tahun 1920.
Resin thermoset adalah polimer yang paling banyak digunakan
pada PMC.
Epoxy dan polyester biasanya dicampur dengan penguat fiber.
Bentuk yang paling banyak digunakan adalah struktur laminar,
dibuat dengan menumpuk dan ikatan lapisan tipis pada fiber dan
polimer sampai ketebalan yang diinginkan diperoleh.
Fibers in PMCs
Polymerisation:This is the process of joining monomers into gaint chain like molecules.
Methods of Polymerisation:• Condensation polymerisation• Addition polymerisation
Degree of polymerization = No of monomer units in a chain
≈≈≈≈ 103 to 105
Thermosets
• Bahan termoset biasanya cair atau lunak sebelum pendinginan,
dan dirancang untuk dicetak menjadi bentuk akhirnya.
• Memiliki sifat mengalami reaksi kimia melalui aksi panas, katalis,
sinar ultraviolet, dll, menjadi zat yang relatif tidak larut dan dapat
dicairkan.
• Mereka mengembangkan struktur ikatan tiga dimensi yang baik
pada pendinginan. Setelah mengeras atau terikat silang, mereka
akan terurai dari pada mencair.
• Bahan termoset umumnya lebih kuat dari pada bahan termoplastik
karena jaringan ikatan 3-D nya, dan juga lebih cocok untuk
aplikasi suhu tinggi hingga mencapai suhu dekomposisi bahan.
• Thermoset dibuat dengan mencampurkan dua komponen (resin dan
hardener) yang bereaksi dan mengeras, baik pada temperatur ruang
atau panas.
• Hasil polimernya biasanya berupa ikat silang yang besar, sehingga
thermoset ini disebut juga dengan polimer jaringan.
• Bentuk ikat silang terjadi selama polimerisasi pada resin cair dan
hardener, sehingga strukturnya hampir selalu amorphous.
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Thermosets
• Extensive cross-linking formed by covalent bonds.
• Bonds prevent chains moving relative to each other.
Types of Thermosetting plastics
Epoxy:
Epoxy is a polymer that contain an epoxide group in its chemical structure.Example: DGEBA (Diglcidyl Ether of Bisphenol A )
Charecteristics of Epoxy:
• Better Moisture Resistence• Low shrinkage• Good adhersion with Reinforcement
Polyester:
A condensation reaction between a glycol and an unsaturated dibasic acid results in polyster. This contains a double bond C=C between its carbon atoms.Example: poly ethylene terephthalate (PET).
Charecteristics of Polyester:
• Cheap• Resistance to variety of chemicals• Adequate moisture resistance
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Thermoplastics
• In thermoplastic polymer, individual molecules are linear in structure with
no chemical linking between them.
• Mereka berada di tempat karena ikatan sekunder yang jelek
(intermolecular force), seperti ikatan van der Walls dan hydrogen.
• Some thermoplastics normally do not crystallize, they are termed
as"amorphous" plastics and are useful at temperatures below the Tg.
• Generally, amorphous thermoplastics are less chemically resistant.
Thermoplastics (80%)
• No cross links between chains.
• Weak attractive forces between chains broken by warming.
• Change shape - can be remoulded.
• Weak forces reform in new shape when cold.
Reasons for the use of thermoplastic matrix composites
• Refrigeration is not necessary with a thermoplastic matrix.
• Parts can be made and joined by heating.
• Parts can be remolded, and any scrap can be recycled.
• Thermoplastics have better toughness and impact resistance than
thermosets.
• Shorter fabrication time.
• Can be recycled.
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UNIQUE CHARACTERISTIC OF
THERMOPLASTIC
• Near to glass transition temperature
Tg, polymeric materials changes a
hard solid to soft, tough ( leather like)
solid. Over a temperature range
around Tg.Near this temperature, the
materials is also highly viscoelastic.
• When load is applied it exhibit Elastic
deformation.
• With increasing temperature polymer
changes into rubberlike solid
undergoing deformation on external
load.
• Further increasing the temp both
amorphous and semicrystallline
thermoplastic achieve highly viscous
state and attain the melting temp Tm.
• Variation of Tensile modulus with temperature for
Amorphous and Semi crytaline thermoplastic.
• Thermoplastic polymer have higher strain-to-failure.
Types of Thermoplastics
COMPARISON OF THE THREE POLYMER CATEGORIES
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Thermoplastics Vs Thermosets Functions of Matrix
• Menopang fiber secara bersama-sama.
• Melindungi fiber dari lingkungan.
• Mendistribusikan beban secara merata di antara fiber sehingga semuafiber terdistribusi sejumlah regangan yang sama.
• Meningkatkan sifat sebuah lapisan tranversal.
• Meningkatkan resisytansi impak dan kerusakan komponen.
• Membantu menghindari rambatan retak yang tumbuh melalui fiber denganmemberikan alternatif kegagalan sepanjang permukaan antara fiber danmatriks.
Desired Properties of a Matrix
• Reduced moisture absorption.
• Low shrinkage.
• Low coefficient of thermal expansion.
• Good flow characteristics so that it penetrates the fibre bundlescompletely and eliminates voids during the compacting/curingprocess.
• Must be elastic to transfer load to fibres.
• Reasonable strength, modulus and elongation (elongationshould be
greater than fibre).
• Strength at elevated temperature (depending on application).
• Low temperature capability (depending on application).
• Excellent chemical resistance (depending on application).
• Should be easily processable into the final composite shape.
• Dimensional stability (maintains its shape).
