ti_col.pdf
TRANSCRIPT
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1Titanium Titanium Titanium Titanium
Alloys IAlloys I
Titanium Titanium
Alloys IAlloys IAlloys IAlloys I
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2General properties of TiGeneral properties of TiGeneral properties of TiGeneral properties of Ti
It has a HEX lattice at low temperature (
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3Page 3
OutlineOutlineOutlineOutline
Ti primary production Ti primary production
CP Ti and applications
-Ti alloying, alloy design
near- alloy microstructures, forging near- alloy microstructures, forging
and heat treatment
/ alloys, Ti-6Al-4V / alloys, Ti-6Al-4V
defects
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4Ti Primary Production Ti Primary Production
Kroll ProcessKroll Process
Ti Primary Production Ti Primary Production
Kroll ProcessKroll Process Ti common in Earths crust Ti common in Earths crust
Energy to separate ~125 MWhr/tonne (7/kg just in
power)
Batch process over 5 days:
Produce TiCl4 from TiO2 and Cl2
TiCl + 2 Mg 2 MgCl + Ti TiCl4 + 2 Mg 2 MgCl2 + Ti
chip out Ti sponge (5-8 t) from reactor
cost 8/kg cost 8/kg
Chlorides corrosive, nasty
World annual capacity ~100,000 t, demand ~60,000t World annual capacity ~100,000 t, demand ~60,000t
Need a cheaper process that is direct
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5Production of TiProduction of Ti
Obtained from minerals:Obtained from minerals:
rutilerutile (TiO(TiO )) rutilerutile (TiO(TiO22))
ilmeniteilmenite (FeO(FeO--TiOTiO22) approx 97) approx 97--98% TiO98% TiO22
Chemically converted to pure TiClChemically converted to pure TiCl Chemically converted to pure TiClChemically converted to pure TiCl44
Kroll Process:Kroll Process:
TiClTiCl reactesreactes with liquid Mg at ~773with liquid Mg at ~773--873873C in a C in a TiClTiCl44 reactesreactes with liquid Mg at ~773with liquid Mg at ~773--873873C in a C in a
closed stainlessclosed stainless--steel vessel (retort)steel vessel (retort)
4TiCl4TiCl (gas) + 2Mg (liquid) (gas) + 2Mg (liquid) Ti (solid) + 2MgClTi (solid) + 2MgCl (liquid)(liquid) 4TiCl4TiCl44 (gas) + 2Mg (liquid) (gas) + 2Mg (liquid) Ti (solid) + 2MgClTi (solid) + 2MgCl22 (liquid)(liquid)
Ti spongeTi spongeTi spongeTi sponge
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6Preparation of Ti IngotsPreparation of Ti Ingots
Molten Ti Molten Ti reactsreacts with oxygen & nitrogenwith oxygen & nitrogen
Ti sponge crushed & compacted into electrode Ti sponge crushed & compacted into electrode
compactscompactscompactscompacts
these welded togetherthese welded together
form consumable electrodeform consumable electrode
for vacuum arc meltingfor vacuum arc melting
For alloy ingots the alloying materials are mixed For alloy ingots the alloying materials are mixed
with the crushed Ti sponge before compactingwith the crushed Ti sponge before compacting
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7Page 7
Subsequent ProcessingSubsequent ProcessingSubsequent ProcessingSubsequent Processing
harvey fig p11
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8Production of TitaniumProduction of Titanium
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9Page 9
CastingCastingCastingCasting Use skull melting (EBHCR) instead of VIM/VAR/ESR for final melting
stage in triple melting process
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Titanium AlloysTitanium Alloys Relatively new engineering metalsRelatively new engineering metals
Been in use as structural materials only since 1952Been in use as structural materials only since 1952
Ti alloys attractive because:Ti alloys attractive because:
High strength/weight ratioHigh strength/weight ratio
High elevated temperature properties (i.e., ~550High elevated temperature properties (i.e., ~550C)C) High elevated temperature properties (i.e., ~550High elevated temperature properties (i.e., ~550C)C)
Excellent corrosion resistance (particularly in Excellent corrosion resistance (particularly in
oxidizing acids and chloride media and in most natural oxidizing acids and chloride media and in most natural oxidizing acids and chloride media and in most natural oxidizing acids and chloride media and in most natural
environments)environments)
Disadvantage is cost i.e., Ti ~8x cost of aluminum and Disadvantage is cost i.e., Ti ~8x cost of aluminum and
5x cost of stainless steel5x cost of stainless steel5x cost of stainless steel5x cost of stainless steel
However they do compete effectively in areas where However they do compete effectively in areas where
strength/weight and highstrength/weight and high--elevated temperature elevated temperature strength/weight and highstrength/weight and high--elevated temperature elevated temperature
properties are of prime importance (i.e. aerospace)properties are of prime importance (i.e. aerospace)
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Commercially attractive propertiesCommercially attractive properties
and applicationsand applicationsand applicationsand applications
resistance to corrosion:resistance to corrosion: resistance to corrosion:resistance to corrosion:
chemical processing, the pulp and paper industry, chemical processing, the pulp and paper industry,
marine applications, and energy production and marine applications, and energy production and
storagestorage
inertness in the human body:inertness in the human body:
biomedical, surgical implants and prosthetic devicesbiomedical, surgical implants and prosthetic devices biomedical, surgical implants and prosthetic devicesbiomedical, surgical implants and prosthetic devices
high specific strength:high specific strength:
automotive industryautomotive industry automotive industryautomotive industry
cameras, jewellery, frames for glasses musical cameras, jewellery, frames for glasses musical
instruments, and sports equipmentinstruments, and sports equipment
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Ti Ti PourbaixPourbaix
Diagram:Diagram:Diagram:Diagram:
good corrosiongood corrosion
resistanceresistanceresistanceresistance
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Susceptibility to crevice corrosionSusceptibility to crevice corrosion
Crevice corrosion of Grade 2Crevice corrosion of
Ti0.3Mo0.8Ni and grade
2 unalloyed Ti in
saturated NaCl solution.
