Dental Materials Science Flashcards
stress
force is applied to an area of a material
stress Pa = force / unit area
strain
when stress is applied to an object it causes it to change shape
level of shape change = strain
proportional limit
highest limit where stress & strain on diagram continue linearly i.e. they are directly proportional to one another
elastic limit
greatest stress that can be applied to a material without causing permanent deformation
ultimate tensile strength
highest amount of stress that can be applied to a material without it breaking up
fracture stress
stress needed for fracture
young’s modulus
measure of how much a material will change its shape with stress i.e. a high YM means a large stress is required to cause a small strain
stress / strain = YM
brittle
where only a small permanent deformation is needed before fracture of material so distance between elastic limit & UTS will be small
ductile
large permanent deformation before there is fracture of material so distance between elastic limit & UTS will be large
elasticity
ability for a material to return to its original shape after stress is removed
high elasticity = flexible
low elasticity = rigid
grain
single crystal lattice with atoms orientated in different directions, when there is a change in direction of a crystal plane there is a grain boundary
with fast cooling, smaller grains are formed and these will have better mechanical properties
dislocation
in all crystal lattices there are imperfections which can slip & propagate through the metal to the grain boundary; as this changes the lattice it means it changes the shape of the metal, these can be impeded and will increase elastic limit, UTS, hardness & corrosion resistance
ductility / impact resistance are lowered
3 methods of impeding dislocations
- if grains are fine this will limit the amount of defects in crystal lattice
- cold working will push dislocations to grain boundary before metal is finally shaped
- use of alloys as they include atoms of different sizes making dislocations harder
cold working
work done on a metal at a low temp i.e. below recrystallisation temp - causes slip so dislocations will collect at grain boundaries which will allow for metal to become stronger & harder
this process will increase residual stress due to instability in crystal lattice & can lead to atoms returning over time to their original positions distorting metal shape - relieved by heat annealing
stress relief annealing
alloy is heated creating thermal vibrations allowing migration of atoms which eliminates stresses by allowing atoms to rearrange within their grains yet the structure of grains & mechanical properties remain unchanged
MUST be done below recrystallisation temp
recrystallisation
temperature by which metal / alloy forms larger equiaxed grains modifying the current structure of metal alloy & it lowers elastic limit / hardness but increases ductility
this is not wanted as it spoils benefit of cold work but may be necessary to gain correct shape
increasing cold work will decrease recrystallisation temp
phase
physically distinct homogenous structure which can have more than 1 component in this situation it is also a solution
solution
homogenous mixture of components at an atomic scale
solid solution
solution in which 2 or more metals coexist forming a common lattice structure at an atomic scale
3 types of solid solution
- random substitutional solid solution
- ordered substitutional solid solution
- interstitial solid solution - atoms of different sizes
solution hardening
where a solid solution forms with metal atoms of different sizes - this distorts grain structure & impedes dislocation movement to grain boundary therefore improving mechanical properties: elastic limit, UTS, hardness
ordered hardening
similar to solution hardening
ordered structure will impede dislocations
liquidus
temp at which solids start to crystallise
solidus
temp at which alloy has completely crystallised
coring
if alloy with large difference between liquidus & solidus is cooled rapidly coring will occur
this is where there are different alloy combinations throughout the grain so initial grain formation is not the same as the alloy combination because atoms are not able to diffuse throughout lattice as they could when cooled slowly
smaller grains in cored alloys = improved mechanical properties but decreased corrosion resistance
to overcome - homogenising annealing
homogenising annealing
alloy is reheated alloying atoms to diffuse causing all grain compositions to become homogenous without altering grain structure (as long as temp below recrystallisation temp)
eutectic alloys
metals which are soluble in the liquid state but insoluble in a solid
as a solid they will form 2 phases with each metal forming physically different grains
at point where liquidus & solidus coincide the crystallisation process will occur at 1 single temperature and grains form simultaneously
these will be hard but very brittle
