Metals Flashcards

(46 cards)

1
Q

How can strength be defined?

A

resistance of a material to fracture
or resistance of a material to plastic flow

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2
Q

How can toughness be defined?

A

resistance to the propagation of a crack. E.g a crack will reduce the cross section and therefore increase the stress for an applied load. A tough material will yield and plastically deform = work hardening and energy will be absorbed. If the material is not tough the crack will propagate, little energy will be absorbed and fracture will then occur as applied stress level are far below yield strength.

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3
Q

Compare brittle vs ductile fracture

A

1.Deformation Before Fracture
Ductile: Significant plastic deformation
Brittle: Little or no plastic deformation
2.Warning Signs
Ductile: Necking & elongation before failure
Brittle: Sudden failure without warning
3. Energy Absorption (Toughness)
Ductile: High energy absorption
Brittle: Low energy absorption
4. Fracture Surface
Ductile: Rough, fibrous, cup-and-cone shaped
Brittle: Smooth, flat, cleavage or granular
5. Crack Propagation
Ductile: Slow, with plastic blunting
Brittle: Fast, unstable crack growth
7. Stress-Strain Graph Shape
Ductile: Curve with yield point, plastic region, and necking
Brittle: Linear elastic until sudden fracture

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4
Q

What are the 3 main modes of brittle failure?

A

Cleavage failure
Intergranular failure

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5
Q

What is cleavage failure?

A

only failure mode in completely brittle materials, but can occur in
normally ductile materials under certain conditions.
* In cleavage fracture, the crack path is transgranular, i.e. it passes through the grains.
* The crack propagates by breaking atomic bonds on a specific
crystallographic planes – normally the most densely packed atomic planes.
* The cleavage plane is normally the {001} plane in BCC materials, such as Fe, Mo, W etc.
* The steps/ridges within a grain are due to small changes in the local
misorientations in the grain, which can change the cleavage plane.
* The crack path will divert on crossing a grain boundary in a polycrystalline material.

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6
Q

What is intergranular failure?

A

Intergranular failure typically occurs when detrimental impurities
(P, As, S etc.) segregate to grain boundaries in polycrystalline
materials. The fracture surface is characterised by a granular
structure showing the individual grains.
The impurities reduce the cohesion between the grains, so the
grains separate with little or no plastic deformation (even if
the individual grains are very ductile)

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7
Q

What does the transition from cleavage to intergranular fracture depend on?

A

Depends on the ratio of the grain boundary energy to the energy of the surface exposed by cleavage.

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8
Q

What can suppress intergranular failure?

A

predicted in many pure metals but the segregation of beneficial impurities suppress intergranular failure

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9
Q

How do plastics Zones form?

A

materials that are able to plastically deform above their yield strength, i.e. most metals, a zone of plastic
deformation is formed ahead of the crack tip. In the plastic region, voids develop and grow, absorbing energy. This localised plastic deformation blunts the crack and the stress concentrating effect is less severe than in a brittle material.
This zone forms where the stress exceeds the yield strength of the material.

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10
Q

What is the size of the plastic zone determined by?

A

The size of the plastic zone can be determined by solving the distance from the crack tip when the stress is equal to the yield stress.

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11
Q

What causes a jagged ductile failure in metal alloys?

A

Most engineering materials contain small particles (carbides, oxides, nitrides etc.) which act as stress
concentrators.
These can separate from the matrix
(decohesion) or fracture depending on the strength of the matrix. This results in an internal crack at the centre of the necked region on a plane normal to the applied tensile axis.
The nucleated voids formed then grow and join up as the crack advances until final fracture.

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12
Q

What is ductile dimpling?

A

The fracture surface
associated with a ductile
fracture in a metal is
characterised by ‘ductile
dimpling’ where the small
particles have separated
from the matrix. Final failure occurs at shear.

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13
Q

Compare brittle fracture and ductile failure mechanisms in summary.

A
  • Brittle fracture occurs via a cleavage or intergranular fracture
    mechanism with very little plastic deformation and little energy
    absorbed.
  • Ductile failure is associated with plastic deformation leading to
    void formation and coalescence at the crack tip, which blunts
    the crack and absorbs energy.
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14
Q

What is fatigue?

A

Occurs under dynamic rather than static stresses, after a long period of time by slow growth of crack under fluctuating stress. Can oocure without warning with limited plastic deformation which would shown impending failure.

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15
Q

What are the 3 factors required for fatigue failure?

A

*A tensile stress of sufficiently high value.
*A large fluctuation in the applied stress.
*A large enough number of cycles to the applied stress.

