Specifications
Surface Treatments
Certifications
- ISO 9001 - 2015 Certified
- PED 2014/68/EC
- NACE MR0175/ISO 15156-2
- NORSOK M-650
- DFAR
- MERKBLATT AD 2000 W2/W7/W10
The Hiduron heat treatment cycle is a two-step solution anneal plus age. Step one solution-anneals at 850 to 900 deg C, holds for one hour to each 25 mm of section thickness, then water-quenches to freeze the gamma-prime formers (nickel and aluminium) in solid solution in the copper matrix. Step two ages at 450 to 500 deg C for 2 to 4 hours followed by air cool, which precipitates the gamma-prime Ni3Al strengthening phase and lifts the yield strength from the as-solutioned soft condition (around 200 MPa) to the specification level (480 MPa on Hiduron 130, 580 MPa on Hiduron 191). The age temperature is the controlling lever for the strength against ductility balance; ageing below 450 deg C under-develops the precipitate and the room-temperature yield falls below the floor, ageing above 500 deg C over-coarsens the precipitate and the strength drops on the other side of the peak.
Request a Quote on Solution-Annealed and Aged Hiduron Bolting
| Step | Temperature | Hold time | Cool | Purpose |
|---|---|---|---|---|
| 1. Solution anneal | 850 to 900 deg C | 1 h to each 25 mm of section | Water quench | Dissolve gamma-prime; freeze Ni and Al in solid solution |
| 2. Age (Hiduron 130) | 475 to 500 deg C | 2 to 4 h | Air cool | Precipitate gamma-prime Ni3Al; lift yield to >=480 MPa |
| 2. Age (Hiduron 191) | 450 to 480 deg C | 3 to 5 h | Air cool | Precipitate gamma-prime Ni3Al; lift yield to >=580 MPa |
| 3. Stress relief (post-machining, optional) | same as age | 1 to 2 h | Air cool | Relieve residual stress without disturbing the age |
In the as-rolled or as-forged condition the gamma-prime Ni3Al precipitate exists as coarse particles or stringers in the grain interior and along the grain boundaries. The solution-anneal at 850 to 900 deg C dissolves these particles back into the copper matrix and the water quench freezes the supersaturated solid solution at room temperature. The age at 450 to 500 deg C then re-precipitates the Ni3Al as fine, coherent particles distributed uniformly through the grains, which is the strengthening morphology. The fine coherent precipitate raises the yield by roughly 280 MPa on Hiduron 130 and roughly 380 MPa on Hiduron 191 against the as-solutioned condition. The age also restores ductility relative to the as-rolled or as-forged condition because the precipitation removes the residual hot-work stress.
| Age time at 475 deg C | Hiduron 130 Rp0.2 | Hiduron 130 Rm | Notes |
|---|---|---|---|
| 0 h (as solutioned) | ~200 MPa | ~480 MPa | Soft; below spec |
| 1 h | ~360 MPa | ~640 MPa | Under-aged; below spec |
| 2 h | ~470 MPa | ~735 MPa | At spec floor |
| 3 h | ~495 MPa | ~770 MPa | In spec band |
| 4 h | ~510 MPa | ~790 MPa | Peak strength; standard hold |
| 6 h | ~500 MPa | ~780 MPa | Plateau; no benefit to extend |
| 8 h | ~485 MPa | ~760 MPa | Over-aged drift begins |
Solution anneal is run in an air-circulating furnace with thermocouple control at the part centre and at a furnace reference location, with the higher of the two readings holding to the 850 to 900 deg C band. The water quench must drop the part to below 100 deg C inside 60 seconds for sections up to 50 mm; for thicker sections a forced-circulation quench tank with agitation maintains the cooling rate at the section centre. The age is run in a separate furnace at 450 to 500 deg C with tight thermocouple control because the strength response is steep against age temperature; a 25 deg C overshoot drops the peak yield by 40 to 60 MPa. Hardness traverse on the test piece confirms that the cycle achieved the intended precipitation; the certificate reports the cycle parameters alongside the hardness reading.
