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T207 – Tutorial block 4 T207 – Tutorial block 4

T207 – Tutorial block 4 - PowerPoint Presentation

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T207 – Tutorial block 4 - PPT Presentation

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structure corrosion metals atoms corrosion structure atoms metals slip crystalline polymers block material temperature stress planes petch hall structures

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Slide1

T207 – Tutorial block 4

Please check your headphone and microphones and adjust them for sound levels

Check your audio settings by running the Audio Setup Wizard: either press the icon in the 'Audio and Video' panel, or navigate to Tools > Audio > Audio Setup Wizard and follow the on-screen instructions.

https://learn1.open.ac.uk/mod/oucontent/view.php?id=8322Slide2
Slide3

T207 – Tutorial 05

Parts 1 - 3

Corrosion

Material PropertiesSlide4

Corrosion

List the different types of corrosion.

Suggest ways of preventing the types of corrosion.Slide5

Corrosion

What is corrosion?

What causes corrosion?

What is necessary for corrosion to occur?Slide6

Corrosion

Corrosion is an electro chemical process that removes electrons from one material and passes them to another.

Corrosion is caused by having two dis-similar metals in contact through an electrolyte and results in an electric current passing between them. Slide7
Slide8

Corrosion

There are FOUR basic requirements in order for corrosion to occur

An ANODE

A CATHODE

An ELECTROLYTE (a solution that will allow electrons to flow

An ELECTRIC CURRENT (or flow of electrons)Slide9

Anode & Cathode

Anode

Loss of electron in oxidation

Oxidation always occurs at the anode

Cathode

Gain of electron in reduction

Reduction always occurs at the cathodeSlide10

Corrosion

The chemical process is dependent upon the Galvanic series and Electro-potential

These series show the electrical potentials (as measured against a datum, such as hydrogen) that are usually listed in order of their NOBILITY (or likelihood to corrode)Slide11
Slide12

Corrosion

Other corrosion mechanisms

See section 4

of Block 5 Part 1

Pitting

corrosion (doesn’t require 2 dissimilar metals – usually a scratch in a protective surface)Slide13

Corrosion

Other corrosion mechanisms

See section 4

of Block 5 Part 1

Pitting

corrosion (doesn’t require 2 dissimilar metals – usually a scratch in a protective surface)Slide14

Corrosion

Other corrosion mechanisms

See section 4

of Block 5 Part 1

Stress-corrosion cracking (combination of a tensile stress, chemical environment and a material susceptible to chemical attackSlide15
Slide16

Corrosion

Other corrosion mechanisms

Crevice corrosion (occurs where conditions suggest corrosion shouldn’t take place; a crevice where moisture can collect and stagnate)Slide17

Corrosion

Other corrosion mechanisms

Erosion

and cavitation

corrosion (fast flowing fluids where low pressures cause air bubbles to collapse)Slide18

Preventing corrosion

You need to remove at least one of the 4 requirements for corrosion to occur

This can be in the form of a layer of protective material, sacrificial metal to corrode etc.Slide19

Preventing corrosion

Use the same metals (not dis-similar)

Avoid crevices where moisture can collect and stagnate

Avoid water accumulation by sealing joints etc.

Joint design

Welding design (double V joints smoothed over)

Coatings, painting etc.

Sacrificial metalsSlide20

Polymers

Polymers can degrade due to

Elevated temperatures for prolonged periods

UV degradation

Chemical degradationSlide21

UV light and polymers

UV light can attack the long molecular chains, breaking them down.Slide22

Chemical degradation of polymers

Usually associated with elevated temperatures and an acidic or alkaline environmentSlide23

Material Properties

How does the atomic structure of metals differ from ceramics?

How does this affect their mechanical properties?Slide24

Metals

Metals are made of a crystalline structure that is fairly simple and repetitive.

They have been investigated through X ray diffraction techniques and the images analysed to ascertain the underlying crystalline structureSlide25

Basic crystalline structuresSlide26

Basic crystalline structures

Face centred cubic

Usually more ductile than other structuresSlide27

Basic crystalline structures

Body centred cubic

Less tightly packed (more free space)Slide28

Basic crystalline structures

Hexagonal close packing

Each atom is surrounded by 6 other atomsSlide29

Slip planes

Atoms can slip (move) in the crystalline structureSlide30

Slip planes

Atoms can slip (move) in the crystalline structureSlide31

Slip planes

The slip planes are associated with the easiest path for atoms to move past each other.

Close packed structures have several slip planes and so they are more malleable and ductile than other packing structuresSlide32

2D slip planesSlide33
Slide34

Dislocations

Dislocations are imperfections in the metallic crystalline structure which make it easier for atoms to move and thus increase the ductility of metals.

This ductility is also associated with the extended plastic behaviour of metals (deformation after the elastic limit has been achieved).

Plasticity requires the presence of dislocations and the ability of them to move through the crystalline structureSlide35
Slide36
Slide37
Slide38

Structure of ceramics

Ceramic materials are crystalline (as metals) but are usually compounds of two or more elements

The arrangement of the atoms is specific (not random) and this affects the packing structure.