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16
Q

What variables can control/ alter the fatigue behaviour?

A
  • Stress concentration
  • Temperature
  • Microstructure
  • Residual stress
  • Environment
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17
Q

What are the 3 main cyclic stresses applied to create failure?

A

1.Completely reversed stress cycle –
amplitude is symmetrical about the
mean zero stress level. Typical of
laboratory testing and may be
experienced by a rotating shaft
operating at constant speed
(without overloads)
2.Repeated stress cycle – amplitude
is asymmetrical about the mean
zero stress level. In this case σmax
is tension and σmin is compression,
but both could be tension.
3. Random (or spectrum) stress
cycle, such as may be
experienced by an aircraft wing
or an automotive suspension
component etc. Unexpected
overloads may occur due to
(say) turbulence or bumpy road
conditions.

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18
Q

How does high cycle fatigue(HCF) and low cycle fatigue(LCF) affect and vary?

A

Low-Amplitude Vibration (Acoustic)
Effect: Elastic response (e.g., ringing a bell)
Result: No permanent damage
Curve: Labelled ‘a’
2. Increased Amplitude Vibration
Effect: Permanent damage begins (fatigue)
Cause: Cyclic stress → Dislocation activity → Crack formation
Result: Crack propagates until reaching a critical size for fracture
3. Low-Cycle Fatigue (Curve ‘c’)
Condition: Stress cycles above the yield strength of the material
Effect: Failure occurs after few cycles
Result: Plastic deformation and failure
4. High-Cycle Fatigue (Curve ‘b’)
Condition: Stresses below the yield strength
Effect: Elastic stress, but plastic deformation may occur at the crack tip
Result: Failure after many cycles

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19
Q

How is fatigue failure usually modelled / plotted?

A

It is plotted on a stress amplitude against log number of cycles to failure known as an S-N curve.

20
Q

What is the fatigue limit?

A

Known as the endurance limit. The stress amplitude about a zero mean stress below which fatigue failure will never occur. e.g in steel or titanium alloys
Non-ferrous alloys do not exhibit this limit as fatigue can occur regardless therefore ‘fatigue strength’ is used here after N cycles

21
Q

What is the fatigue life?

A

Number of cycles to failure at a specified stress amplitude

22
Q

What does the fracture toughness describe?

A

The critical stress for the propagation of a sharp crack of a certain size so = critical stress intensity factor. It measures the resistance to brittle fracture when a crack is present. KI is larger for touch materials and low for brittle materials.

23
Q

How does the plastic zone relate to the yield strength?

A

As the yield strength increases from material shrinkage. A crack in soft metal will have a large plastic zone whereas a ceramic or glass with a high yield strength will have a small plastic zone.

24
Q

What is stress corrosion cracking(SCC)?

A

Refers to cracking due to the
simultaneous action of a (specific) corrosion environment under an applied and/or residual tensile stress. Can lead to a significant reduction in the material strength with minimal material loss. Damage is largely hidden and can result in fast and catastrophic final failure.
Sometimes described as a subset of phenomena of embrittlement including hydrogen embrittlement / anodic dissolution

