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Chapter 7: Dislocations & Strengthening Mechanisms
ISSUES TO ADDRESS... • Why are dislocations observed primarily in metals and alloys? • How are strength and dislocation motion related? • How do we increase strength? • How can heating change strength and other properties?
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Dislocations & Materials Classes
Dislocation types: edge and screw • Metals: Disl. motion easier. -non-directional bonding -close-packed directions for slip. electron cloud ion cores + • Covalent Ceramics (Si, diamond): Motion hard. - very hard, Tm>3550C -directional bonding • Ionic Ceramics (NaCl): Motion hard. -need to avoid ++ and - - neighbors. - non-directional bonding + - PD corresponds to the motion of large numbers of dislocations
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Dislocation Motion Plastic deformation mechanisms are 1. slipping 2. twinning Dislocations & plastic deformation Cubic & hexagonal metals - plastic deformation by plastic shear or slip where one plane of atoms slides over adjacent plane by defect motion (dislocations). So we saw that above the yield stress plastic deformation occurs. But how? In a perfect single crystal for this to occur every bond connecting tow planes would have to break at once! Large energy requirement Now rather than entire plane of bonds needing to be broken at once, only the bonds along dislocation line are broken at once. If dislocations don't move, deformation doesn't occur!
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Dislocation Motion Slip is the process by which plastic deformation is produced by dislocation motion Dislocation moves along slip plane in slip direction perpendicular to dislocation line( slip system) Slip direction have the same direction as Burgers vector Edge dislocation Screw dislocation
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Slipping Mechanism Slip System
Slip plane – plane along which the dis. line traverses plane allowing easiest slippage highest planar densities Slip direction - direction of movement - Highest linear densities FCC Slip occurs on {111} planes (close-packed) in <110> directions (close-packed) => total of 12 slip systems in FCC in BCC & HCP other slip systems occur
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The slip planes are usually the most densely packed planes
The slip planes are usually the most densely packed planes. Slip is favored on closed packed planes since a lower shear stress for atomic displacement is required than for less densely packed planes. Slip in the closed packed direction is also favored since less energy is required to move the atoms from one position to another if the atoms are closer together.
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Slip: The process by which plastic deformation is produced by dislocation motion
The slip system depends on the crystal structure of the metal and is such that the atomic distortion that accompanies the motion of a dislocation is a minimum dislocation density: (The number of dislocations). is expressed as the total dislocation length per unit volume, or equivalently, the number of dislocations that intersect a unit area of a random section. The units of dislocation density are millimeters of dislocation per cubic millimeter or just per square millimeter. Dislocation densities as low as 10 3 mm -2 All metals and alloys contain some dislocations that were introduced during 1.solidification, 2.during plastic deformation, and as a consequence of 3.thermal stresses that result from rapid cooling.
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Stress and Dislocation Motion
• Crystals slip due to a resolved shear stress, tR. • Applied tension can produce such a stress. Applied tensile stress: = F/A s direction slip F A slip plane normal, ns Resolved shear stress: tR = F s /A direction slip AS FS direction slip Relation between s and tR = FS /AS F cos l A / f nS AS
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Critical Resolved Shear Stress
• Condition for dislocation motion: Critical resolved shear stress: is the minimum shear stress required to initiate slip and is a property of the material that determine when yielding occurs 10-4 GPa to 10-2 GPa typically • Crystal orientation can make it easy or hard to move dislocation tR = 0 l =90° s tR = s /2 l =45° f tR = 0 f =90° s maximum at = = 45º
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For The crystal ordinarily fractures rather than deforming plastically
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Single Crystal Slip
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Ex: Deformation of single crystal
a) Will the single crystal yield? b) If not, what stress is needed? =60° crss = 3000 psi =35° = 6500 psi So the applied stress of 6500 psi will not cause the crystal to yield.
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Ex: Deformation of single crystal
What stress is necessary (i.e., what is the yield stress, sy)? So for deformation to occur the applied stress must be greater than or equal to the yield stress
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Slip Motion in Polycrystals
300 mm • Stronger metals- grain boundaries pin deformations • Slip planes & directions (l, f) change from one crystal to another. • tR will vary from one • The crystal with the largest tR yields first. • Other (less favorably oriented) crystals yield later.
