FabDigit

Titanium Ti-17

UNS R58650 · GB TC17

Ti-17 (UNS R58650, TC17) is a deep-hardening, beta-rich alpha-beta titanium alloy developed for large jet-engine fan and compressor disks.

High cost $$$$

Reference datasheet — Ti-17 is not in the instant-quote catalog. Upload your part and an engineer will quote it in this grade or suggest the closest stocked equivalent.

Values for the STA condition

Ti-17 tempers and conditions

Ti-17 is supplied in 5 conditions, soft to hard. STA is the default FabDigit quotes; the values on this page are for it.

Compare all 5 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
Solution annealed
Supplied for further hot working, machining of near-net shapes or straightening before the customer performs the ageing cycle.8809501531 HRC1 % IACS
As-forged / mill-annealed billet and bar
Raw billet, bar and forging stock condition sold for onward forging; not a design-strength condition.9301,0201233 HRC1 % IACS
Overaged
Used where dimensional/thermal stability and toughness matter more than peak strength, e.g. large stabilised disk forgings.9501,0301234 HRC1 % IACS
Beta solution treated (above beta transus ~890-900 °C) and aged
Choose when maximum fracture toughness and crack-growth resistance in very thick sections outweigh a modest loss of ductility and fatigue strength.1,0201,100736 HRC1 % IACS
STADefault
Solution treated and aged
Standard high-strength condition for fan/compressor disks and thick forgings needing strength plus good LCF life.1,0751,1501037 HRC—

What is Ti-17?

Ti-17 (UNS R58650, TC17) is a deep-hardening, beta-rich alpha-beta titanium alloy developed for large jet-engine fan and compressor disks. It combines high strength with fracture toughness in thick sections, giving 1075 MPa yield, 1150 MPa tensile, 10% elongation and 37 HRC in STA, with service to 350 °C; it is supplied as billet, forgings and rings in STA, BSTA, ST, OA and as-forged conditions. Machinability is low (score 16), cold forming is impractical and welding is normally excluded from critical rotating hardware. Ti-6Al-2Sn-4Zr-6Mo is the closest alternative where higher temperature capability is needed. Ti-17 has a density of 4.65 g/cm³ (0.168 lb/in³), heavier than 90% of titanium grades. It melts at 1,600°C (2,912 °F). Ti-17 has a yield strength of 1,075 MPa (156 ksi) and a tensile strength of 1,150 MPa (167 ksi) — stronger than 98% of titanium grades. Elongation at break is 10% and the elastic modulus is 112 GPa (16.2 Msi).

What is Ti-17 used for?

  • jet engine fan disks
  • compressor disks
  • high-strength rotating parts

Advantages

  • High strength — 1,075 MPa (156 ksi), better than 98% of titanium grades

Limitations

  • Difficult to weld — 30/100, worse than 98% of titanium grades
  • Limited ductility — 10%, worse than 93% of titanium grades
  • Limited formability — 15/100, worse than 93% of titanium grades
  • Low fracture toughness — 55 MPa·√m (50.1 ksi·√in), worse than 90% of titanium grades

Ti-17 properties

Typical room-temperature values for Ti-17-STA; bars are the position among titanium grades.

Physical3

Ti-17 has a density of 4.65 g/cm³ (0.168 lb/in³), heavier than 90% of titanium grades. It melts at 1,600°C (2,912 °F).

Density4.65 g/cm³0.17 lb/in³
Melting Point (Solidus)1,600°C2,912 °F
Liquidus Temperature1,650°C3,002 °F

Mechanical15

Ti-17 has a yield strength of 1,075 MPa (156 ksi) and a tensile strength of 1,150 MPa (167 ksi) — stronger than 98% of titanium grades. Elongation at break is 10% and the elastic modulus is 112 GPa (16.2 Msi).

Elastic (Young's) Modulus112 GPa16.2 Msi
Shear Modulus42.5 GPa6.2 Msi
Bulk Modulus104 GPa15.1 Msi
Poisson's Ratio0.32
Tensile Strength (Ultimate)1,150 MPa167 ksi
Yield Strength (0.2% offset)1,075 MPa156 ksi
Elongation at Break10%
Reduction in Area25%
Compressive Strength1,150 MPa167 ksi
Shear Strength700 MPa102 ksi
Fatigue Strength (Endurance Limit)600 MPa87 ksi
Fracture Toughness (K_IC)55 MPa·√m50.1 ksi·√in
Charpy V-Notch Impact (RT)17 J12.5 ft·lbf
Hardness, Rockwell C37 HRC
Hardness, Vickers365 HV

Thermal6

Ti-17 is rated for continuous service to 350°C (662 °F). It conducts heat at 7 W/m·K (4.04 BTU/hr·ft·°F), worse than 76% of titanium grades. Thermal expansion is 9.4 µm/m·K (5.22 µin/in·°F).