Grade 2
saturated NaCl solution.
Shaded band represents
transition zone between
active and passive active and passive
behavior.
Ti0.3Mo0.8Ni
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Selected physical properties ofSelected physical properties of
titanium as compared to those of titanium as compared to those of titanium as compared to those of titanium as compared to those of
aluminium and ironaluminium and iron
Titanium Aluminium Iron
Density gm/cm3 4.54 2.70 7.87
Modulus of elasticity, x103 MPa 113 70 208
Melting point [C] 1,668 660 1,537Melting point [C] 1,668 660 1,537
Crystal structure at room
temperature
HCP FCC BCC
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ConsiderConsider pure Tipure TiConsiderConsider pure Tipure Ti
Purity ranges from 99.5Purity ranges from 99.5--99.099.0% Ti% Ti Purity ranges from 99.5Purity ranges from 99.5--99.099.0% Ti% Ti
Main alloying elements: Fe, C, O, N (interstitials)Main alloying elements: Fe, C, O, N (interstitials)
Can be considered an Can be considered an --phase alloy in which oxygen phase alloy in which oxygen Can be considered an Can be considered an --phase alloy in which oxygen phase alloy in which oxygen
content determines the grade and strength content determines the grade and strength %O equivalent %O equivalent
= %O + 2%N + 0.67%C= %O + 2%N + 0.67%C
Each 0.1%O equivalent of interstitial elements in pure Ti increases Each 0.1%O equivalent of interstitial elements in pure Ti increases
strength by ~120 strength by ~120 MPaMPa
Although interstitials increase strength they decrease toughnessAlthough interstitials increase strength they decrease toughness Although interstitials increase strength they decrease toughnessAlthough interstitials increase strength they decrease toughness
Therefore if high toughness is desired (especially at low Therefore if high toughness is desired (especially at low
temperatures), an alloy will be produced with extratemperatures), an alloy will be produced with extra--low low
interstitials interstitials (ELI)(ELI)interstitials interstitials (ELI)(ELI)
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Miller indices of hexagonal Miller indices of hexagonal
crystal planescrystal planescrystal planescrystal planes
(a) Basal planes (b) Prism planes (a) Basal planes (b) Prism planes (c) (c) Pyramidal planesPyramidal planes
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Deformation properties of pure TiDeformation properties of pure Ti
Can be coldCan be cold--rolled at room temperature to rolled at room temperature to
>90% without >90% without crackingcracking>90% without >90% without crackingcracking
Unusual for HCP metals due to low c/a ratioUnusual for HCP metals due to low c/a ratio
Relatively high ductility of HCP Ti is attributed Relatively high ductility of HCP Ti is attributed Relatively high ductility of HCP Ti is attributed Relatively high ductility of HCP Ti is attributed
to the many operative slip systems and to the many operative slip systems and
available twinning planes in the crystal latticeavailable twinning planes in the crystal lattice
i.e. slip occurs on the {1010} prism planes i.e. slip occurs on the {1010} prism planes
and the {1011} pyramidal plans as well as on and the {1011} pyramidal plans as well as on
the basal planesthe basal planesthe basal planesthe basal planes
Twinning in plastic deformation more important Twinning in plastic deformation more important
in Ti than in Mg, Zn and in Ti than in Mg, Zn and CdCdin Ti than in Mg, Zn and in Ti than in Mg, Zn and CdCd
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Lattice parameters of HCP metalsLattice parameters of HCP metals
Metal a c c/a*
Beryllium 2.2840 3.5841 1.5692Beryllium 2.2840 3.5841 1.5692
Cadmium 2.9787 5.6170 1.8857
Cobalt 2.5070 4.0690 1.6230
Hafnium 3.2060 5.0870 1.5867
Magnesium 3.2092 5.2103 1.6235
Titanium 2.9504 4.6833 1.5873Titanium 2.9504 4.6833 1.5873
Zinc 2.6640 4.9450 1.8562
Zirconium 3.2300 5.1330 1.5892
*High c/a ratio leads to primary slip system on basal planes
Note: c/a affects tendency towards 2 secondary slip systems:
PyramidalPyramidal
Prismatic (primary is Basal plane)
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Alloys DesignationAlloys Designation
CATEGORY CATEGORY
Grade 1 Pure Titanium, low oxygen Grade 16 Pure Titanium + 0,040,08% Pd, standard oxygen
Grade 2 Pure Titanium, standard oxygen Grade17 Pure Titanium + 0,040,08% Pd, low Grade 2 Pure Titanium, standard oxygen Grade17 Pure Titanium + 0,040,08% Pd, low oxygen
Grade 3 Pure Titanium, high oxygen Grade 18 Alloy (Al 3%, V 2,5%) + 0,040,08% Pd
Grade 4 Pure Titanium, very high oxygen Grade 19 Alloy (Al 3%, V 8%, Cr 6%, Zr 4%, Mo 4%)
Grade 5 Alloy (Al 6%, V 4%) Grade 20 Alloy (Al 3%, V 8%, Cr 6%, Zr 4%, Mo Grade 5 Alloy (Al 6%, V 4%) Grade 20 Alloy (Al 3%, V 8%, Cr 6%, Zr 4%, Mo 4%) + 0,040,08% Pd
Grade 6 Alloy (Al 5%, Sn 2,5%) Grade 21 Alloy (Mo 15%, Al 3%, Nb 2,7%, Si 0,25%)
Grade 7 Pure Titanium + 0,120,25% Pd, standard oxygen
Grade 22 - - - - - - -
Grade 8 - - - - - - Grade 23 Alloy (Al 6%, V 4%) ELI Grade 8 - - - - - - Grade 23 Alloy (Al 6%, V 4%) ELI
Grade 9 Alloy (Al 3%, V 2,5%) Grade 24 Alloy (Al 6%, V 4%) + 0,040,08% Pd
Grade 10 - - - - - - Grade 25 Alloy (Al 6%, V 4%) + Ni 0,30,8%, 0,040,08% Pd
Grade 11 Pure Titanium + 0,120,25% Pd, low oxygen
Grade 26 Pure Titanium + 0,080,14% Ru oxygen
Grade 12 Alloy (Mo 0,3%, Ni 0,8%) Grade 27 Pure Titanium + 0,080,14% Ru
Grade 13 Alloy (Ni 0,5%, Ru 0,05%), very low oxygen
Grade 28 Alloy (Al 3%, V 2,5%) + 0,080,14% Ru
Grade 14 Alloy (Ni 0,5%, Ru 0,05%) low oxygen Grade 29 Alloy (Al 6%, V 4%) ELI + 0,080,14%
Ru
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Ru