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Anisotropy in sy Isotropic. Having identical values of a property in all crystallographic directions. • Can be induced by rolling a polycrystalline metal - before rolling - after rolling - anisotropic since rolling affects grain orientation and shape. rolling direction 235 mm - isotropic since grains are approx. spherical & randomly oriented.
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Anisotropy in Deformation
• The noncircular end view shows anisotropic deformation of rolled material. end view 3. Deformed cylinder plate thickness direction 1. Cylinder of Tantalum machined from a rolled plate: rolling direction 2. Fire cylinder at a target. side view
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Twinning mechanism A part of the atomic lattice is deformed so that is forms a mirror image of the un-deformed lattice next to it. Twinning plane: is the plane between the un-deformed and deformed parts of the metal lattice
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Comparison between slip and twinning mechanisms
slipping twinning the atoms in one side of the slip plane all move equal distances the atoms move distances proportional to their distance from the twinning plane Slip Leaves a series of steps (lines) 2. Twinning leaves small but well defined regions of the crystal deformed 3. Most for FCC and BCC structure, they have more slip systems 3. Is most important for HCP structure , because its small number of slip system 4. normally slip results in relatively large deformations 4. only small deformations result for twinning
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Mechanisms of strengthening in metals
The ability of a metal to plastically deform depends on the ability of dislocations to move. ductility is sacrificed when an alloy is strengthened restricting or hindering dislocation motion renders a material harder and stronger. strengthening mechanisms for single phase metals, by grain size reduction, solid-solution alloying, and strain hardening(cold work).
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4 Strategies for Strengthening: 1: Reduce Grain Size
• Grain boundaries are barriers to slip. Change direction Discontinuity of slip planes • Barrier "strength" increases with Increasing angle of mis-orientation. • Smaller grain size: more barriers to slip. • Hall-Petch Equation: d = average grain diameter σy - yield strength σ0, ky are constant for particular material
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Materials are a fine grained materials (one that has small grains) and a coarse grained. Fine grained material is harder and stronger than coarse grained. Grain size may be regulated by the rate of solidification from the liquid phase, and also by plastic deformation followed by an appropriate heat treatment ( depends on time and temperature). The greater tem. And time the greater grain size.
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4 Strategies for Strengthening: 2: Solid Solutions
• Impurity atoms distort the lattice & generate stress. • Stress can produce a barrier to dislocation motion. • Smaller substitutional impurity Impurity generates local stress at A and B that opposes dislocation motion to the right. A B • Larger substitutional impurity Impurity generates local stress at C and D that opposes dislocation motion to the right. C D
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Stress Concentration at Dislocations
Don’t move past one another – hardens material
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Strengthening by Alloying
small impurities tend to concentrate at dislocations reduce mobility of dislocation increase strength
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Strengthening by alloying
large impurities concentrate at dislocations on low density side
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Ex: Solid Solution Strengthening in Copper
• Tensile strength & yield strength increase with wt% Ni. Tensile strength (MPa) wt.% Ni, (Concentration C) 200 300 400 10 20 30 40 50 Yield strength (MPa) wt.%Ni, (Concentration C) 60 120 180 10 20 30 40 50 • Empirical relation: • Alloying increases sy and TS.
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4 Strategies for Strengthening: 3: Cold Work (%CW)
Strain hardening: a ductile metal becomes harder and stronger as it is plastically deformed( the effect of CW may be removed by annealing HT) • Room temperature deformation. • Common forming operations change the cross sectional area: -Forging A o d force die blank -Rolling roll A o d -Drawing tensile force A o d die -Extrusion ram billet container force die holder die A o d extrusion
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Dislocations During Cold Work
• Ti alloy after cold working: 0.9 mm • Dislocations entangle with one another during cold work. • Dislocation motion becomes more difficult.