partial solid solubility of AgCu
solid solution can only form at certain compositions
below H1 & above H2 a solid solution will form but between there will be 2 solid phases both of which have alpha & beta grains
beta grains are Cu rich & Ag low however they are in a solid solution above H2
if it is not cooled rapidly, the solid solution is not maintained as there is time allowed for atoms to diffuse and a 2nd phase to form
rapid cooling necessary to maintain beta structure at room temp even if the solid solubility does not allow it
hardness
resistance to scratching or its indentation resistance
compressive strength
maximum stress a material can sustain upon crush loading
tensile strength
maximum tensile stress a material can withstand
fatigue strength
measures failure of material by repeated applications of small loads
transverse strength
ability for material to deflect the load to be resisted in another area of the material
impact strength
ability of material to withstand large stresses applied rapidly to material
thermal expansion coefficient
how much material will expand when heated
thermal conductivity
arbitrary measure of how much heat is transmitted through material
flow
change in shape of a material with a static load e.g. amalgam
creep
after long periods of low stresses below elastic limit materials may flow causing permanent deformation i.e. causing ditched margins in amalgam
configuration factor
amount of tooth bonded tooth surfaces to unbonded in a restoration
adhesion
attraction between 2 dissimilar molecules / materials
cohesion
attraction between 2 similar molecules / materials
crazing
cracks appear on surface of material - produced by mechanical stresses / different TECs
viscoelastic behaviour
occurs in elastic impression materials
undergoes elastic deformation but when removed there is some permanent strain leading to overall permanent deformation
how to decrease permanent deformation in IMs
if load time is less i.e. impression removed with a sharp pull there is less overall permanent strain (lower deformation)
comp resin properties depend on (4)
- filler particle size
- amount of filler
- material used as filler
- coupling agents used
impact of filler particle size on CR
the more filler the less flowable CR is
large amount of filler means it will not undergo much polymerisation shrinkage making it more porous allowing bacterial ingress
lower filler content means more polymerisation shrinkage so less porous but will be difficult to apply
generally want a middle version
impact of particle size on CR
larger particles = stronger CR but will have issues with finishing & staining
smaller particles = give smooth filled structure but have inferior mechanical properties
modern resins are a hybrid of both
comp resin flaws
- low TEC so insulates pulp but this is higher than enamel & dentine
- slightly radiopaque
- not anticariogenic
- experiences high polymerisation shrinkage that can affect bond strength so must be built in increments
CRs made from (5)
resin BISGMA
glass filler particles
camphorquinone
low weight dimethacrylate
silane coupling agent
CR component properties
- BISGMA resin - undertakes FRAP that forms a large chain bonding glass filler particles together; exothermic reaction that may harm pulp
- glass filler particles - mainly silica
- camphorquinone - source of free radicals for FRAP, molecule is activated by blue light & causes increased strength/viscosity/RMM of resin but not all reacts (35-80% unreacted in CR)
- low weight dimethacrylate - used to adjust viscosity & reactivity of CR
- silane coupling agent - help bond between resin & glass filler as any water contaminating CR will impact this
how to use CR
- etch with phosphoric acid 20s enamel 10s dentine
- this removes smear layer produced from use of slow speed & allows collagen matrix to be formed so bonding agents can infiltrate
- remove with water & dry slightly
- overdrying dentine will cause collagen matrix collapse
- primer HEMA (hydroxyethyl methacrylate) added to infiltrate etched enamel & collagen matrix; required as BISGMA is hydrophobic & dentine is wet so allows for intimate bond. this is blown gently over surface
- BISGMA then added to infiltrate etched surface & increase contact angle so more contact with tooth between restoration & tooth surface, will also bond with CR & allow for greater retention
- this is blown dry & light cured; this mix dentine & resin produced is the hybrid layer which will stop microleakage
why add flowable CR to cavities
to lower stress caused by polymerisation shrinkage of CR & on high configuration factor areas to decrease stress on these areas
why add flowable CR to cavities
to lower stress caused by polymerisation shrinkage of CR & on high configuration factor areas to decrease stress on these areas
when will bonding system in CR not work
it won’t work well for tertiary dentine so would use a RMGI in this case as this reacts with tooth surface and increases bonding to tooth