Grade 15 Alloy (Ni 0,5%, Ru 0,05%) standard oxygen
Grade 30 Pure Titanium + Co 0,200,80%, 0,040,08% Pd
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Influence of interstitial elementsInfluence of interstitial elementsInfluence of interstitial elementsInfluence of interstitial elements
800
1000
R
e
s
i
s
t
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a
[
M
P
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20
30
R
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(
s
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%
Azoto
Ossigeno
600
800
R
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s
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a
[
M
P
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]
Azoto
Ossigeno
10
20
R
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(
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)
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%
Ossigeno
Carbonio
400
0 0,1 0,2 0,3 0,4 0,5 0,6 0,7 0,8
Contenuto di interstiziali, %
Ossigeno
Carbonio
0
0 0,1 0,2 0,3 0,4 0,5 0,6 0,7 0,8
Contenuto di interstiziali, %R
o
t
t
u
r
a
a
f
l
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s
s
i
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(
s
a
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d
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,
%
The graphs evidence the strength and elongation as a The graphs evidence the strength and elongation as a The graphs evidence the strength and elongation as a The graphs evidence the strength and elongation as a
Contenuto di interstiziali, % Contenuto di interstiziali, %
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The graphs evidence the strength and elongation as a The graphs evidence the strength and elongation as a function of interstitial elements amount (N, function of interstitial elements amount (N, O, C).O, C).The graphs evidence the strength and elongation as a The graphs evidence the strength and elongation as a function of interstitial elements amount (N, function of interstitial elements amount (N, O, C).O, C).
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Impact propertiesImpact propertiesImpact propertiesImpact properties200
grado 2
grado 3
100
150
R
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s
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l
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z
a
[
J
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grado 3
grado 4
50
100
R
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a
[
J
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0
-200 -100 0 100 200 300 400
Trend of impact energy Trend of impact energy of of three three different titanium alloysdifferent titanium alloys
Temperatura [C]
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different titanium alloysdifferent titanium alloys
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Corrosion ResistanceCorrosion Resistance
0,8V
e
l
o
c
i
t
d
i
c
o
r
r
o
s
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n
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,
Ti-0,3Mo-0,8Ni
Grado 2
Ti-0,2Pd
0,4
0,6
V
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c
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d
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c
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r
r
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m
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Ti-0,2Pd
0,2
0,4
V
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r
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m
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0
0 20 40 60 80
Concentrazione di HNO3, %
V
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c
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c
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r
r
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,
CCorrosion orrosion resistance as a function of nitric acid resistance as a function of nitric acid
concentration concentration of of three titanium alloysthree titanium alloys
Concentrazione di HNO3, %
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concentration concentration of of three titanium alloysthree titanium alloys
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Phase Diagram IPhase Diagram I
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TiTi-- AlAl
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Phase Diagram Phase Diagram IIII
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TiTi-- VV
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Phase Diagram Phase Diagram IIIIII
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TiTi-- ZrZr
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Influence of alloying elementsInfluence of alloying elementsInfluence of alloying elementsInfluence of alloying elements
Alloying Element Range weight % Effect on structure
Aluminium 2 7 stabilizingAluminium 2 7 stabilizing
Tin 2 6 stabilizing
Vanadium 2 20 stabilizingMolibdenum 2 20 stabilizing
Chromium 2 12 stabilizingCopper 2 6 stabilizing - e hardening
A very important A very important property property of the alloying elements is of the alloying elements is
Zirconium 2 8 -
Silicon 0,05 1 Increase creep resistance
A very important A very important property property of the alloying elements is of the alloying elements is their influence on the stabilization the their influence on the stabilization the phase (low phase (low
temperature) or the temperature) or the phase (high temperature).phase (high temperature).
22/03/2010 Prof. G. Ubertalli
Carbon, oxygen and nitrogen are Carbon, oxygen and nitrogen are stabilizing.stabilizing.