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Result of Cold Work total dislocation length Dislocation density =
unit volume Dislocation density = Carefully grown single crystal ca. 103 mm-2 Deforming sample increases density mm-2 Heat treatment reduces density mm-2 Again it propagates through til reaches the edge large hardening small hardening s e y0 y1 • Yield stress increases as rd increases:
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Effects of Stress at Dislocations
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Impact of Cold Work As cold work is increased
• Yield strength (sy) increases. • Tensile strength (TS) increases. • Ductility (%EL or %AR) decreases.
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Cold Work Analysis Cu Cu Cu • What is the tensile strength &
=12.2mm Copper • What is the tensile strength & ductility after cold working? D o =15.2mm % Cold Work 100 300 500 700 Cu 20 40 60 yield strength (MPa) % Cold Work tensile strength (MPa) 200 Cu 400 600 800 20 40 60 ductility (%EL) % Cold Work 20 40 60 Cu s y = 300MPa 300MPa 340MPa TS = 340MPa 7% %EL = 7%
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s- e Behavior vs. Temperature
• Results for polycrystalline iron: -200C -100C 25C 800 600 400 200 Strain Stress (MPa) 0.1 0.2 0.3 0.4 0.5 • sy and TS decrease with increasing test temperature. • %EL increases with increasing test temperature. • Why? Vacancies help dislocations move past obstacles. 3 . disl. glides past obstacle 2. vacancies replace atoms on the disl. half plane 1. disl. trapped by obstacle obstacle
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4 Strategies for Strengthening: 4: Precipitation Strengthening
• Hard precipitates are difficult to shear. Ex: Ceramics in metals (SiC in Iron or Aluminum). Side View precipitate Top View Slipped part of slip plane Unslipped part of slip plane S spacing Large shear stress needed to move dislocation toward precipitate and shear it. Dislocation “advances” but precipitates act as “pinning” sites with spacing S . • Result:
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Application: Precipitation Strengthening
• Internal wing structure on Boeing 767 • Aluminum is strengthened with precipitates formed by alloying. 1.5mm
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Note: The strengthening effects due to grain size reduction and strain hardening can be eliminated or at least reduced by an elevated temperature heat treatment. Conversely, solid solution strengthening is unaffected by heat treatment
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Recovery, Recrystallization, and Grain Growth
These properties and structures may revert back to the precold-worked states by appropriate heat treatment (sometimes termed an annealing treatment). Such restoration results from two different processes that occur at elevated temperatures: recovery and recrystallization, which may be followed by grain growth.
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Effect of Heating After %CW
• 1 hour treatment at Tanneal... decreases TS and increases %EL. • Effects of cold work are reversed! tensile strength (MPa) ductility (%EL) tensile strength ductility Recovery Recrystallization Grain Growth 600 300 400 500 60 50 40 30 20 annealing temperature (ºC) 200 100 700 • 3 Annealing stages to discuss...
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Recovery tR Annihilation reduces dislocation density. • Scenario 1
Results from diffusion extra half-plane of atoms Dislocations annihilate and form a perfect atomic plane. atoms diffuse to regions of tension • Scenario 2 tR 1. dislocation blocked; can’t move to the right Obstacle dislocation 3 . “Climbed” disl. can now move on new slip plane 2 . grey atoms leave by vacancy diffusion allowing disl. to “climb” 4. opposite dislocations meet and annihilate
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Recrystallization • New grains are formed that:
-- have a small dislocation density -- are small -- consume cold-worked grains. 33% cold worked brass New crystals nucleate after 3 sec. at 580C. 0.6 mm
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Further Recrystallization
• All cold-worked grains are consumed. After 4 seconds After 8 0.6 mm
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TR = recrystallization temperature
TR TR = recrystallization temperature
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Recrystallization Temperature, TR
TR = recrystallization temperature = point of highest rate of property change Tm => TR Tm (K) Due to diffusion annealing time TR = f(t) shorter annealing time => higher TR Higher %CW => lower TR – strain hardening Pure metals lower TR due to dislocation movements Easier to move in pure metals => lower TR
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Grain Growth grain growth: After recrystallization is complete, the strain-free grains will continue to grow if the metal specimen is left at the elevated temperature this phenomenon is called grain growth. Grain growth does not need to be preceded by recovery and recrystallization; it may occur in all polycrystalline materials, metals and ceramics alike As grains increase in size, the total boundary area decreases, yielding an attendant reduction in the total energy; this is the driving force for grain growth. Grain growth occurs by the migration of grain boundaries. Obviously, not all grains can enlarge, but large ones grow at the expense of small ones that shrink. The directions of boundary movement and atomic motion are opposite to each other growth via atomic diffusion
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Grain Growth • At longer times, larger grains consume smaller ones.