| Designation system | Hiduron 130 | Hiduron 191 |
|---|---|---|
| UNS (Unified Numbering System) | C72400 | C72420 |
| Werkstoff (German register) | 2.1504 | not formally assigned |
| Chemical-symbol designation | CuNi14Al3Fe1 | CuNi14Mn4AlFe |
| UK Air Ministry | DTD 900/4805 | not applicable |
| UK Naval Engineering Standard | not applicable | NES 835 |
| UK Ministry of Defence | not applicable | DEF STAN 02-835 |
| US Department of Defense | not applicable | DOD-C-24676 |
| Originator and brand | Langley Alloys (UK) | Langley Alloys (UK) |
| Form factor | Standard sizes | Page |
|---|---|---|
| Round bar (raw stock) | OD 16 to 250 mm | Round Bar |
| Stud bolts | M12 to M100, 50 to 600 mm | Stud Bolts |
| Hex bolts (DIN 931 / ISO 4014) | M12 to M64 | Hex Bolts |
| Heavy hex bolts (ASME B18.2.1) | 1/2 to 3 inch | Heavy Hex Bolts |
| Nuts and heavy hex nuts | M12 to M100 | Nuts |
| Washers (flat, spring, locking) | M12 to M48 | Washers |
| Forgings (subsea connector blank) | up to 600 kg piece | Forgings |
| Machined components (custom) | to project drawing | Machined Components |
| Standard | Scope | Relevance |
|---|---|---|
| NES 835 | UK Naval Engineering Standard for Cu-Ni-Al bolting | Hiduron 191 controlling spec |
| DEF STAN 02-835 | UK Ministry of Defence adoption of NES 835 | Hiduron 191 MoD procurement |
| DOD-C-24676 | US Department of Defense Cu-Ni-Al spec | Hiduron 191 US Navy procurement |
| DTD 900/4805 | UK Air Ministry specification | Hiduron 130 original spec |
| NACE MR0175 | Sour service materials qualification | Hiduron 191 qualified to 286 HBW limit |
Every Hiduron 130 and Hiduron 191 stock and finished fastener ships with EN 10204 type 3.1 mill test certificate as standard. Type 3.2 third-party witness by Lloyd's Register, DNV, BV, SGS or TUV is supplied on call-out and is standard practice on naval and subsea procurement orders. The certificate carries the melt heat number, full chemical analysis to the controlling specification, solution-anneal plus age cycle parameters, tensile and yield results, hardness, Charpy V impact result where called out, and the dimensional report. For Hiduron 191 sour-service orders, an additional NACE MR0175 hardness certificate confirms that every test piece reads below the 286 HBW (28 HRC) limit.
TorqBolt supplies Hiduron 130 (UNS C72400, DTD 900/4805) and Hiduron 191 (UNS C72420, NES 835, DEF STAN 02-835, DOD-C-24676) in round bar, stud bolts, hex bolts, heavy hex bolts, nuts, washers, forgings and machined components. Standard fastener lead time is 4 to 8 weeks from order, subsea machined components quote project-specific lead time. Send an enquiry through TorqBolt Contact with the controlling specification, the form factor, the size envelope and the certification level (3.1 default, 3.2 on call-out, NACE on call-out).
Request a Quote on Hiduron 130 and Hiduron 191 Bolting Stock and Fasteners
Q. What is the Hiduron solution-anneal temperature?
The standard band is 850 to 900 deg C, hold one hour to each 25 mm of section thickness, then water quench. The quench must drop the part to below 100 deg C inside 60 seconds for sections up to 50 mm to freeze the gamma-prime formers in solid solution.
Q. What is the Hiduron age temperature?
The age is 450 to 500 deg C for 2 to 4 hours followed by air cool. Hiduron 130 typically ages at the upper end (475 to 500 deg C) and Hiduron 191 at the lower end (450 to 480 deg C) to land inside the strength specification band.
Q. Can Hiduron be re-solutioned and re-aged if the first cycle is off-spec?
Yes. The cycle is fully reversible. A re-solutioned and re-aged Hiduron part returns to the standard property envelope with no loss of toughness or fatigue endurance. This is one of the supply-chain advantages of the gamma-prime mechanism.
Q. Should fasteners be aged before or after machining?
For finished bolting, the bar is solution-annealed before machining (soft and machinable condition) and aged after machining to the finished dimension. This sequence avoids the dimensional change associated with the strengthening cycle and lets the age also serve as a stress-relief on the machined surface.