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Material Specification

Grade 19

Grade 19 Fasteners
Metastable Beta Alloy – Three ASTM Strength Levels to 1138 MPa

Titanium Grade 19 (Beta C) Fasteners

Buy Titanium Grade 19 (Beta C / Ti-3Al-8V-6Cr-4Mo-4Zr / UNS R58640 / ASTM B348 Grade 19) bolts, studs, springs and custom machined components from Exotic Alloy. Beta C is a metastable beta alloy carrying 7.5 to 8.5% vanadium, 5.5 to 6.5% chromium, 3.5 to 4.5% each of molybdenum and zirconium, and 3 to 4% aluminium. ASTM B348 recognises it at three distinct strength levels, from 793 MPa solution treated up to 1138 MPa fully aged.

Exotic Alloy manufactures Grade 19 components to ASTM B348 and ASTM B265 in metric M3–M36 and imperial #6–1½" sizes, with full EN 10204 3.1 material test certificates for oilfield and downhole hardware, springs, and high-strength fastener applications. Grade 20 is the same chemistry with a palladium addition for improved crevice resistance.

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Product Range

Grade 19 Fasteners Available

Grade 19 Hex Bolts
Grade 19
Hex Bolts
Grade 19 Heavy Hex Bolts
Grade 19
Heavy Hex Bolts
Grade 19 Stud Bolts
Grade 19
Stud Bolts
Grade 19 Threaded Rods
Grade 19
Threaded Rods
Grade 19 Anchor Bolts
Grade 19
Anchor Bolts
Grade 19 Hex Nuts
Grade 19
Hex Nuts
Grade 19 Washers
Grade 19
Washers
Grade 19 Cotter Pins
Grade 19
Cotter Pins
Grade 19 Springs
Grade 19
Springs
Grade 19 Circlips
Grade 19
Circlips
Grade 19 Coated Fasteners
Grade 19
Coated Fasteners
Grade 19 Custom Spacers
Grade 19
Custom Spacers
Technical Data

Grade 19 Specifications

Chemical Composition — Titanium Grade 19 (Beta C) (wt. %)
ElementTiVCrMoZrAlOFe
Min %Balance7.505.503.503.503.00––
Max %Balance8.506.504.504.504.000.120.30
Mechanical Properties — Titanium Grade 19 (Beta C)
ConditionUTS (MPa)YS 0.2% (MPa)Elongation (%)Hardness
ASTM B348 Grade 19E — Solution Treated≥ 793 (115 ksi)≥ 759 (110 ksi)≥ 15 in 4DRA ≥ 25%
ASTM B348 Grade 19F — Aged≥ 930 (135 ksi)897–1096 (130–159 ksi)≥ 10 in 4DRA ≥ 20%
ASTM B348 Grade 19G — Aged, High Strength≥ 1138 (165 ksi)1104–1276 (160–185 ksi)≥ 5 in 4DRA ≥ 20%
Alloy Class–––Metastable beta
Physical Properties
DensityApproximately 4.82 g/cm³
Modulus of ElasticityApproximately 86–103 GPa depending on condition
Melting RangeApproximately 1482–1593°C
Thermal ConductivityApproximately 7.6 W/m·K at 20°C
Maximum Service TemperatureApproximately 315°C
Alloy ClassMetastable beta — three ASTM strength levels
Equivalent Grades & Standards
UNSWerkstoff / DINASTM DesignationCommon Name
R58640 – ASTM B348 Grade 19 Beta C / Ti-38-6-44

Key Specifications: ASTM B348 (Bar & Billet) / ASTM B265 (Plate, Sheet & Strip) / ASTM B381 (Forgings). Note the three strength levels: B348 designates them 19E, 19F and 19G, and they are not interchangeable — the condition must be stated on the order. Grade 20 is the same chemistry with a 0.04 to 0.08% palladium addition for improved crevice corrosion resistance.

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. Machine in the solution-treated 19E condition where possible and finish after ageing. In the 19G condition at 1138 MPa and above the alloy is demanding and finish grinding may be preferable on critical diameters.

Welding: fusion welding of load-bearing joints is not recommended — the metastable beta structure and the carefully controlled ageing response do not survive a weld thermal cycle. 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. Mechanical fastening is the intended joining method.

Forming: in the solution-treated condition Beta C is soft and cold formable, which is the characteristic beta-alloy advantage — cold head, bend, coil or thread roll first, then age. Hot work in the 790–900°C range.

Heat Treatment: solution treat to retain metastable beta, form or machine, then age to precipitate alpha. The three ASTM conditions correspond to solution treated and two levels of ageing. Because the yield strength in the aged conditions is specified as a range rather than a minimum, over-ageing as well as under-ageing can put material out of specification. 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.

Beta C is one of the few titanium alloys with a genuine industrial following outside aerospace, because its combination of high strength, deep hardenability and cold formability in the solution-treated condition suits downhole and oilfield hardware — springs, hangers and high-strength fasteners — and titanium’s immunity to chloride stress corrosion cracking is valuable in sour service. The 6% chromium also gives it rather better corrosion performance than most alloyed titanium grades.

The three ASTM strength levels are the thing to get right on an order. 19E at 793 MPa is the solution-treated condition and is the one to buy if you intend to form or machine the part yourself; 19F and 19G are aged, and their yield strengths are specified as ranges, not minimums, so material can fail inspection for being too strong as well as too weak.

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

  • Three distinct ASTM B348 strength levels from 793 to 1138 MPa.
  • Cold formable in the solution-treated condition, then age hardened.
  • Deeply hardenable through thick sections.
  • 6% chromium gives better corrosion performance than most Ti alloys.
  • Established in oilfield and downhole hardware as well as aerospace.

Typical Applications

  • Oilfield and downhole: springs, hangers and high-strength fixings.
  • Aerospace: cold-formed and aged fastener assemblies.
  • Springs and spring-temper components.
  • Sour service hardware exploiting titanium’s SCC immunity.
  • High-strength bolting in small to medium diameters.