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Material Specification

Grade 23

Grade 23 Fasteners
Extra Low Interstitial Ti-6Al-4V – Fracture Toughness and Implant Grade

Titanium Grade 23 (Ti-6Al-4V ELI) Fasteners

Buy Titanium Grade 23 (Ti-6Al-4V ELI / UNS R56401 / ASTM B348 Grade 23) bolts, screws, machined components and implant hardware from Exotic Alloy. Grade 23 is Ti-6Al-4V held to extra low interstitial limits — oxygen capped at 0.13% against Grade 5’s 0.20%, hydrogen at 0.0125% against 0.015%, iron at 0.25% against 0.40% and aluminium at 6.5% against 6.75%. The result is improved ductility and fracture toughness at a modest cost in strength.

Exotic Alloy manufactures Grade 23 components to ASTM B348, ASTM B265, ASTM F136 for surgical implant applications and ASTM F467 and F468 for nonferrous nuts and bolts, in metric M3–M36 and imperial #4–1½" sizes, with full EN 10204 3.1 material test certificates for fracture-critical airframe structure, offshore tubulars and medical applications.

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Product Range

Grade 23 Fasteners Available

Grade 23 Hex Bolts
Grade 23
Hex Bolts
Grade 23 Heavy Hex Bolts
Grade 23
Heavy Hex Bolts
Grade 23 Stud Bolts
Grade 23
Stud Bolts
Grade 23 Threaded Rods
Grade 23
Threaded Rods
Grade 23 Anchor Bolts
Grade 23
Anchor Bolts
Grade 23 Hex Nuts
Grade 23
Hex Nuts
Grade 23 Washers
Grade 23
Washers
Grade 23 Cotter Pins
Grade 23
Cotter Pins
Grade 23 Springs
Grade 23
Springs
Grade 23 Circlips
Grade 23
Circlips
Grade 23 Coated Fasteners
Grade 23
Coated Fasteners
Grade 23 Custom Spacers
Grade 23
Custom Spacers
Technical Data

Grade 23 Specifications

Chemical Composition — Titanium Grade 23 (Ti-6Al-4V ELI) (wt. %)
ElementTiAlVOFeNCH
Min %Balance5.503.50–––––
Max %Balance6.504.500.130.250.030.080.0125
Mechanical Properties — Titanium Grade 23 (Ti-6Al-4V ELI)
ConditionUTS (MPa)YS 0.2% (MPa)Elongation (%)Hardness
ASTM B348 Minimum≥ 828 (120 ksi)≥ 759 (110 ksi)≥ 10 in 4D–
Reduction of Area, Minimum–––≥ 15%
Annealed (Typical)900–970830–90012–18–
Alloy Class–––Alpha-beta, extra low interstitial
Physical Properties
Density4.42 g/cm³
Modulus of ElasticityApproximately 114 GPa
Melting RangeApproximately 1604–1660°C
Thermal ConductivityApproximately 6.7 W/m·K at 20°C
Maximum Service TemperatureApproximately 400°C
Oxygen Limit0.13% max — against 0.20% for Grade 5
Equivalent Grades & Standards
UNSWerkstoff / DINASTM DesignationCommon Name
R56401 – ASTM B348 Grade 23 / ASTM F136 Ti-6Al-4V ELI

Key Specifications: ASTM B348 (Bar & Billet) / ASTM B265 (Plate, Sheet & Strip) / ASTM B381 (Forgings) / ASTM F136 (Wrought Ti-6Al-4V ELI for Surgical Implant Applications) / ASTM F467 and F468 (Nonferrous Nuts and Bolts). The standard-interstitial version is Grade 5.

Machinability: titanium’s low thermal conductivity is the governing problem — the heat generated at the cut stays at the cutting edge instead of being carried away. Use rigid setups, sharp tooling, low surface speeds, heavy positive feeds and high-volume flood coolant directed into the cutting zone, and never let the tool dwell. Fine chips and grinding dust are a fire hazard and are handled wet. Threads are rolled rather than cut wherever the section permits, both for fatigue life and because cutting titanium threads invites the same galling that affects them in service. Grade 23 machines essentially as Grade 5 does — the interstitial reduction slightly lowers strength and raises ductility, which makes chips marginally stringier but changes little else. Thermal conductivity is the same low 6.7 W/m·K, so surface speeds must stay low and coolant volume high.