25
What makes stress corrosion cracking complex?
As the processes occur at a highly localised level (typically at the crack tip. Different microstructural variables and heterogeneities, stress concentrations, temperature and modified chemical environments all contribute to the interaction of the material, environment and the stress. e.g. hydrogen induced environmental cracking has lead to brittle intergranular failure.
26
What is the electrochemical process of stress corrosion cracking (SCC)?
1.Anodic Reaction at Crack Tip Process: Localized metal dissolution Result: High metal ion concentration → Hydrolysis → H⁺ formation Effect: Low pH at crack tip (pH ~3–4), even if bulk solution is neutral (pH ~7) 2. Hydrogen Generation H⁺ Ions: Reduced to atomic hydrogen (not H₂ gas) Result: Hydrogen adsorbs and diffuses into metal ahead of crack tip 3. Embrittlement Effect: Local hydrogen accumulation → Hydrogen embrittlement Materials Affected: Susceptible alloys like Aluminum and steels
27
What are the 3 main requirements for SCC?
1. A susceptible material Generally alloys with a good general corrosion resistance (Al, Ti, stainless steels etc), will undergo SCC. Note some steels are susceptible to both general corrosion and SCC. 2. A specific environment that causes SCC in the material (specific metals with different environments like hydroxides or nitrates or methanol or sea water etc ref pg10] 3. Sufficient stress Externally applied and/or residual stress (say from machining or welding) or self generating (wedging from corrosion products). In some alloy/environment combinations the threshold stress for SCC can be as low as 5% of the yield strength.
28
What are the 4 main mechanisms of SCC and how can they be categorised?
Dissolution Effects 1.Anodic dissolution (sometimes called active path dissolution). 2.Film rupture Absorption/mechanical effects 3.Stress-sorption cracking 4.Hydrogen embrittlement
29
What is anodic dissolution?
heterogeneous regions in the microstructure (precipitation or segregation to grain boundaries) produce a local anodic path. This will lead to intergranular SCC as the grain boundary regions are dissolved. SIDE NOTE: in sensitised(from the precipitation of Cr containing carbides at the grain boundaries so the grain boundaries deplete of Cr so these regions are anodic compared to undepleted grains) stainless steel the cracking can be transgranular or intergranular.
30
What is film rupture SCC mechanism?
* Here a passive film ruptures due to the stress to reveal bare metal at the crack tip. * This leads to anodic dissolution in the presence of the stress. The crack then propagates a small distance (say 1µm) and is then arrested due to crack-tip blunting (which lowers the stress intensity). * The metal can then be repassivated and the process continues again. * The fracture surface shows evidence of discontinuous fracture and this mechanisms is seen in SCC of brass in ammonia, where dealloying can result in a brittle film being produced.
31
What is stress-sorption mechanism?
If damaging ions are adsorbed at the crack tip they can reduce the cohesive strength of the atomic bonds. The adsorption process leads to a reduction in the surface energy of the solid. From fracture mechanics, this reduces the fracture stress
32
What is hydrogen embrittlement mechanism?
Atomic hydrogen can be produced by reduction of H+ ions and due to its small atomic size, it can rapidly diffuse into the metal lattice as an interstitial impurity. This can lead to metal embrittlement either by: 1: The interstitial hydrogen causes an internal pressure if the hydrogen atoms combine to produce hydrogen gas in voids or flaws in the material. 2. Brittle metal-hydrides can form (particularly in Mg, Zr and Ti alloys, which are easily fractured. 3. Hydrogen is adsorbed at the crack tip to reduce the surface energy (as for stress-sorption). 4. Hydrogen diffuses ahead of the crack tip and makes plastic deformation and cleavage fracture easier
33
What is the difference of a SCC to regular failure from KI?
SCC is not just a process corrosion activity causes a stress concentration which then leads to failure. It is a combination of the material, environment and the stress leading to crack propagation. The stress concentration due to corrosion is unlikely to lead directly to failure in an inactive environment. the stress intensity required for cracks to propagate under stress corrosion cracking condition is less than that required for brittle fracture.
34
What does crack initiation rely on?
Some form of defect: * A pre-existing crack-like defect (such as porosity in a weld), groves from machining operations that could lead to cracking in (say) brittle martensitic microstructures, cracked inclusions etc. * A corrosion induced defect e.g. a corrosion pit, regions where a passive film is reduced such as at grain boundaries, intergranular corrosion (localised corrosion at grain boundaries due to galvanic effects), crevice corrosion, dealloying etc. * Localised cracking of a passive oxide film due to the mechanical stress or chemical attack (e.g. by Cl- ions), which then leads to pitting.
35
What are the 3 regions of crack propagation?
1. No crack propagation is observed below K1SCC, with this value dependent on the environment, the alloy and the alloy microstructure. 2.At low stress intensity values (short crack lengths) the crack growth rate increases rapidly as K increases (region 1). It will then approach a constant crack growth velocity (region 2) when some rate limiting process is established – say transport of chemical species to the crack tip. 3.Region 3 corresponds to the transition to the point where the stress intensity exceeds that for fracture in an inert environment and final brittle fracture will occur. This region seen only in very susceptible alloys.
36
What is transgranular and intergranular cracking?
Transgranular (i.e. the crack propagates through the grains) or Intergranular (i.e. the crack path is along grain boundaries). The nature of the crack path depends on the alloy and/or the environment.
37
How can stress corrosion cracking be controlled?