Thermal Conductivity7 W/m·K4 BTU/hr·ft·°F
Specific Heat Capacity500 J/kg·K0.12 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)9.4 µm/m·K5.2 µin/in·°F
Latent Heat of Fusion325 J/g140 BTU/lb
Max Service Temperature (continuous)350°C662 °F
Min Service Temperature-100°C-148 °F

Electrical2

Ti-17 has an electrical resistivity of 1.7×10⁻⁶ Ω·m.

Electrical Resistivity1.7×10⁻⁶ Ω·m66.9 µΩ·in
Magnetic Responsenon-magnetic

Chemical & Environmental3

Corrosion resistance is excellent (85/100), worse than 93% of titanium grades.

Galvanic Potential (seawater, vs SCE)-0.1 V
Corrosion ResistanceExcellent85/100
Chemical Resistance SummaryExcellent in seawater, chlorides, oxidizing acids and most industrial atmospheres thanks to the TiO2 film; attacked by HF, hot concentrated HCl/H2SO4 and dry chlorine, and susceptible to hot-salt stress corrosion above ~300 °C.

Sustainability4

Producing a kilogram of Ti-17 takes about 680 MJ of energy and emits 42 kg of CO₂ — more than 51% of titanium grades. Typical recycled content is 20%.

Embodied Energy (primary production)680 MJ/kg292,348 BTU/lb
Embodied Carbon (primary production)42 kg CO₂/kg
Embodied Water500 L/kg59.9 gal/lb
Typical Recycled Content20%

Manufacturability7

Ti-17's machinability is poor (16/100, worse than 93% of titanium grades); weldability poor (30/100); formability poor (15/100).

MachinabilityPoor16/100
Machinability Rating (AISI 1212 = 100 %)15%
WeldabilityPoor30/100
Formability (cold)Poor15/100
Brazeability / SolderabilityFair35/100
PolishabilityVery good70/100
Anodizing Responsegood — anodic (Type II/AMS 2488 chemical or anodic) treatments give coloured, wear-resistant oxide used for anti-galling on titanium hardware; not a decorative aluminium-style anodize

Common Calculations5

Specific Strength (UTS / density)calculated247 kN·m/kg
Specific Stiffness (E / density)calculated24.1 MN·m/kg
Modulus of Resiliencecalculated5,159 kJ/m³
Thermal Diffusivitycalculated3 mm²/s
Thermal Shock Resistance Indexcalculated8

Values are nominal handbook figures for design screening. Certified mill or lot data ships with every FabDigit order on request.

Strength versus weight in the titanium family

Yield strength against density for every titanium grade FabDigit runs. Ti-17 is highlighted; hover a dot for its name, or open the interactive family chart.

3005007001,0004.555.5Density (g/cm³)Yield strength (MPa) — log scaleTi-17

Working with Ti-17

Is Ti-17 easy to machine?

Machine like a hard beta-rich titanium: rigid setup, sharp uncoated-carbide or coated inserts, ~15-30 m/min in the aged condition, heavy flood coolant, positive rake and no dwelling to avoid work hardening and edge notching.

Can Ti-17 be welded?

GTAW/EBW is metallurgically possible with full inert or vacuum shielding, but the aged HAZ loses ductility, so post-weld solution+age is required and welding is normally excluded from critical rotating hardware.

Can Ti-17 be formed, bent or molded?

Essentially a hot-work alloy — forge/ring-roll just below or above the beta transus (~850-925 °C) with controlled cooling; cold forming is impractical, so bends and rings are made hot or by machining.

Ti-17 chemical composition (wt %)

Limits by weight percent from the governing specification, written the way the spec states them — a single maximum for impurities, a range for alloying elements, and the base element as balance. Nominal is the typical mid-range value.