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Ti Allotropes, Phase Ti Allotropes, Phase
DiagramDiagram
Ti Allotropes, Phase Ti Allotropes, Phase
DiagramDiagram
Pure Ti:
L (bcc) @ 1,668 C
(hcp) @ 882.5 C (hcp) @ 882.5 C
=4.7 g/cc
highly protective TiO2 film2
Diffusion in 100x slower
than in
origin of better creep origin of better creep
resistance
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4 alloys to be considered4 alloys to be considered
Grades 1Grades 14 increase in O4 increase in O--CC--N N UsageUsage
A. Pure Ti (99.0 + A. Pure Ti (99.0 + %Ti%Ti) HCP 35%) HCP 35%
B. B. alloyalloy (Ti(Ti--5Al5Al--2.5Sn) 2.5Sn) GradeGrade 6 10%6 10%B. B. alloyalloy (Ti(Ti--5Al5Al--2.5Sn) 2.5Sn) GradeGrade 6 10%6 10%
-- phasephase stabiliserstabiliser
C. C. alloyalloy (Ti(Ti--13V13V--11Cr11Cr--3Al) BCC ~1%3Al) BCC ~1%C. C. alloyalloy (Ti(Ti--13V13V--11Cr11Cr--3Al) BCC ~1%3Al) BCC ~1%
-- phasephase stabiliserstabiliser
D. D. + + alloyalloy TiTi--6Al6Al--4V 4V GradeGrade 5/23 55%5/23 55%D. D. + + alloyalloy TiTi--6Al6Al--4V 4V GradeGrade 5/23 55%5/23 55%
-- phasephase stabiliserstabiliser -- phasephase stabiliserstabiliser
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Mechanical propertiesMechanical propertiesMechanical propertiesMechanical properties
Grade Y.S. (MPa) UTS (MPa) % Elongation
1. Pure Ti 241585 331661 30201. Pure Ti 241585 331661 3020
2. Ti-5Al-2.5Sn () 806 861 16
3. Ti-1V-11Cr-3Al () 1,205 (H.T.) 1,275 8
4. Ti-6Al-4V (+) 1,102 (H.T.) 1,171 10
(H.T.) = Solution anneal quench and aged
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Alloys Alloys
Ti-5Al-2Sn-2Zr-4Mo-4Cr (Ti-17) Designed for high strength and depth sections and uses at
intermediate temperatureTi-6Al-2Sn-4Zr-6Mo
Ti-6Al-2Sn-4Zr-6Mo (Ti-6242) Designed for creep resistance
Ti-6Al-2Nb-1Ta-1Mo Designed for stress corrosion cracking in acqueous salt solution
and for high fracture toughnessTi-6Al-4V-ELI
Ti-5Al-2.5Sn Designed for weld ability
Ti-5Al-2.5Sn-ELI Adopted for cryogenic applicationsTi-5Al-2.5Sn-ELI Adopted for cryogenic applications
Ti-6Al-4V - lega ( + )-the most usedTi-6Al-6V-2Sn
Ti-10V-2Fe-3Al
They evidence a poor quench-ability in case of high depth
Designed for high strength at room and intermediate temperature
AlloyAlloy ,, suchsuch asas TiTi--55AlAl--22..55Sn,Sn, areare slightlyslightly lessless corrosioncorrosion resistantsresistants
butbut evidenceevidence aa higherhigher strengthstrength thanthan purepure titaniumtitanium..
AlloyAlloy areare generallygenerally ductileductile;; thethe ELIELI gradegrade maintainsmaintains thisthis propertyproperty AlloyAlloy areare generallygenerally ductileductile;; thethe ELIELI gradegrade maintainsmaintains thisthis propertyproperty
atat cryogeniccryogenic temperaturetemperature..
AlloyAlloy areare notnot hardenablehardenable byby heatheat treatmenttreatment becausebecause thesethese alloysalloys
areare stablestable.. TheseThese alloysalloys cancan bebe hardenedhardened byby graingrain sizesize reductionreduction.. TheThe
22/03/2010 Prof. G. Ubertalli
areare stablestable.. TheseThese alloysalloys cancan bebe hardenedhardened byby graingrain sizesize reductionreduction.. TheThe
mostmost importantimportant alloyingalloying elementelement isis AlAl..
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Microstructures Microstructures near near
alloysalloys
Microstructures Microstructures near near
alloysalloys stabilisers raise / stabilisers raise /
transus
stabilisers to widen /
field and allow hot workingfield and allow hot working
heat treatable
~10% primary (grain boundary)
during h.t. @ > 900 Cduring h.t. @ > 900 C
oil quench intragranular
plates + retained
age at ~ 625 C to form , age at ~ 625 C to form ,
spheroidise and stress relieve
Then >> 90%
Lightly deformed (~5%) Ti-834
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Imperial College London
Page 32
Refined grain size
stronger
better fatigue resistance better fatigue resistance
Predominantly few good slip systems
good creep resistance
Si segregates to dislocation cores inhibit glide/climb further Si segregates to dislocation cores inhibit glide/climb further
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HeatingHeating TemperatureTemperature
TheThe heatingheating temperaturetemperature isis
fundamentalfundamental inin thethe workabilityworkability 1100fundamentalfundamental inin thethe workabilityworkability
andand inin thethe finalfinal obtainableobtainable
propertiesproperties..
DifferentDifferent forgingforging and/orand/or
1000
1050
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Regione beta 100 % beta
10 % alfa
60 % alfa
90 % alfa
DifferentDifferent forgingforging and/orand/or
heatheat treatmenttreatment temperaturetemperature
areare adoptedadopted forfor thethe TiTi--66AlAl--44VV
alloyalloy alphaalpha--betabeta..900
950
T
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C
Regione
alfa + betaRegione alfaalloyalloy alphaalpha--betabeta..
TheThe higherhigher thethe temperaturetemperature
ofof treatment,treatment, thethe greatergreater isis thethe800
850
T
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C
Ti + 6Al
Regione alfa
ofof treatment,treatment, thethe greatergreater isis thethe
amountamount ofof betabeta phasephase thatthat
cancan bebe transformedtransformed inin
quenchingquenching andand temperingtempering..
750
0 2 4 6 8
Vanadio, % in peso
Ti + 6Al
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Heating Temperature
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AlloysAlloys + + The alloys + can be obtained with opportune composition; the percentage ranges from 10 to 50%. The heat treatment is solutionheat treatment, quench and tempering at temperature ranging fromheat treatment, quench and tempering at temperature ranging from480 and 650 C. The microstructure is a fine mixture of + in ametallic matrix of residual or transformed phase.