Welding: weldability matches Grade 5 and is rated fair rather than good. The lower interstitial content does improve weld ductility somewhat. Welding requires full inert gas shielding of the weld, the heat-affected zone and the root — trailing shields and backing gas are standard practice. Weld colour is the first-pass check: bright silver is acceptable, straw and blue indicate increasing contamination, and grey or white powder means the weld must be cut out. Post-weld stress relief is normally required, and for fatigue-loaded joints mechanical fastening is preferable to welding.

Forming: somewhat more formable than Grade 5 thanks to the lower oxygen, but still an alpha-beta alloy and mostly formed hot, in the 870–955°C range. Thread rolling is preferred to cutting.

Heat Treatment: Grade 23 is heat treatable by solution treatment and ageing in the same way as Grade 5, in sections up to about 25 mm. Most fasteners and implant components are supplied annealed at the ASTM minimums, because the reason for choosing ELI material is toughness and ductility rather than peak strength. All heat treatment above roughly 500°C must be carried out in vacuum or inert gas, or the oxygen-enriched alpha case removed afterwards, because titanium absorbs oxygen, nitrogen and hydrogen rapidly at temperature and a contaminated surface layer is brittle.

The case for Grade 23 over Grade 5 is damage tolerance. Interstitial oxygen strengthens titanium but embrittles it, so capping oxygen at 0.13% and hydrogen at 0.0125% raises fracture toughness and ductility measurably — which matters in two situations. The first is fracture-critical structure: airframe parts and offshore tubulars where crack growth and residual strength, not yield, set the design. The second is surgical implants, where ASTM F136 specifically requires the ELI chemistry, and where the lower interstitial content also improves biocompatibility consistency.

The cost is strength: 828 MPa minimum tensile against Grade 5’s 895, and 759 MPa yield against 828. Where strength governs and toughness does not, Grade 5 remains the right specification and is cheaper.

Corrosion behaviour matches Grade 5 — excellent in marine and offshore environments and in oxidising acids, but less resistant than the CP grades in reducing media, so it is not a substitute for them on corrosion duty.

Titanium alloys divide into four classes, and the class tells you more than the grade number does. Alpha and near-alpha alloys are weldable and creep resistant and run hottest, but are not heat treatable to high strength. Alpha-beta alloys — of which Ti-6Al-4V is the archetype — are heat treatable, strong and the general structural choice. Near-beta and metastable beta alloys are deeply hardenable, can be cold formed in the solution-treated condition and then aged to very high strength, which makes them the natural choice for fasteners and springs. Commercially pure and lean corrosion grades trade all strength away for corrosion performance.

Three absolute exclusions apply to every titanium grade: it must not be used in dry chlorine, with which it reacts violently; not with red fuming nitric acid; and it is rapidly attacked by hydrofluoric acid at any concentration. Fine titanium swarf and grinding dust are a fire hazard and are handled wet.

Titanium galls, and for a threaded fastener this is the dominant practical issue. A titanium thread run against another titanium thread will cold-weld and seize, often badly enough that the fastener has to be cut off. Every titanium bolted joint needs one of three mitigations: an anti-seize compound or dry-film lubricant such as molybdenum disulphide; a plated or coated thread, commonly silver or solid-film lubricant; or a nut in a dissimilar material. Specify which at order stage.

Titanium is galvanically noble. It will not corrode itself, but a titanium fastener in an aluminium, carbon steel, zinc or magnesium assembly drives accelerated corrosion of the structure around it, and a bolted joint’s small-anode, large-cathode geometry is the worst case. Insulating washers and sleeves or a barrier coating should be specified in those assemblies.

Key Characteristics

  • Extra low interstitial Ti-6Al-4V — oxygen capped at 0.13%.
  • Improved ductility and fracture toughness over Grade 5.
  • The grade required by ASTM F136 for surgical implants.
  • Specified for fracture-critical airframe and offshore structure.
  • Heat treatable by solution treatment and ageing to 25 mm sections.

Typical Applications

  • Medical: surgical implant screws, plates and fixation hardware.
  • Aerospace: fracture-critical airframe fastener assemblies.
  • Offshore: tubular and riser components where toughness governs.
  • Cryogenic service requiring retained ductility.
  • Fatigue and damage-tolerance critical fixings.