1. By lowering the stress intensity below the threshold for SCC, cracks will not be able to propagate. Be aware of residual stresses that can arise during fabrication or additional stress concentrations from notches, sharp changes in cross-section etc. Residual stresses can be relieved by an appropriate heat-treatment, but this may not be possible for very large structures and the heat-treatment process can cause other deleterious effects (such as sensitisation in stainless steels). 2. Ensure that the alloy/ environment combination will not give rise to SCC. This can be difficult and requires that at the design stage there is appropriate materials selection. Additionally, different heat-treatments for the same alloy will give different behaviour. SCC-resistant materials can be very expensive. 3. Coatings can be applied to remove the environment from the material, but careful consideration must be made of what happens if the coating is damaged.
38
What are examples of sources for the hydrogen that causes hydrogen embrittlement?
* Storage/containment of hydrogen gas * Corrosion (see previous slides) * Electroplating processes * Dissolved hydrogen due to liquid-state processing of metals, e.g. welding or casting * Picking of metals in acids (used to remove surface scale)
39
How can this hydrogen be absorbed ? what conditions support and cause this for hydrogen embrittlement?
Gaseous hydrogen is not normally absorbed into metals. However as the temperature is increased, molecular hydrogen can dissociate and into atomic hydrogen and high-temperature heat treatments etc. can result in hydrogen absorption. The solubility of hydrogen is higher in liquid metals than in the solid state. The dissolved hydrogen gets largely trapped in interstitial sites. For example hydrogen can be dissolved during welding, leading to subsequent cracking. (Poorly controlled casting conditions - say excess moisture present - can also result in hydrogen-related problems, e.g. gas porosity.)
40
What is electrodeposition of hydrogen?
Depending on how efficient the plating process is, electrodeposition processes (e.g. electroplating) can result in hydrogen by cathode reactions. But atomic hydrogen, not molecular hydrogen, is absorbed into the material (although recombination can cause molecular hydrogen to form in the material). e.g either hydrogen can get absorbed into the metal surface due to its high mobility(freely move in interstitial locations) and bond with another H to form H2 within the metal. ORR a metal hydrogen bond is formed which can weaken the bond (stress sorption) so then more reactions can happen to form H2 or evolution of gas via desportion if lots of H2 is absorbed
41
What does hydrogen embrittlement look like on the surface of a metal?
the fracture surfaces of hydrogen embrittled failures vary from 1.microvoids (as for ductile fracture) to 2. ‘quasi-cleavage’ (like cleavage for brittle fracture, but with the fracture plane not a typical cleavage-plane) 3. to intergranular.
42
What is de-embrittlement and why is it used?
De-embrittlement is a heat-treatment performed as soon as possible (within 1-3hour) after processing (normally after electroplating) – for ~2-4 hours at ~200°C. This allow some of the diffusible hydrogen to leave the metal, but also redistribute the remaining hydrogen, to reduce areas of high local concentrations.
43
What does control of hydrogen embrittlement rely on?
* Choosing materials with good resistance (or not using alloys particularly susceptible). * Removing hydrogen from the environment – either in service or during processing (e.g. use of mechanical removal of oxide scale rather than acid pickling). * Applying coatings to act as barriers to hydrogen ingress, but the practical use of coatings depends on the environment and the coating process may induce hydrogen. * Ensuring plating processes have a high cathode current efficiency (so that the current applied works to apply the coating and not produce hydrogen). * Use ‘hydrogen trapping’ which involves inducing defects (things like dislocations, vacancies, certain atom-types etc.) in the metal to trap hydrogen and reduce its mobility
44
What are typical SCC - HE microstructural features?
 There would be fine cracks propagate though the material in a direction perpendicular to the applied stress. It may also be possible to determine a crack initiation site, such as a pit, grain boundary etc.  Cracking can be either transgranular (i.e. the crack propagates through the grains) or intergranular (i.e. the crack path is along grain boundaries).  The fracture surface could show different fractures such as microvoids (as for ductile fracture) to ‘quasi-cleavage’ (like cleavage for brittle fracture, but with the fracture plane not a typical cleavage-plane) to intergranular fracture.  The SCC investigation would require a range of microscopy techniques such as optical microscopy to determine the crack path and scanning electron microscopy to analyse features on the fracture surface.
45
Why is there a large discrepancy between the theoretical and observed fracture strength in brittle materials?
Small cracks in the material lead to a large stress concentration at the tip of the crack. The crack can be very sharp (of the order of the atomic spacing in the material and = stress levels at the crack tip that exceed the cohesion strength of material. So although the applied stress may be lower than the theoretical fracture strength, the stress concentrating nature of the crack means the local stress at the crack tip is sufficient to break the bonds = fracture.
46
Is brittle or ductile material more sensitive to cracks in the material?
a brittle material is more sensitive to cracks in the material. For a brittle material, the yield strength is high so there is little or no plastic deformation as there's no way to relieve stress at the crack tip. Ductile materials have void formation and growth absorbs energy so the localised plastic deformation at the crack tip acts to blunt the crack and so the stress concentration effect is not as severe as in brittle.