AE 1354 - HIGH TEMPERATURE MATERIALS - PowerPoint PPT Presentation

1 / 100
About This Presentation
Title:

AE 1354 - HIGH TEMPERATURE MATERIALS

Description:

AE 1354 - HIGH TEMPERATURE MATERIALS UNIT 1 UNIT 1 CREEP CREEP Definition Creep The rate of this deformation is a function of the material properties ... – PowerPoint PPT presentation

Number of Views:1700
Avg rating:3.0/5.0
Slides: 101
Provided by: spatergir
Category:

less

Transcript and Presenter's Notes

Title: AE 1354 - HIGH TEMPERATURE MATERIALS


1
AE 1354 - HIGH TEMPERATURE MATERIALS
  • UNIT 1

2
UNIT 1
  • CREEP

3
(No Transcript)
4
CREEP
  • Definition

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
5
Creep
  • 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.

6
Creep
Stress
Strain
Time
7
Mechanisms 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

8
Mechanisms 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.

9
(No Transcript)
10
Figure Showing slip of an edge dislocation
11
Grain 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.

12
Evidence for grain boundary sliding
13
(No Transcript)
14
(No Transcript)
15
Mechanisms of Creep
16
Classical creep curve
17
(No Transcript)
18
(No Transcript)
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

21
Practical 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

22
Other 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.

24
Stages 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.

25
Mechanisms 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

27
Dislocation 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.
28
Creep 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.
29
(No Transcript)
30
(No Transcript)
31
Effect of stress on creep curves at constant
temperature
32
(No Transcript)
33
(No Transcript)
34
(No Transcript)
35
(No Transcript)
36
(No Transcript)
37
(No Transcript)
38
(No Transcript)
39
(No Transcript)
40
Unit III
  • Fracture

41
(No Transcript)
42
(No Transcript)
43
(No Transcript)
44
(No Transcript)
45
(No Transcript)
46
(No Transcript)
47
(No Transcript)
48
(No Transcript)
49
(No Transcript)
50
(No Transcript)
51
(No Transcript)
52
(No Transcript)
53
(No Transcript)
54
(No Transcript)
55
(No Transcript)
56
(No Transcript)
57
(No Transcript)
58
(No Transcript)
59
Unit IV
  • Oxidation and corrosion

60
What 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).

61
(No Transcript)
62
Pilling-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.

63
continued
  • 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.

64
Kinetic 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

68
Third 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

69
Introduction 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.

70
continued
  • 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

71
(No Transcript)
72
(No Transcript)
73
(No Transcript)
74
High 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

75
Combat of hot corrosion
76
Unit V
  • Super alloys and other Material

77
Introduction
78
(No Transcript)
79
(No Transcript)
80
(No Transcript)
81
(No Transcript)
82
(No Transcript)
83
superalloy
  • 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

84
(No Transcript)
85
(No Transcript)
86
(No Transcript)
87
Alloy designations for some common superalloys
88
(No Transcript)
89
(No Transcript)
90
Solid 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

91
Precipitation 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

92
Grain 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.

93
TCP phase
94
Embrittlement
  • 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

95
(No Transcript)
96
Intermetallics
  • 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

97
(No Transcript)
98
(No Transcript)
99
(No Transcript)
100
(No Transcript)
Write a Comment
User Comments (0)
About PowerShow.com