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Effect of Temperature on Thermoplastics
� Degradationtemperature - Thetemperature abovewhich a polymerburns, chars, ordecomposes.
� Glass temperature -The temperaturerange below whichthe amorphouspolymer assumes arigid glassystructure.
The effect of temperature on the modulus of
elasticity for an amorphous thermoplastic.
Stress-strain behavior of different polymer
matrices
0
10
20
30
40
50
60
70
80
90
0 1 2 3 4 5
Strian(%)
Str
ess (M
pa)
Phenolic
Polyester Epoxy
0
10
20
30
40
50
60
70
80
0 100 200 300 400 500
Strian(%)S
tress (M
pa)
Polysulfon
PolyamidPolyethylene
Thermoplastic polymers Thermosetting polymers
Notice to the range of ultimate strains of different polymers
Comparision of various polymers as matrix materialsLimitations of PMC (Termoplastis)
– Low maximum working temperature.
– High coefficient of thermal expansion- dimensional instability
– Sensitivity to radiation and moisture.
– Processing temperature are generally higher than those with
thermosets.
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Pultrusion
Advantages:
� Minimal kinking of
fibres/fabrics
� Rapid processing
� Low material scrap rate
� Good quality control
Potential Problems:
� Improper fibre wet-out
� Fibre breakage
� Inadequate cure
� Die jamming
� Complex die design
Pultrusion -characteristics
• seek uniform thickness in order to achieve uniform cooling and hence minimise
residual stress.
• hollow profiles require a cantilevered mandrel to enter the die from the fibre-feed
end.
• continuous constant cross-section profile
• normally thermoset (thermoplastic possible)
– impregnate with resin
– pull through a heated die
• resin shrinkage reduces friction in the die
• polyester easier to process than epoxy
• tension control as in filament winding
• post-die, profile air-cooled before gripped
– hand-over-hand hydraulic clamps
– conveyor belt/caterpillar track systems.
• moving cut-off machine ("flying cutter"). The solid laminate will be cut to the
desired length
• Inside the metal die, precise temperature control activates the curing of the thermoset resin.
Interfacial bonding
• Good bonding (adhesion) between matrix phase and dispersed
phase provides transfer of load, applied to the material to the
dispersed phase via the interface. Adhesion is necessary for
achieving high level of mechanical properties of the composite.
• There are three forms of interface between the two phases:
• Direct bonding with no intermediate layer. In this case adhesion
(”wetting”) is provided by either covalent bonding or van der
Waals force.
• Intermediate layer (inter-phase) is in form of solid solution of the
matrix and dispersed phases constituents.
• Intermediate layer is in form of a third bonding phase
(adhesive).
The Interface
• There is always an interface between constituent phases in acomposite material.
• For the composite to operate effectively, the phases must bondwhere they join at the interface.
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Reinforcement-Matrix Interface
• The load acting on the matrix has to be transferred to the reinforcement via. Interface.
• The reinforcement must be strongly bonded to the matrix if high stiffness and strength are desired in the composite materials
• A weak interface results in low stiffness and strength but high resistance to fracture.
• A strong interface produces high stiffness and strength but often low resistance to fracture, i.e. brittle behavior
2 types of failure at interface
1) Adhesive failure - failure occur at interface2) Cohesive failure – failure occur close to the interface (either at the fiber or
matrix)
• Setelah matriks memiliki kebasahan (wetability) terhadap penguat,
ikatan akan terjadi.
• Untuk sistem tertentu, lebih dari satu mekanisme ikatan mungkin
terjadi pada waktu yang sama.
• Ikatan dapat berubah selama tahap produksi atau selama perbaikan.
Interfacial bonding
Types of interfacial bonding at interface
• Mechanical bonding• Physical bonding• Chemical bonding
Mechanical Bonding
• It is a simple mechanical keying or interlocking effect between the fiber-matrix phases.
• When the matrix shrinks radially on cooling over the reinforcement leads to a griping action of the matrix on the fiber.
Physical Bonding
• These kind of bonding involves weak secondary or vanderwaals forces, dipolar interactions and hydrogen bonds.
• These type of bonding mechanism is of low significance because of itslow magnitude.
• The bond energy lies in the range of 8-16 kJ/mol.
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Chemical bonding
• Dissolution Bonding: This bonding is of short range and occurs at anelectronic scale. This type of bonding is hindered by the presence ofimpurities on the fiber surface and also gas or air bubbles at theinterface.
• Reaction Bonding: This bonding is due to the transport of the molecules,atoms or ions which diffuse to the interface.
Interphase• In some cases, a third ingredient must be added to achieve
bonding of primary and secondary phases
• Called an interphase, this third ingredient can be thought of as
an adhesive
Another Interphase
Interphase consisting of a solution of primary and
secondary phases
APPLICATIONS OF PMCs
• Polymer composites are used to make very light bicycles that arefaster and easier to handle than standard ones, fishing boats thatare resistant to corrosive seawater and lightweight turbine bladesthat generate wind power efficiently. New commercial aircraft alsocontain more composites than their predecessors. A 555-passengerplane recently built by Airbus, for example, consists of 25 percentcomposite material, while Boeing is designing a new jumbo aircraftthat is planned to be more than half polymer composites.
• Polymer Matrix Composites (PMCs) are used for manufacturing:secondary load-bearing aerospace structures, boat bodies, canoes,kayaks, automotive parts, radio controlled vehicles, sport goods (golfclubs, skis, tennis racquets), fishing rods, bullet-proof vests andother armor parts, brake and clutch linings.