Size of atoms affects the structure (large and small ions may not form a rectangular structure)Slide39

Sodium chloride (salt)Slide40

Barium Titanate

Ba

Ti

O4Slide41

Amorphous ceramics

Usually oxides, these have no close packed structure and hence have no crystalline structure as suchSlide42

Amorphous ceramicsSlide43
Slide44

Differences between metals and ceramics

Metal bonding allows the atoms to move past each other (slip planes) which give

srise

to ductility, malleability and plasticity

Ceramic atoms are chemically bonded to each other, so there are NO slip planes for the atoms to move past each other

Force on a ceramic will lead to fracture of the bonds, and hence the material (but at high temperatures there may be limited slip)Slide45

Structure of polymers

Polymers are made up of long strings of atoms, which are built up of regular or irregular sub stringsSlide46

Bonding in polymers

Individual chains are strongly chemically bonded, but links with other chains is from weaker inter-atomic Van der Vaal's forcesSlide47

How polymer chains appear Slide48

Transition temperatures

From block 2, the ductile brittle temperature is the temperature where the material will suffer a ductile failure rather than brittleSlide49

Melting temperature

This is the temperature when the substance changes phase from solid to liquid (T

m

)Slide50

Melting temperature

This is the temperature when the substance changes phase from solid to liquid (T

m

)Slide51

Glass temperature

For an amorphous ceramic, it is the temperature when the material will become less brittle and less stiffSlide52

Stress strain relationships for polymersSlide53

Stress strain relationships for polymersSlide54

Stress strain relationships for polymersSlide55

Viscoelasticity

Where a polymer exhibits both viscous and elastic behaviour

Viscous is where polymer chains slip pass each other

Elastic is where the chains are subjected to tensile forces

Tine dependent (hysteresis behaviour on

laoding

/unloading)Slide56
Slide57

Increasing strength of metals

Controlling the strength of metals is all about controlling how the atoms slip past each other and impeding the passage of dislocations.Slide58

Impeding dislocation movement

Plastically deforming the material will cause dislocations to interfere, entangle and impede the motion of other – WORK HARDENING

As crystal boundaries impede the motion of the dislocations, reducing the size of the crystal grain size also impedes the movement of dislocations – GRAIN SIZE STRENGTHENINGSlide59

Impeding dislocation movement

Changing the size of the atoms (alloying with other atoms) – this addition of alloying elements to make a solid solution is called SOLUTION HARDENING

Discrete particles of different composition of the second

phas

can present obstacles to dislocation movement – AGE HARDENING or PRECIPITION HARDENINGSlide60

Hall-Petch Equation

SAQ 3.1 Page 123 Block 5 Part 3

The 0.1% proof stress of an aluminium alloy was measured for different grain diameters, d, produced by annealing at various temperatures. At the largest grain diameter of 0.5 mm the 0.1% proof stress was 110 MN m

-2

and the value of k was found to be 0.45 MN m

-3/2

. Estimate the 0.1% proof stress with a grain diameter of 0.04 mm.

d = 0.5 mm = 0.0005 m

σ

t

= 110 MN m

-2

= 110x10

6

N m

-2

and k = 0.45 MN m

-3/2

= 0.45x10

6

N m

-3/2

Using the Hall-

Petch

equation

σ

t

= σ

0

+

kd

–0.5Slide61

Hall-Petch Equation

SAQ 3.1 Page 123 Block 5 Part 3

d = 0.5 mm = 0.0005 m σ

t

= 110 MN m

-2

= 110x10

6

N m

-2

and k = 0.45 MN m

-3/2

= 0.45x10

6

N m

-2

Using the Hall-Petch equation

σ

t

= σ

0

+

kd

–0.5

Know d,

σ

t

and k Need to find

σ

0

σ

0

= σ

t

-

kd

–0.5

σ

0

= 110x10

6

- 0.45x10

6

x 0.0005

-0.5

So

σ

0

= 89875388 N m

-2

= 90 MN m

-2Slide62

Hall-Petch Equation

SAQ 3.1 Page 123 Block 5 Part 3

d = 0.5 mm = 0.0005 m σ

t

= 110 MN m

-2

= 110x10

6

N m

-2

and k = 0.45 MN m

-3/2

= 0.45x10

6

N m

-2

Using the Hall-Petch equation

σ

t

= σ

0

+

kd

–0.5

Know d,

σ

t

and k Need to find

σ

0

σ

0

= σ

t

-

kd

–0.5

σ

0

= 110x10

6

- 0.45x10

6

x 0.0005

-0.5

So

σ

0

= 89875388 N m

-2

= 90 MN m

-2

σ

t

= 90 + 0.45

d

–0.5

With a grain diameter, d = 0.04 mm = 0.00004 m

σ

t

= 90

10

6

+ (0.45

10

6

0.00004

–0.5

)

σ

t

= 161151247 N m

-2

=

161 MN m

–2Slide63

Hall-Petch Equation

I was asked to explain the transposition of a formula

in Exercise 3.1 of Block 5 Part 3 to mke k the subject.

σ

t

= σ

0

+

kd

–0.5

Know

σ

t

and

σ

0

need to find k

σ

t

– σ

0

=

kd

–0.5

t

– σ

0

) / d

-0.5

=

k or k =

t

– σ

0

) / d

-0.5

A negative index means the inverse so 1 / d

-0.5

= d

0.5

So k = (σ

t

– σ

0

) d

0.5

σ

0

= 90x10

6

N m

-2

σ

t

= 113x10

6

N m

-2

d= 0.0004 m

k = (113x10

6

– 90x10

6

) x 0.0004

0.5

k = 460000 = 460x10

3

N m

-3/2Slide64

Strengthening polymers

Change the chain structure by copolymerisation or modification of the repeated monomer unit

Alignment of the chains in the direction of loading

Fabrication of composites – such as the Mosquito aircraft in WW2 – made by cabinet makers with wood and glue. Now the Boeing Dreamliner continues the work!