Title: AE 1354 - HIGH TEMPERATURE MATERIALS
1AE 1354 - HIGH TEMPERATURE MATERIALS
2UNIT 1
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4CREEP
Creep is the
tendency of a solid material to slowly move or
deform permanently under the influence of
stresses. It occurs as a result of long term
exposure to levels of stress that are below the
yield strength of the material. Creep is more
severe in materials that are subjected to heat
for long periods, and near the melting point.
Creep always increases with temperature
5Creep
- The rate of this deformation is a function of the
material properties, exposure time, exposure
temperature and the applied structural load.
Depending on the magnitude of the applied stress
and its duration, the deformation may become so
large that a component can no longer perform its
function for example creep of a turbine blade
will cause the blade to contact the casing,
resulting in the failure of the blade.
6Creep
Stress
Strain
Time
7Mechanisms of Creep
- High rates of diffusion permit reshaping of
crystals to relieve stress - Diffusion significant at both grain boundaries
and in the bulk - High energy and weak bonds allow dislocations to
climb around structures that pin them at lower
temperature
8Mechanisms of Creep in metals
- Mechanisms of Creep in metals There are three
basic mechanisms that can - contribute to creep in metals, namely
- (i) Dislocation slip and climb.
- (ii) Grain boundary sliding.
- (iii) Diffusional flow.
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10Figure Showing slip of an edge dislocation
11Grain Boundary sliding
- Grain Boundary sliding The onset of
tertiary creep is a sign that structural damage
has occurred in an alloy. Rounded and wedge
shaped voids are seen mainly at the grain
boundaries and when these coalesce creep rupture
occurs. The mechanism of void formation involves
grain boundary sliding which occurs under the
action of shear stresses acting on the
boundaries.
12Evidence for grain boundary sliding
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15Mechanisms of Creep
16Classical creep curve
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19- Creep deformation is important not only in
systems where high temperatures are endured such
as nuclear power plants, jet engines and heat
exchangers, but also in the design of many
everyday objects
20- Generally, the minimum temperature required for
creep deformation to occur is 30-40 of the
melting point for metals and 40-50 of melting
point for ceramics - creep can be seen at relatively low temperatures
for some materials. Plastics and
low-melting-temperature metals, including many
solders, creep at room temperature as can be seen
marked in lead and zinc
21Practical example
- An example of an application involving creep
deformation is the design of tungsten lightbulb
filaments. Sagging of the filament coil between
its supports increases with time due to creep
deformation caused by the weight of the filament
itself. If too much deformation occurs, the
adjacent turns of the coil touch one another,
causing an electrical short and local
overheating, which quickly leads to failure of
the filament
22Other some examples
- Other examples
- Though mostly due to the reduced yield stress at
higher temperatures, the Collapse of the World
Trade Center was due in part to creep from
increased temperature operation. - The creep rate of hot pressure-loaded components
in a nuclear reactor at power can be a
significant design-constraint, since the creep
rate is enhanced by the flux of energetic
particles. - Creep was blamed for the Big Dig tunnel ceiling
collapse in Boston, Massachusetts that occurred
in July 2006
23- In steam turbine power plants, steam pipes carry
superheated vapour under high temperature
(1050F/565.5C) and high pressure often at 3500
psi (24.131 MPa) or greater. - In a jet engine temperatures may reach to 1000C,
which may initiate creep deformation in a weak
zone. - For these reasons, it is crucial for public and
operational safety to understand creep
deformation behavior of engineering materials.
24Stages of creep
- In the initial stage, known as primary creep, the
strain rate is relatively high, but slows with
increasing strain. - The strain rate eventually reaches a minimum and
becomes near-constant. This is known as secondary
or steady-state creep. This stage is the most
understood. The characterized "creep strain
rate", typically refers to the rate in this
secondary stage. The stress dependence of this
rate depends on the creep mechanism.