Property Beta processed Alfa/beta processedProperty Beta processed Alfa/beta processed
Strength Moderate Good
Creep Resistance Good Low950
1000
1050
1100
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Regione beta 100 % beta
10 % alfa
60 % alfa
90 % alfa
Creep Resistance Good Low
Fatigue Resistance Moderate Good
FractureToughness Good Low750
800
850
900
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Regione
alfa + beta
Ti + 6Al
Regione alfa
InIn thethe tabletable areare reportedreported thethe vantagesvantages andand disadvantagesdisadvantages
Rate of crack propagation Good Moderate
Grains size Coarse Fine
750
0 2 4 6 8
Vanadio, % in peso
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InIn thethe tabletable areare reportedreported thethe vantagesvantages andand disadvantagesdisadvantagesofof thethe twotwo treatmentstreatments..
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Microstructure Microstructure -- PropertiesPropertiesMicrostructure PropertiesMicrostructure Properties
Equiaxed
Higher ductility and HT deformability.
Higher minimal strength in stress corrosion cracking phenomena in
hot salt baths.
Higher strength (for equivalent heat treatments).Higher strength (for equivalent heat treatments).
Better fatigue resistance at low cycles (crack initiation)
Acicular
Higher properties of creep resistance.
High values of fracture toughness.
Slightly decrease in hardening (in case of the same heat treatment).
The properties of different alloys depend on their microstructures. The properties of different alloys depend on their microstructures.
Acicular Slightly decrease in hardening (in case of the same heat treatment).Higher stress corrosion cracking values.
Lower values of crack propagation.
The microstructure depends on chemical composition and heat The microstructure depends on chemical composition and heat
treatment. treatment.
The The microstructure microstructure can be:can be:
-- equiaxedequiaxed, obtained heating the alloy in the , obtained heating the alloy in the -- range and range and
annealed at lower temperatureannealed at lower temperature
-- acicular, obtained by mechanical working or heat treated over acicular, obtained by mechanical working or heat treated over
22/03/2010 Prof. G. Ubertalli
-- acicular, obtained by mechanical working or heat treated over acicular, obtained by mechanical working or heat treated over
transustransus temperature with a following rapid cooling (quench).temperature with a following rapid cooling (quench).
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Influence of treatment temperatureInfluence of treatment temperature
a b cForged at 900 C, below the
standard range. Equiaxed
alpha grains (light) and
mixed alpha-beta
Forged at 1005 C (standard
temperature range) air
cooled. Primary equiaxed
grains (white) in a beta
Forged at 1093 C, over the
beta transus temperature and
rapid cooling in air. Beta
transformed containing fine
a b c
Figures a, b, c: Microstructures observed on the Ti-8Al-1Mo-1V
mixed alpha-beta
microstructure (dark).grains (white) in a beta
transformed matrix (dark)
containing acicular alpha.
transformed containing fine
and coarse acicular
microstructure.
22/03/2010 Prof. G. Ubertalli
Figures a, b, c: Microstructures observed on the Ti-8Al-1Mo-1V
alloy after forging at the different temperature.
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Microstructure Microstructure Ti6Al4VTi6Al4V
Rolled alloy, annealed from Rolled alloy, annealed from + + Alloy as produced, quenched from Rolled alloy, annealed from Rolled alloy, annealed from + + range temperature.range temperature.
The microstructure is polygonal The microstructure is polygonal and and -- 500x500x
Alloy as produced, quenched from
+ range temperature.The microstructure is acicular and inside primary grains of -
22/03/2010 Prof. G. Ubertalli
and and -- 500x500x and inside primary grains of -500x
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MicrostructureMicrostructure Ti6Al4VTi6Al4VMicrostructureMicrostructure Ti6Al4VTi6Al4V
Alloy as produced, quenched Alloy as produced, quenched Rolled alloy, annealed from + Alloy as produced, quenched Alloy as produced, quenched from from + + range temperature.range temperature.The microstructure is constituted The microstructure is constituted
from from acicular acicular surrounded from surrounded from
Rolled alloy, annealed from + range temperature.
Microstructure is polygonal and - 500x.
22/03/2010 Prof. G. Ubertalli
from from acicular acicular surrounded from surrounded from fine lamellae of fine lamellae of -- 100x100x - 500x.
