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Material Specification

Alloy 191 (C19100)

Alloy 191 (C19100) Fasteners
Cu-Ni-P-Te — Free-Machining, Precipitation Hardenable

Alloy 191 — Copper C19100 Fasteners

Alloy 191 is UNS C19100, a copper-nickel-phosphorus-tellurium alloy. It does contain nickel — 0.9–1.3% — but the Copper Development Association classifies it under Wrought High Copper Alloys, not among the Wrought Copper Nickels, and at around 1% nickel it is a very different material from the 90/10 and 70/30 marine grades. The other deliberate additions are 0.15–0.35% phosphorus and 0.35–0.6% tellurium.

Those three additions each do a distinct job, and together they make C19100 unusual. The nickel and phosphorus form nickel phosphide, which makes the alloy precipitation hardenable — rare among coppers, and it reaches 717 MPa in hard, stress-relieved rod. The tellurium makes it free machining, with a CDA machinability rating of 75 against 20 for plain copper. And the alloy still holds 55% IACS conductivity in the precipitation heat treated condition. The result is a copper that can be turned at speed, heat treated to real strength and still conduct — which is why it is used for screw-machined electrical hardware, connector pins and relay parts. Exotic Alloy supplies C19100 for machined components.

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Product Range

Alloy 191 (C19100) Fasteners Available

Alloy 191 (C19100) Hex Bolts
Alloy 191 (C19100)
Hex Bolts
Alloy 191 (C19100) Heavy Hex Bolts
Alloy 191 (C19100)
Heavy Hex Bolts
Alloy 191 (C19100) Stud Bolts
Alloy 191 (C19100)
Stud Bolts
Alloy 191 (C19100) Threaded Rods
Alloy 191 (C19100)
Threaded Rods
Alloy 191 (C19100) Anchor Bolts
Alloy 191 (C19100)
Anchor Bolts
Alloy 191 (C19100) Hex Nuts
Alloy 191 (C19100)
Hex Nuts
Alloy 191 (C19100) Washers
Alloy 191 (C19100)
Washers
Alloy 191 (C19100) Cotter Pins
Alloy 191 (C19100)
Cotter Pins
Alloy 191 (C19100) Springs
Alloy 191 (C19100)
Springs
Alloy 191 (C19100) Circlips
Alloy 191 (C19100)
Circlips
Alloy 191 (C19100) Coated Fasteners
Alloy 191 (C19100)
Coated Fasteners
Alloy 191 (C19100) Custom Spacers
Alloy 191 (C19100)
Custom Spacers
Technical Data

Alloy 191 (C19100) Specifications

Chemical Composition — Alloy 191 — Copper C19100 (wt. %)
ElementMinimum %Maximum %
Copper (Cu), including silverRemainder—
Nickel (Ni)0.91.3
Tellurium (Te)0.350.6
Phosphorus (P)0.150.35
Zinc (Zn)—0.50
Iron (Fe)—0.20
Lead (Pb)—0.10
Copper + sum of named elements99.5—
Mechanical Properties — Alloy 191 — Copper C19100
ConditionUTS (MPa)YS 0.5% EUL (MPa)Elongation (%)Hardness
Forgings, as forged and quenched M11248—35—
Forgings, as hot forged air cooled M10310—50—
Forgings, precipitation hardened TF00400262—70 HRB
Rod 25 mm, 1/4 hard and stress relieved HR015384692784 HRB
Rod 13 mm, 1/4 hard and stress relieved HR015524831585 HRB
Rod 9.5 mm, 1/4 hard and stress relieved HR016485171090 HRB
Rod 6 mm, 1/4 hard and stress relieved HR015795031085 HRB
Rod 3 mm, 1/4 hard and stress relieved HR01717531695 HRB
Physical Properties
Density8.94 g/cm³ (0.323 lb/in³)
Melting Point — Liquidus1082 °C (1980 °F)
Melting Point — Solidus1038 °C (1900 °F)
Electrical Conductivity55% IACS at 20 °C, precipitation heat treated
Thermal Conductivity251 W/m·K at 20 °C
Coefficient of Thermal Expansion17.6 × 10⁻⁶ /°C (20–300 °C)
Specific Heat Capacity385 J/kg·K at 20 °C
Modulus of Elasticity110 GPa
Modulus of Rigidity41 GPa
Machinability Rating75 (C36000 = 100) — free machining
Forgeability Rating65
Solution Treatment704–788 °C (1300–1450 °F)
Precipitation Treatment454 °C (850 °F)
CDA ClassificationWrought High Copper Alloys — not Copper Nickels
Magnetic ResponseNon-magnetic
Equivalent Grades & Standards
UNSEN / CEN DesignationNominal CompositionCommon Name
C19100 — Cu-1Ni-0.25P-0.5Te Alloy 191, Nickel-Tellurium Copper