25Mechanisms of creep The mechanism of creep
depends on temperature and stress. The various
methods are Thermally activated glide - e.g.,
via cross-slip Climb assisted glide - here the
climb is an enabling mechanism, allowing
dislocations to get around obstacles Climb -
here the strain is actually accomplished by climb
Grain boundary diffusion
26- General creep equation
- where e is the creep strain, C is a constant
dependent on the material and the particular
creep mechanism, m and b are exponents dependent
on the creep mechanism, Q is the activation
energy of the creep mechanism, s is the applied
stress, d is the grain size of the material, k is
Boltzmann's constant, and T is the absolute
temperature
27Dislocation creep At high stresses (relative to
the shear modulus), creep is controlled by the
movement of dislocations. When a stress is
applied to a material, plastic deformation
occurs due to the movement of dislocations in
the slip plane. Materials contain a variety of
defects, for example solute atoms, that act as
obstacles to dislocation motion.
28Creep arises from this because of the phenomenon
of dislocation climb. At high temperatures
vacancies in the crystal can diffuse to the
location of a dislocation and cause the
dislocation to move to an adjacent slip plane.
By climbing to adjacent slip planes dislocations
can get around obstacles to their motion,
allowing further deformation to occur. Because
it takes time for vacancies to diffuse to the
location of a dislocation this results in time
dependent strain, or creep.
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31Effect of stress on creep curves at constant
temperature
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40Unit III
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59Unit IV
60What is Oxidation ?
- Oxidation means the loss of electrons. The
oxidation of a metal occurs when the metal loses
one or more electrons, so that the atoms of the
metal go from the neutral state and become a
positively charge ion. This commonly results in
the formation of a metal oxide (in the case of
iron, that is known as rust).
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62Pilling-Bedworth ratio
- In their 1923 paper "The oxidation of metals in
high temperature" presented to the Institute of
Metals, N. B. Pilling and R. E. Bedworth first
correlated the porosity of a metal oxide with the
specific density1. The Pilling-Bedworth ratio,
(P-B ratio) R, of a metal oxide is defined as the
ratio of the volume of the metal oxide, which is
produced by the reaction of metal and oxygen, to
the consumed metal volume -
- M and D are the molecular weight and density of
the metal oxide whose composition is
(Metal)a(oxygen)b m, and d are the atomic weight
and density of the metal.
63continued
- Pilling and Bedworth realized that, when R is
less than 1, a metal oxide tends to be porous and
non-protective because it cannot cover the whole
metal surface. Later researchers found that, for
excessively large R, large compressive stresses
are likely to exist in metal oxide, leading to
buckling and spalling. In addition to R, factors
such as the relative coefficients of thermal
expansion and the adherence between metal oxide
and metal should also be favorable in order to
produce a protective oxide.
64Kinetic laws of corrosion
- Three basic kinetic laws have been used to
characterize the oxidation rates of pure metals.
It is important to bear in mind that these laws
are based on relatively simple oxidation models.
Practical oxidation problems usually involve
alloys and considerably more complicated
oxidation mechanisms and scale properties than
considered in these simple analyses
65- The parabolic rate law assumes that the diffusion
of metal cations or oxygen anions is the rate
controlling step and is derived from Fick's first
law of diffusion. The concentrations of diffusing
species at the oxide-metal and oxide-gas
interfaces are assumed to be constant. The
diffusivity of the oxide layer is also assumed to
be invariant. This assumption implies that the
oxide layer has to be uniform, continuous and of
the single phase type. Strictly speaking, even
for pure metals, this assumption is rarely valid.