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40
++ alloys: alloys:
Microstructures Microstructures Microstructures Microstructures Contain significant
stabilisers to enable to be stabilisers to enable to be
retained to RT
Classic Ti alloy: Ti-6Al-4V
>50% of all Ti used >50% of all Ti used
Classically
1065 C all
forge @ 955C acicular forge @ 955C acicular
on grain boundaries to
inhibit coarsening
Air cool produce Air cool produce
lamellae colonies formed
in prior grains (minimise
strain), w/ in between
(think at the pearlite)(think at the pearlite)
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Mechanical propertiesMechanical properties
22/03/2010 Prof. G. Ubertalli
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42
TiTi--66--4: properties4: propertiesTiTi--66--4: properties4: properties
N.B. Must avoid Ti3Al formation
Al equivalent: Al+0.33 Sn + 0.16 Zr + 10 (O+C+2N) < 9 wt%
Precipitation
hardening
+ grain size
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43
Imperial College London
Page 43
TiTi--66--4: 4: TiTi--66--4: 4:
heat treatheat treat
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44
--Ti Alloy designTi Alloy design--Ti Alloy designTi Alloy designHard to completely stabilize
w.r.t. hexagonal phases
stabilisers: O, Al (N,C)
stabilisers: V,Mo,Nb,Si,Fe
neutral: Sn, Zr neutral: Sn, Zr
Strengthen near- alloys by
solid solution Fe,Nb,V
Hall-Petch
cold work
Uses: highly formable
Landing gear Landing gear
Auto bodies
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--AlloysAlloys
Highest strength Ti alloys Highest strength Ti alloys used in specialized used in specialized
applicationsapplications
Higher density because of Mo, V, Fe additionsHigher density because of Mo, V, Fe additions
Add Al to lower density and give solid solution strength Add Al to lower density and give solid solution strength
and high temperature oxidation resistanceand high temperature oxidation resistanceand high temperature oxidation resistanceand high temperature oxidation resistance
Easy to cold work (BCC) in solution treated and Easy to cold work (BCC) in solution treated and
quenchedquenched conditionconditionquenchedquenched conditioncondition
Can be subsequently aged to very high strengthsCan be subsequently aged to very high strengths
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--AlloysAlloys--AlloysAlloys
-- omega omega transition phase is brittletransition phase is brittle -- omega omega transition phase is brittletransition phase is brittle
TiTi--13%V13%V--11%Cr11%Cr--3%Al 3%Al onlyonly --alloyalloy producedproduced
in in largelarge quantitiesquantitiesin in largelarge quantitiesquantities
LimitedLimited useuse becausebecause ofof::
Relatively high density because of V, MoRelatively high density because of V, Mo Relatively high density because of V, MoRelatively high density because of V, Mo
Low ductility in high strength conditionLow ductility in high strength condition
In thick sections In thick sections chemical segregation; chemical segregation; In thick sections In thick sections chemical segregation; chemical segregation;
large grain size therefore low tensile ductility large grain size therefore low tensile ductility
and poor fatigue performanceand poor fatigue performance
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MicrostructureMicrostructure forfor
TiTi--13%V13%V--11%Cr11%Cr--3%Al3%Al
MicrostructureMicrostructure forfor
TiTi--13%V13%V--11%Cr11%Cr--3%Al3%Al
SolutionSolution treatedtreated at at
788788C C forfor 30min 30min 788788C C forfor 30min 30min
Water Water quenchedquenched
Metastable Metastable
phase (BCC)
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--Ti Alloys: SurveyTi Alloys: Survey
Strength and Selection of -Ti alloys
/ E
Landing Gear210-250105970-1170Ti 10 V 2Fe 3Al
y/y E
Springs163-21970-103780-1050Ti 15V 3Cr 3Al 3Sn
Springs (Beta C)17188
825Ti 3Al 8V 6Cr 4Mo 4Zr
Low Cost Beta (LCB)
Development of Beta C
250-290110950-1400Ti 4.5Fe 6.8Mo 1.5Al
Springs163-21970-103780-1050Ti 15V 3Cr 3Al 3Sn
Development of Beta C
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ApplicationsApplications in in medicalmedical fieldsfields
HipHip prosthesisprosthesis
AorticAortic ValvesValves AorticAortic ValvesValves
PeacemakerPeacemaker PeacemakerPeacemaker
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50
DentalDental applicationsapplicationsDentalDental applicationsapplications
Dental prosthesisDental prosthesis
Dental plantsDental plants
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51
AutomotiveAutomotive applicationsapplicationsAutomotiveAutomotive applicationsapplications
ValvesValves ValvesValves
ConnectingConnecting rodsrods ConnectingConnecting rodsrods
Exhaust gas systemExhaust gas system Exhaust gas systemExhaust gas system
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52
Shock absorbersShock absorbersShock absorbersShock absorbersSpring mass calculationSpring mass calculation::
C
FGm
maz
f
2
2
2
Applications
Year Components Material Company Type Use/Year
1998
1998
Brake pin
Flat washers
Grade 2
Grade 1s
Mercedes-Benz
Volkswagen
S-class
All
~ 8 t/yr
~ 40 t/yr1998
1998
1999
1999
1999
2000
Flat washers
Knob of the gearbox
Connecting rod
Valves
Rotor for turbocharger
Absorber springs
Grade 1s
Grade 1
Ti-6Al-4V
Ti-6Al-4V
Ti-6Al-4V
LCB
Volkswagen
Honda
Porsche
Mercedes-Benz
Volkswagen
Mitsubishi
All
S2000 Roadster
GT3
Heigth 6-cil.
Truck
Lupo FSI
~ 40 t/yr
n/a
~ 1 t/yr
n/a
n/a
3-4 t/yr2000
2000
2000
2001
2002
Absorber springs
Sump valve
Rotor for turbocharger
Exhaust gas system
Valves
LCB
Alloy
TiAl
Grade 2
Ti-6Al-4V
Mitsubishi
Mitsubishi
General Motors
Nissan
Lupo FSI
All 1.8l-4 cil.
Lancer
Corvette Z06
Infinity Q 45
3-4 t/yr
n/a
n/a
> 150 t/yr
n/a2002 Valves Ti-6Al-4V Infinity Q 45 n/a
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SeaSea applicationsapplicationsSeaSea applicationsapplications
Rotary Rotary drillingdrilling systemssystems
Submarine coatingsSubmarine coatings
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54
AerospaceAerospace SectorSectorAerospaceAerospace SectorSector
FigthersFigthers airplanesairplanes
Gas compressor deviceGas compressor device
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55
Page 55
Fan Blade TechnologyFan Blade TechnologyFan Blade TechnologyFan Blade Technology
+ 4% efficiency+ 4% efficiencyClappered + 4% efficiency+ 4% efficiencyClappered Wide-chord fan
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56
Page 56WideWide--chord Fan Technologychord Fan Technology
1st generation:
1984
2nd generation:
1995
Honeycomb
construction
DB/SPF
construction
-
57
Page 57Fan SectionFan Section
-
58
Page 58
Swept FansSwept FansSwept FansSwept Fans
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59
Tank of ShuttleTank of Shuttle Tank of ShuttleTank of Shuttle
Retractable undercarriage of Boeing 747Retractable undercarriage of Boeing 747 Retractable undercarriage of Boeing 747Retractable undercarriage of Boeing 747
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60
At 570 At 570 C it is preferred to substitute C it is preferred to substitute At 570 At 570 C it is preferred to substitute C it is preferred to substitute
the Ti alloys with Ni base alloys for the the Ti alloys with Ni base alloys for the
following reasons:following reasons:following reasons:following reasons:
Temperature too high for their properties.Temperature too high for their properties. Temperature too high for their properties.Temperature too high for their properties.