• Why? Grain boundary area (and therefore energy) is reduced. After 8 s, 580ºC After 15 min, 0.6 mm • Empirical Relation: elapsed time coefficient dependent on material and T. grain diam. at time t. exponent typ. ~ 2
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Coldwork Calculations
A cylindrical rod of brass originally 0.40 in (10.2 mm) in diameter is to be cold worked by drawing. The circular cross section will be maintained during deformation. A cold-worked tensile strength in excess of 55,000 psi (380 MPa) and a ductility of at least 15 %EL are desired. Further more, the final diameter must be 0.30 in (7.6 mm). Explain how this may be accomplished.
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Coldwork Calculations Solution
If we directly draw to the final diameter what happens? Brass Cold Work D f = 0.30 in D o = 0.40 in
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Coldwork Calc Solution: Cont.
420 540 6 For %CW = 43.8% Adapted from Fig. 7.19, Callister 7e. y = 420 MPa TS = 540 MPa > 380 MPa %EL = 6 < 15 This doesn’t satisfy criteria…… what can we do?
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Coldwork Calc Solution: Cont.
380 12 15 27 For TS > 380 MPa > 12 %CW For %EL < 15 < 27 %CW our working range is limited to %CW = 12-27
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Coldwork Calc Soln: Recrystallization
Cold draw-anneal-cold draw again For objective we need a cold work of %CW 12-27 We’ll use %CW = 20 Diameter after first cold draw (before 2nd cold draw)? must be calculated as follows: So after the cold draw & anneal D02=0.335m Intermediate diameter =
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Coldwork Calculations Solution
Summary: Cold work D01= 0.40 in Df1 = m Anneal above D02 = Df1 Cold work D02= in Df 2 =0.30 m Therefore, meets all requirements Fig 7.19
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Rate of Recrystallization
Hot work above TR Cold work below TR Smaller grains stronger at low temperature weaker at high temperature log t start finish 50%
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Summary • Dislocations are observed primarily in metals and alloys.
• Strength is increased by making dislocation motion difficult. • Particular ways to increase strength are to: --decrease grain size --solid solution strengthening --precipitate strengthening --cold work • Heating (annealing) can reduce dislocation density and increase grain size. This decreases the strength.
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problem The lower yield point for an iron that has an average grain diameter of 1x10-2 mm is 230 MPa (33,000 psi). At a grain diameter of 6x10-3 mm, the yield point increases to 275 MPa (40,000 psi). At what grain diameter will the lower yield point be 310 MPa (45,000 psi)?
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We are asked to determine the grain diameter for an iron which will give a yield strength of 310 MPa (45,000 psi). The best way to solve this problem is to first establish two simultaneous expressions of Equation 7.7, solve for σ0 and ky, and finally determine the value of d when σy = 310 MPa. The data pertaining to this problem may be tabulated as follows:
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problem The critical resolved shear stress for copper is 0.48 MPa (70 psi). Determine the maximum possible yield strength for a single crystal of Cu pulled in tension. Answer: In order to determine the maximum possible yield strength for a single crystal of Cu pulled in tension, we simply employ Equation 7.5 as
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problem Two previously un-deformed cylindrical specimens of an alloy are to be strain hardened by reducing their cross-sectional areas (while maintaining their circular cross sections). For one specimen, the initial and deformed radii are 15 mm and 12 mm, respectively. The second specimen, with an initial radius of 11 mm, must have the same deformed hardness as the first specimen; compute the second specimen’s radius after deformation.
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In order for these two cylindrical specimens to have the same deformed hardness, they must be deformed to the same percent cold work. For the first specimen For the second specimen, the deformed radius is computed using the above equation and solving for rd as
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