Key Specifications: CDA list no applicable product specifications for C19100. Material is supplied to the composition limits above with mechanical requirements, product form, temper and acceptance criteria agreed on the order.

A note on where this grade sits. The Copper Development Association does not classify this alloy among the Wrought Copper Nickels (the C7xxxx family). We have built it here because it appears on this category list, but the classification is worth knowing when you specify, and the detail is set out below. C19100 is nickel-bearing at 0.9–1.3%, but CDA place it among the Wrought High Copper Alloys. It has none of the iron addition or seawater film behaviour of the C7xxxx marine grades and should not be substituted for them. If you need a copper-nickel for marine duty, see C70600 or C71500.

Note on fastener standards: Of the alloys on this hub, only C71500 is covered by the ASTM nonferrous fastener standards. ASTM F468 and F467 list C71500 (as Cu 715) along with C71000 and a range of brasses and bronzes — but C70600 is not among them, and neither are the other grades here. That is a genuinely useful distinction: where a certified copper-nickel bolt, hex cap screw, stud or nut is required, C71500 (70/30) is the grade that has a standard behind it, and specifying 90/10 instead means the fastener is supplied to the mill product requirements with acceptance criteria agreed on the order rather than to a fastener specification.

On strength, annealed 70/30 is specified at 345 MPa minimum and hard-drawn at 485 MPa, against 830 MPa for an ordinary ASTM A325 structural steel bolt. Copper-nickel fasteners are chosen for seawater corrosion resistance, biofouling resistance, freedom from chloride stress-corrosion cracking and compatibility with copper-nickel pipework — not for load. The one exception on this hub is C72900, the spinodal Cu-15Ni-8Sn alloy, which reaches 1138 MPa and is a genuine high-strength material.

Every copper-nickel order ships with EN 10204 3.1 certification giving the heat analysis, the temper, and the mechanical test results for the product form and section supplied. Iron and manganese are reported explicitly on the 90/10 and 70/30 grades, because iron within the specified range is what makes the protective seawater film work and material at the bottom of the range performs measurably worse. Carbon, phosphorus and sulfur are reported on the welding grades C70620 and C71520, where they are the whole reason for the grade. Positive material identification, hardness testing and additional NDT can be added at order stage.

Machining is the headline property. C19100 carries a CDA machinability rating of 75 against 20 for the plain coppers, where free-cutting brass C36000 is 100. The 0.35–0.6% tellurium is nearly insoluble in copper and sits as a finely dispersed second phase that breaks the chip mechanically and lubricates the cutting edge — the same mechanism as in C14500, but here combined with a precipitation-hardening response that C14500 does not have. Expect short broken chips, clean threads and good hole quality at screw-machine rates.

Forming: cold working and hot forming are both rated Good, with a forgeability rating of 65. The alloy heads, upsets, roll-threads, swages and hot forges satisfactorily, though the tellurium limits severe drawing and spinning.

Joining: the tellurium that makes the alloy machine well makes it poor to weld. CDA rate C19100 Excellent for soldering but only Good for brazing and Fair for oxyacetylene, gas-shielded arc and coated metal arc welding, with spot, seam and butt welding all rated Poor. Tellurium promotes hot cracking in the weld metal. Design for soldered, brazed or mechanically fastened joints.

Heat treatment: C19100 is one of the few precipitation-hardenable coppers, and the mechanism is nickel phosphide precipitation — the nickel and phosphorus additions working together. The cycle is solution treatment at 704–788 °C (1300–1450 °F), quench, optional cold work, then precipitation treatment at 454 °C (850 °F). Annealing is carried out at 482–704 °C and hot working at 760–871 °C.