The rate constant, kp, changes with temperature
according to an Arrhenius type relationship -
66- where
- x is the oxide film thickness (or the mass gain
due to oxidation, which is proportional to the
oxide film thickness) - t is time
- kp is the rate constant, directly proportional to
the diffusivity of the ionic species that is rate
controlling - x0 is a constant
67- The logarithmic rate law is an empirical
relationship with no fundamental underlying
mechanism. This law is mainly applicable to thin
oxide layers formed at relatively low
temperatures, and therefore rarely applicable to
high temperature engineering problems - where
- ke is the rate constant
- c and b are constants
-
68Third law
- The linear rate law is also an empirical
relationship that is applicable to the formation
and build-up of a non-protective oxide layer. -
-
- where
- kL is the rate constant
69Introduction to High Temperature Corrosion
- High temperature corrosion is a form of corrosion
that does not require the presence of a liquid
electrolyte. Sometimes, this type of damage is
called "dry corrosion" or "scaling". The term
oxidation is ambivalent since it can either refer
to the formation of oxides or to the mechanism of
oxidation of a metal, i.e. its change to a higher
valence than the metallic state. Strictly
speaking, high temperature oxidation is only one
type of high temperature corrosion. In fact,
oxidation is the most important high temperature
corrosion reaction.
70continued
- In most corrosive high temperature environments,
oxidation often participates in the high
temperature corrosion reactions, regardless of
the predominant mode of corrosion. Alloys often
rely upon the oxidation reaction to develop a
protective scale to resist corrosion attack such
as sulfidation, carburization and other forms of
high temperature attack. In general, the names of
the corrosion mechanisms are determined by the
most abundant dominant corrosion products
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74High temperature corrosion is a widespread
problem in various industries such as
- power generation (nuclear and fossil fuel)
- aerospace and gas turbine
- heat treating
- mineral and metallurgical processing
- chemical processing
- refining and petrochemical
- automotive
- pulp and paper
- waste incineration
75Combat of hot corrosion
76Unit V
- Super alloys and other Material
77Introduction
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83superalloy
- A superalloy is a metallic alloy which can be
used at high temperatures, often in excess of 0.7
of the absolute melting temperature. Creep and
oxidation resistance are the prime design
criteria. Superalloys can be based on iron,
cobalt or nickel, the latter being best suited
for aeroengine applications
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87Alloy designations for some common superalloys
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90Solid solution strengthening
- Solid solution strengthening is a type of
alloying that can be used to improve the strength
of a pure metal. The technique works by adding
atoms of one element (the alloying element) to
the crystalline lattice another element (the base
metal). The alloying element diffuses into the
matrix, forming a solid solution. In most binary
systems, when alloyed above a certain
concentration, a second phase will form. When
this increases the strength of the material, the
process is known as precipitation strengthening
91Precipitation hardening
- Precipitation hardening, also called age
hardening, is a heat treatment technique used to
strengthen malleable materials, including most
structural alloys of aluminum, magnesium, nickel
and titanium, and some stainless steels. It
relies on changes in solid solubility with
temperature to produce fine particles of an
impurity phase, which impede the movement of
dislocations, or defects in a crystal's lattice.
Since dislocations are often the dominant
carriers of plasticity, this serves to harden the
material. The impurities play the same role as
the particle substances in particle-reinforced
composite materials
92Grain boundary strengthening
- Grain boundary strengthening (or Hall-Petch
strengthening) is a method of strengthening
materials by changing their average crystallite
(grain) size. It is based on the observation that
grain boundaries impede dislocation movement and
that the number of dislocations within a grain
have an effect on how easily dislocations can
traverse grain boundaries and travel from grain
to grain. So, by changing grain size one can
influence dislocation movement and yield
strength.
93TCP phase
94Embrittlement
- Embrittlement is a loss of ductility of a
material, making it brittle. Various materials
have different mechanisms of embrittlement. - Hydrogen embrittlement is the effect of hydrogen
absorption on some metals and alloys. - Sulfide stress cracking is the embrittlement
caused by absorption of hydrogen sulfide. - Liquid metal embrittlement (LME) is the
embrittlement caused by liquid metals. - (MIE) is the embrittlement caused by diffusion
of atoms of metal, either solid or liquid, into
the material. - Neutron radiation causes embrittlement of some
materials, neutron-induced swelling, and buildup
of Wigner energy. This is a process especially
important for neutron moderators and nuclear
reactor vessels
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96Intermetallics
- Intermetallics are compounds that form when
certain combinations of two or more metals are
mixed together in certain proportions and react
to produce a solid phase that is distinctively
different from the constituent elements
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