The cares that titanium could evidenced The cares that titanium could evidenced
some burning or flash phenomena.some burning or flash phenomena.some burning or flash phenomena.some burning or flash phenomena.
Oxidation problems for titanium, consequent Oxidation problems for titanium, consequent
oxygen enrichment of phase and lose of oxygen enrichment of phase and lose of oxygen enrichment of phase and lose of oxygen enrichment of phase and lose of
some properties (ductility).some properties (ductility).
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61
EnergyEnergy
Heat exchangers, radiatorsHeat exchangers, radiators
Fan vapor turbinesFan vapor turbines
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62
TitaniumTitanium in in tankstanksTitaniumTitanium in in tankstanks
M1 M1 AbramsAbrams M1 M1 AbramsAbrams
Armor plating propertiesArmor plating propertiesArmor plating propertiesArmor plating properties STEEL
PHA MIL-A-12560
ALUMI#IUM 5083
MIL-A-46026 Ti-6Al-4V
MIL-A-46077
Tensile strength (MPa) 1170 350 970 Tensile strength (MPa) 1170 350 970
Density (g/cm3) 7.86 2.70 4.50
Specific strength
(MPa / cm3/g)
150 130 220
(MPa / cm /g)
Mass efficiency (Em) 1 1.0-1.2 1.5
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63
Building Building applicationsapplications
The properties of titanium in architecture are:The properties of titanium in architecture are:
ThermalThermal dilatationdilatation:: TitaniumTitanium hashas aa coefficientcoefficient veryvery lowlowandand thereforetherefore isis lessless influencedinfluenced fromfrom thethe seasonseasonchangechange ofof temperaturetemperature andand aa consequentconsequent higherhigherchangechange ofof temperaturetemperature andand aa consequentconsequent higherhigherdimensionaldimensional andand geometricalgeometrical stabilitystability..
TitaniumTitanium dodo notnot changechange colourcolour asas aa consequenceconsequence ofofultravioletultraviolet raysrays andand dodo notnot evidenceevidence pittingpitting corrosioncorrosionultravioletultraviolet raysrays andand dodo notnot evidenceevidence pittingpitting corrosioncorrosioninducedinduced fromfrom seawaterseawater environmentenvironment oror fromfrom acidacid rainsrains..
GoodGood resistanceresistance atat thethe environmentenvironment:: thethe changechange ofoftemperaturetemperature andand thethe presencepresence ofof pollutionpollution dodo notnottemperaturetemperature andand thethe presencepresence ofof pollutionpollution dodo notnotinfluenceinfluence thethe corrosioncorrosion resistanceresistance ofof titanium,titanium, thatthat ininveryvery highhigh..
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Guggenheim Guggenheim MuseumMuseum in in BilbaoBilbao Guggenheim Guggenheim MuseumMuseum in in BilbaoBilbao
Van Van GoghGogh MuseumMuseum Van Van GoghGogh MuseumMuseum
National Center National Center ofof Science Science in in ScotlandScotland National Center National Center ofof Science Science in in ScotlandScotland
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The The titaniumtitanium in sportin sportThe The titaniumtitanium in sportin sport
GolfGolfGolfGolf
CyclingCyclingCyclingCycling
DivingDivingDivingDiving
TrekkingTrekkingTrekkingTrekking
Winter SportWinter SportWinter SportWinter Sport
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66
OtherOther applicationsapplicationsOtherOther applicationsapplications
Jewellery and fashionJewellery and fashion Jewellery and fashionJewellery and fashion
SafetySafety SafetySafety
NanotechnologyNanotechnology
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ComponentsComponents IIComponentsComponents II
CastCast technologytechnology..
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ComponentsComponents IIIIComponentsComponents IIII
CastCast technologytechnology.. CastCast technologytechnology..
22/03/2010 Prof. G. Ubertalli
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High temperature High temperature propertiesproperties asas
comparedcompared toto steelssteelscomparedcompared toto steelssteels
Tensile strength of different Tensile strength of different Specific tensile strength of different
22/03/2010 Prof. G. Ubertalli
Tensile strength of different Tensile strength of different
metallic alloys at different metallic alloys at different
temperature.temperature.
Specific tensile strength of different
metallic alloys at different
temperature.
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70
Ti Creep RatesTi Creep Rates
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71
ComparisonComparison 2 2
High High
TheThe mechanicalmechanical propertiesproperties atat highhightemperaturetemperature ofof titaniumtitanium alloysalloys arearemainlymainly thatthat ofof alphaalpha oror nearnearalphaalpha alloysalloys.. WheneverWhenever thethe creepcreep High High
temperaturetemperature
alphaalpha alloysalloys.. WheneverWhenever thethe creepcreepphenomenaphenomena isis notnot soso importantimportant atathighhigh temperature,temperature, thethe tensiletensilestrengthstrength ofof betabeta alloys,alloys, atat highhightemperaturetemperature forfor shortshort time,time, isis
temperaturetemperaturetemperaturetemperature forfor shortshort time,time, isishigherhigher..
InIn factfact thesethese alloys,alloys, untiluntil aboutabout425425 C,C, havehave higherhigher specificspecifictensiletensile strengthstrength thanthan HH1111 tooltooltensiletensile strengthstrength thanthan HH1111 tooltoolsteels,steels, whilewhile alphaalpha andand nearnear alphaalphaalloysalloys areare notnot inin advantageadvantage..
