An Update on Properties and Applications for Ti-5Al-5Mo-5V-3Cr · International Titanium...
Transcript of An Update on Properties and Applications for Ti-5Al-5Mo-5V-3Cr · International Titanium...
International Titanium AssociationInternational Titanium AssociationScottsdale 2005Scottsdale 2005
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An Update on Properties and Applications for Ti-5Al-5Mo-5V-3Cr
International Titanium AssociationInternational Titanium AssociationScottsdale 2005Scottsdale 2005
TiTi--55535553• Evolved from Russian alloy, VT-22
– Commonly used for airframe structural forgings– Applications in Ilyushin, Tupolev, Antonov, Yakovlev aircraft
• 1995/1996 – VSMPO began work with Boeing– Goal: Higher strength / lower cost than 10V-2Fe-3Al– Candidate alloy for forged, landing gear components– Led to development of VST-5553 (Ti-5553)
• Selected for applications on 787– Landing gear components– Airframe structural components
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TiTi--55535553Advantages Over Ti-10V-2Fe-3Al
• Less prone to segregation• Higher strength; ~15%• Better hardenability in thick sections
– Up to 6” section thickness vs. 3” for 10V-2Fe-3Al– Potentially lower machining costs
• Air cool vs. water quench– Potentially less distortion
• Able to use higher % level of revert
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Chemical Composition
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Chemical CompositionChemical Composition
1.5
0.5
Fe
1.55.55.55.7Basemax
0.54.04.04.4Basemin
CrVMoAlTiVT22
0.50
0.30
Fe
3.55.55.55.7Basemax
2.54.04.04.4Basemin
CrVMoAlTiTi-
5553
Higher Cr
Lower Fe
VT22 vs. TiVT22 vs. Ti--55535553
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Heat Treat Conditions
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TiTi--55535553Heat Treat Conditions
• Solution treat and age (STA)– Typical cycle: βt-60F, 2 Hrs, A.C.; Age @ 1100F,
8 Hrs, A.C.– High strength applications (180 KSI)– Landing Gear Applications
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Ti-5Al-5Mo-5V-3CrHeat Treat Conditions
• β anneal, slow cool and age (BASCA)– Typical cycle: βt+50F, 1 Hr, F.C. @ 5F/min; Age
@ 1050F, 8 Hrs, A.C.– Lower strength (160 KSI) but much better fatigue– Used on airframe structural components
• Enables design with thinner cross-sections = weight reduction
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Ti 5Al-5Mo-5V-3CrHeat Treat Conditions
• Beta-forged, solution treat and age– Forge above beta-transus– Standard STA heat treat cycle– Similar properties to BASCA with the advantage
of closer-to-net forging design
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Mechanical Properties
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TiTi--5553 Forging Properties5553 Forging Properties
Ti 6Al4VTi 6Al4V Ti 5553Ti 5553Ti 10V2Fe3AlTi 10V2Fe3Al
YS, MPa (KSI)YS, MPa (KSI)
UTS, MPa (KSI)UTS, MPa (KSI)
El, %El, %
KK1C1C, MPa Vm (KSI Vin), MPa Vm (KSI Vin)
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MECHANICAL PROPERTIESMECHANICAL PROPERTIESTiTi--6Al6Al--4V vs. Ti4V vs. Ti--5Al5Al--5Mo5Mo--5V5V--3Cr3Cr
160 KSI Condition160 KSI Condition
0
50
100
150
200
KSI
VST 5553 STA 165 145 6 60 37VST 5553 BASCA 160 140 6 70 40Ti-6Al-4V AMS 4928 130 120 10 60 35.4
Ftu Fty %El K1c da/dN
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Dynamic Property EvaluationsDynamic Property EvaluationsTi-5553 LCF Behavior
0
0.2
0.4
0.6
0.8
1
1.2
1.E+03 1.E+04 1.E+05 1.E+06
Cycles to Failure
Max
Str
ain,
%
r = 0.1
Cast Ti-5553
Cast Ti-64
Source: The Boeing Company
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Machining
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Ti 5553 MachiningTi 5553 Machining• Machining parameters still being
developed– Trials being performed by various end-users– No parts have been machined in production– Cutting tools still being optimized– So, much is yet to be defined
• But in general we can say…– 180 KSI material machines comparably to Ti 10-2-3– 160 KSI material machines much better than 180 KSI
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Ti 5553 MachiningTi 5553 Machining• Machine performance vs. Ti-6Al-4V
– ~ 20% - 30% lower metal removal rates than Ti-6Al-4V
– Tool life 10% - 20% shorter than for Ti 6Al-4V– Carbide inserts do not perform well– Solid cobalt cutters seem to be the best choice
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Current Applications
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Ti 5553 ForgingsTi 5553 Forgings• ~20% of 787 primary structure is
titanium– Ti-5553 makes up a significant portion of this
volume, mostly in forgings
• ~75 configurations – landing gear & airframe structural– Forging weights range from 23kg (50 lbs) to 2600 kg
(5700 lbs)– Sizes range from 400mm (16”) to 5700mm (225”)
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787 Forgings FromTi787 Forgings FromTi--55535553
Size: 2448 x 622 x 550 mmWeight: 1145 kg
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787 Forgings FromTi787 Forgings FromTi--55535553
Size: 2101 x 434 x 320 mmWeight: 980 kg
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787 Forgings FromTi787 Forgings FromTi--55535553
Size: 782 x 295 x 135 mmWeight: 53 kg
Size: 675 x 479 x 158 mmWeight: 96 kg
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787 Forgings FromTi787 Forgings FromTi--55535553
Overall size: 5688 х 555 х 376 mmWeight: 2610 kg (β – die forging)
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787 Forgings FromTi787 Forgings FromTi--55535553
Overall size: 1170 x 663 x 254 mmWeight: 276 kg (β – die forging)
Overall size: 1807 x 426 x 273 mmWeight: 158 kg (β – die forging)
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Other Applications
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TiTi--5553 Applications5553 Applications
• Investment casting– Comparable to Ti-6242 and Ti-15-3-3-3 in
castability– Higher strength and better fatigue than Ti 6-4
• Plate product– Demonstrated good strength and K1C
properties
• Extrusions – 787 applications
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Ti 5AlTi 5Al--5Mo5Mo--5V5V--3Cr3CrSummary
• Alloy entering into full production• Two heat treat conditions developed – 180 KSI
and 160 KSI• Widely used in forgings throughout the 787
airplane• Potential use in castings, plate and extrusions
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