ElementSpec limit (wt %)Nominal
Alalpha stabilizer4.5 – 5.55
Sn1.6 – 2.42
Zr1.6 – 2.42
Mobeta stabilizer, deep hardenability3.5 – 4.54
Crbeta stabilizer3.5 – 4.54
Fe≤ 0.3
Ocontrolled range0.08 – 0.130.11
C≤ 0.05
N≤ 0.05
H≤ 0.01
Simax (some specs)≤ 0.15
Tibalance

What surface finishes work on Ti-17?

Shot peen or low-stress grind highly loaded surfaces; anodic/AMS 2488 conversion coatings, ion plating or dry-film lube prevent galling, and pickling must avoid hydrogen pickup.

Surface treatments FabDigit runs on titanium parts — pick them in the quote configurator or call them out on the drawing. Each links to its datasheet in the surface-finish library (thickness, specs, call-out, material verdicts).

Thermal Spray

Equivalent designations

Standards and trade names that resolve to Titanium Ti-17 in FabDigit's catalog. Equivalence is nominal — check the exact specification when certification matters.

UNS
R58650
GB (China)
TC17
Other
4970

How much does Ti-17 cost?

Ti-17 is a high-cost titanium ($$$$), pricier than about 78% of the materials FabDigit quotes. Part price depends far more on geometry, tolerance and quantity than on the raw stock — upload a CAD file for a live quote.

Ti-17 — frequently asked

What is Ti-17 used for?

Ti-17 is typically used for jet engine fan disks, compressor disks and high-strength rotating parts. In short: deep-hardening disk alloy; high fracture toughness; hot-work only, no cold forming.

What is the yield strength of Ti-17?

Ti-17 has a typical yield strength of 1,075 MPa (156 ksi) and a tensile strength of 1,150 MPa (167 ksi) — stronger than 98% of titanium grades. Strength varies by condition: see the 5 listed tempers.

Is Ti-17 easy to machine?

Not especially — machinability is rated poor (16/100, worse than 93% of titanium grades). Machine like a hard beta-rich titanium: rigid setup, sharp uncoated-carbide or coated inserts, ~15-30 m/min in the aged condition, heavy flood coolant, positive rake and no dwelling to avoid work hardening and edge notching.

Can Ti-17 be welded?

Not readily — weldability is rated poor (30/100). GTAW/EBW is metallurgically possible with full inert or vacuum shielding, but the aged HAZ loses ductility, so post-weld solution+age is required and welding is normally excluded from critical rotating hardware.

What surface finishes work on Ti-17?

Shot peen or low-stress grind highly loaded surfaces; anodic/AMS 2488 conversion coatings, ion plating or dry-film lube prevent galling, and pickling must avoid hydrogen pickup.

Can Ti-17 be formed, bent or molded?

Essentially a hot-work alloy — forge/ring-roll just below or above the beta transus (~850-925 °C) with controlled cooling; cold forming is impractical, so bends and rings are made hot or by machining.

What is the maximum service temperature of Ti-17?

Ti-17 is rated for continuous use to about 350°C (662 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

What is the difference between Ti-17-STA and Ti-17-ST?

STA is the default condition — standard high-strength condition for fan/compressor disks and thick forgings needing strength plus good LCF life. ST: supplied for further hot working, machining of near-net shapes or straightening before the customer performs the ageing cycle. Yield strength is 1,075 MPa in STA versus 880 MPa in ST.

How much does Ti-17 cost?

Ti-17 is a high-cost titanium ($$$$), pricier than about 78% of the materials FabDigit quotes. Part price depends far more on geometry, tolerance and quantity than on the raw stock — upload a CAD file for a live quote.

Sources

  1. AMS 4995 — Titanium Alloy Forgings Ti-5Al-2Sn-2Zr-4Mo-4Cr, Solution and Precipitation Heat Treated — SAE International (2019)
  2. AMS 4970 — Titanium Alloy Bars, Forgings and Rings Ti-5Al-2Sn-2Zr-4Mo-4Cr — SAE International (2018)
  3. Materials Properties Handbook: Titanium Alloys — ASM International (1994)
  4. ASM Handbook Vol. 2 — Properties and Selection: Nonferrous Alloys and Special-Purpose Materials — ASM International (1990)
  5. GB/T 2965 / TC17 (2007)
  6. Ti-17 (TC17) forging billet datasheets (2023)

Property data is compiled from published supplier and standards handbooks and normalised for comparison; hardness values on non-Brinell scales are converted approximately for charting only. Manufacturability limits are FabDigit quote-engine defaults and may be relaxed by engineering review. Nothing on this page is a certification — request mill certs, CoC or material test reports with your order.