ForFor longlong timetime applicationsapplications thethealphaalpha andand nearnear alphaalpha alloysalloys havehavealphaalpha andand nearnear alphaalpha alloysalloys havehavesubstitutedsubstituted thethe steelssteels ininaeronauticalaeronautical turbinesturbines..
InIn figurefigure areare plottedplotted thethe curvescurves ofofspecificspecific tensiletensile strengthstrength ofof twotwospecificspecific tensiletensile strengthstrength ofof twotwotitaniumtitanium alloysalloys adad threethree steelssteelsadoptedadopted forfor aeronauticalaeronautical turbines,turbines,inin thethe averageaverage lowlow temperaturestemperaturesrangerange.. InIn comparisoncomparison withwith steels,steels,
22/03/2010 Prof. G. Ubertalli
rangerange.. InIn comparisoncomparison withwith steels,steels,thethe titaniumtitanium alloysalloys havehave higherhigherpropertiesproperties untiluntil 540540 CC..
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72
SuperSuper--plasticityplasticitySuperSuper--plasticityplasticity
AtAt highhigh temperaturetemperature ((870870925925 C,C,withoutwithout exceedingexceeding thethe betabeta--
1200
withoutwithout exceedingexceeding thethe betabeta--transustransus)) somesome alloysalloys evidenceevidence thethesupersuper--plasticityplasticity phenomenaphenomena.. ToToinduceinduce thisthis behaviourbehaviour somesome wellwelldefinedefine conditionsconditions areare neededneeded:: 800
1000
definedefine conditionsconditions areare neededneeded::
VeryVery finefine graingrain dimensionsdimensions (about(about1010 mm size)size)..RelativelyRelatively highhigh temperaturetemperature (higher(higher
600
800
A
l
l
u
n
g
a
m
e
n
t
o
,
%
RelativelyRelatively highhigh temperaturetemperature (higher(higherthanthan 11//22 thethe meltingmelting temperaturetemperature K)K)..
AA controlledcontrolled deformationdeformation raterate(generally(generally fromfrom 00..00010001 toto 00..0101 ss--11))..
AA twotwo phasephase microstructuremicrostructure (( andand 200
400
A
l
l
u
n
g
a
m
e
n
t
o
,
%
Ti-6Al-4V
Ti-6Al-4V-2NiAA twotwo phasephase microstructuremicrostructure (( andand inin titanium)titanium)..
0
200
0 20 40 60 80 100
Ti-6Al-4V-2Ni
Ti-6Al-2Sn-4Zr-2Mo
Ti-8Mn
Valori minimi
Valori massimi
22/03/2010 Prof. G. Ubertalli
InIn figurefigure isis evidencedevidenced suchsuch influenceinfluence..
0 20 40 60 80 100
Contenuto di beta, vol.%
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73
Fracture toughness of TitaniumFracture toughness of TitaniumFracture toughness of TitaniumFracture toughness of Titanium
TheThe fracturefracture toughnesstoughness valuesvalues80
TheThe fracturefracture toughnesstoughness valuesvaluescancan bebe improvedimproved byby aa factorfactor 22 oror33 forfor TiTi alloys,alloys, ifif thethe appropriateappropriateheatheat treatmenttreatment andand chemicalchemicalcompositioncomposition areare chosenchosen
60
T
e
n
a
c
i
t
a
f
r
a
t
t
u
r
a
[
M
P
a
m
]
compositioncomposition areare chosenchosen(microstructure(microstructure andand preferredpreferredorientation)orientation).. 40
T
e
n
a
c
i
t
a
f
r
a
t
t
u
r
a
[
M
P
a
m
]
Ti-6Al-4V piastra
Ti-6Al-4V getto
HoweverHowever OxygenOxygen mustmust bebemaintainedmaintained lowlow;; iitt isis alwaysalways ananimpurityimpurity..
20Te
n
a
c
i
t
a
f
r
a
t
t
u
r
a
[
M
P
a
m
]
Ti-6Al-4V getto
Ti-17 (a-b) processato
Ti-17 b processato
Beta III
Valori minimi
0
700 900 1100 1300
Snervamento [MPa]
Valori massimi
22/03/2010 Prof. G. Ubertalli
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74
SSchemecheme ofof propertiesproperties
Ti 834 Ti-6Al-2Sn-4Zr- Ti-6Al-2Sn-4Zr-2Mo Ti 17
2Mo-0,8Si 2Mo-0,8Si TA5E IMI 685 Betacez
transus
Ti-6Al-4V
Deformability
Flusso
tensioniStrain rate sensitivity
Weldability Hardeability
HighT strength Room T strength
22/03/2010 Prof. G. Ubertalli
Leghe Leghe "near" Leghe + Leghe "near" Leghe
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75
P/M Ti alloys?P/M Ti alloys?P/M Ti alloys?P/M Ti alloys?
Have been produced: would be useful in Have been produced: would be useful in
e.g. controlling grain size in pure
forging
BUT: problem of avoiding oxide layer on
powder particles and consequent TiOpowder particles and consequent TiO2
and inclusions
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76
SinteredSintered components toughnesscomponents toughness
60
65
[
M
p
a
m
]
50
55
60F
r
a
t
t
u
r
e
t
o
u
g
h
n
e
s
s
K
Q
[
M
p
a
m
]
40
45
50
F
r
a
t
t
u
r
e
t
o
u
g
h
n
e
s
s
40
94 95 96 97 98 99 100
F
r
a
t
t
u
r
e
t
o
u
g
h
n
e
s
s
Density % of theoretical
EffectEffect ofof density on density on fracturefracture toughnesstoughness ofof sinteredsintered
Ti6Al4V Ti6Al4V partsparts. .
22/03/2010 Prof. G. Ubertalli
Ti6Al4V Ti6Al4V partsparts. .