As with any precipitation-hardening copper, holding the alloy above the ageing temperature over-ages the structure and softens it permanently; only a full re-solution-treat and re-age will restore it. Note that the common commercial condition is HR01 — quarter hard and stress relieved — which combines cold work with a stress-relief that also develops some precipitation response, and which is where the 538–717 MPa rod figures come from.

Classification first: C19100 is nickel-bearing but it is not a marine copper-nickel. CDA place it among the Wrought High Copper Alloys. At 0.9–1.3% nickel with no deliberate iron addition, it has none of the protective seawater film behaviour that makes C70600 and C71500 the marine standards, and it should not be substituted for them in seawater service.

Corrosion behaviour is broadly that of copper. Good resistance to fresh water, atmospheric exposure, non-oxidising acids free of oxygen, and neutral and alkaline salts; attacked by oxidising acids, oxidising salts and sulfides. CDA publish no corrosion rate data for this alloy. One caution specific to the chemistry: the tellurium-rich second phase is slightly less noble than the copper matrix, so very fine selective attack at those particles is possible in an aggressive electrolyte — not a practical concern in the electrical and screw-machine duties the grade is normally used for.

Copper-nickels are markedly more resistant to stress-corrosion cracking than the brasses, which is one of their quiet advantages. Dezincification does not apply — there is no zinc to lose — and the ammonia stress-corrosion cracking that destroys brass fittings is far less of a threat here. They are also resistant to the chloride SCC that limits austenitic stainless steel in warm seawater, which is the reason copper-nickel rather than 316 is specified for many seawater services. That said, the alloys are not immune: concentrated ammonia and amine environments should still be treated with caution for stressed components such as tightened fasteners, and stress relief after heavy cold work remains sensible practice for parts going into borderline service.

Galvanically the copper-nickels sit usefully in the middle of the seawater series. They are more noble than carbon steel, cast iron, aluminium and zinc, so a copper-nickel fastener will drive corrosion of those materials and needs isolation from them — the classic problem being copper-nickel pipework bolted into a steel structure. They are less noble than the passive stainless steels, titanium and the high-molybdenum nickel alloys, so in a mixed seawater system with those materials the copper-nickel is the part that suffers, and the area ratio matters: a small copper-nickel component among large titanium surfaces is the bad case. They are compatible with the other coppers and bronzes and with Monel. Copper-nickel is also commonly used as the sacrificial partner in controlled fashion — coupling to a small area of steel is sometimes deliberate.

How these grades divide. The two that matter for most marine work are C70600 (90/10) and C71500 (70/30). The 70/30 is stronger — 345 MPa against 262 MPa annealed — tolerates a higher flow velocity, performs better hot, and is the one carried by ASTM F468 for fasteners; the 90/10 is cheaper, conducts heat better at 45 against 29 W/m·K, and is adequate for the majority of seawater service. C70620 and C71520 are the same two compositions with carbon, phosphorus and sulfur tightened for welded fabrication. C71580 is a 70/30 variant with iron and manganese cut right back. Beyond those, the family diverges sharply: C72150 at 43–46% nickel is a Constantan-type electrical resistance alloy, not a marine material; C72420 adds aluminium and manganese for higher strength; and C72900 is a spinodally hardened Cu-15Ni-8Sn alloy reaching 1138 MPa, a different material in everything but name. Alloy 130 and Alloy 191 sit outside the copper-nickel class altogether — see the notes on those pages.

Key Characteristics

  • Nickel-bearing at 0.9–1.3% — but a high copper alloy, not a marine copper-nickel.
  • CDA classify it under Wrought High Copper Alloys.
  • Free machining — machinability rating 75 against 20 for plain copper.
  • Precipitation hardenable via nickel phosphide — rare among coppers.
  • Reaches 717 MPa in hard, stress-relieved small-section rod.
  • Retains 55% IACS conductivity precipitation heat treated.
  • Tellurium 0.35–0.6% breaks the chip; phosphorus 0.15–0.35%.
  • Poor for spot, seam and butt welding — tellurium promotes hot cracking.

Typical Applications

  • Screw-machined electrical hardware and terminals.
  • Connector pins, contacts and relay components.
  • Machined fasteners requiring conductivity and strength.
  • Switchgear and circuit breaker machined parts.
  • Welding torch and resistance welding machined components.
  • Cross-drilled, slotted and threaded conductive parts.
  • Forged electrical fittings and lugs.
  • High-volume turned parts requiring heat-treatable strength.