Hiduron Heat Treatment

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

Standard Solution-Anneal and Age Cycle

StepTemperatureHold timeCoolPurpose
1. Solution anneal850 to 900 deg C1 h to each 25 mm of sectionWater quenchDissolve gamma-prime; freeze Ni and Al in solid solution
2. Age (Hiduron 130)475 to 500 deg C2 to 4 hAir coolPrecipitate gamma-prime Ni3Al; lift yield to >=480 MPa
2. Age (Hiduron 191)450 to 480 deg C3 to 5 hAir coolPrecipitate gamma-prime Ni3Al; lift yield to >=580 MPa
3. Stress relief (post-machining, optional)same as age1 to 2 hAir coolRelieve residual stress without disturbing the age

Why the Two-Step Cycle Is Needed

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 Response and Time at Temperature

Age time at 475 deg CHiduron 130 Rp0.2Hiduron 130 RmNotes
0 h (as solutioned)~200 MPa~480 MPaSoft; below spec
1 h~360 MPa~640 MPaUnder-aged; below spec
2 h~470 MPa~735 MPaAt spec floor
3 h~495 MPa~770 MPaIn spec band
4 h~510 MPa~790 MPaPeak strength; standard hold
6 h~500 MPa~780 MPaPlateau; no benefit to extend
8 h~485 MPa~760 MPaOver-aged drift begins

Furnace and Quench Notes for Production Heat Treatment

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.

Hiduron 130 + 191 Designation Chain

Designation systemHiduron 130Hiduron 191
UNS (Unified Numbering System)C72400C72420
Werkstoff (German register)2.1504not formally assigned
Chemical-symbol designationCuNi14Al3Fe1CuNi14Mn4AlFe
UK Air MinistryDTD 900/4805not applicable
UK Naval Engineering Standardnot applicableNES 835
UK Ministry of Defencenot applicableDEF STAN 02-835
US Department of Defensenot applicableDOD-C-24676
Originator and brandLangley Alloys (UK)Langley Alloys (UK)

Hiduron Forms TorqBolt Supplies

Form factorStandard sizesPage
Round bar (raw stock)OD 16 to 250 mmRound Bar
Stud boltsM12 to M100, 50 to 600 mmStud Bolts
Hex bolts (DIN 931 / ISO 4014)M12 to M64Hex Bolts
Heavy hex bolts (ASME B18.2.1)1/2 to 3 inchHeavy Hex Bolts
Nuts and heavy hex nutsM12 to M100Nuts
Washers (flat, spring, locking)M12 to M48Washers
Forgings (subsea connector blank)up to 600 kg pieceForgings
Machined components (custom)to project drawingMachined Components

Where Hiduron Is Specified

Hiduron Controlling Standards

StandardScopeRelevance
NES 835UK Naval Engineering Standard for Cu-Ni-Al boltingHiduron 191 controlling spec
DEF STAN 02-835UK Ministry of Defence adoption of NES 835Hiduron 191 MoD procurement
DOD-C-24676US Department of Defense Cu-Ni-Al specHiduron 191 US Navy procurement
DTD 900/4805UK Air Ministry specificationHiduron 130 original spec
NACE MR0175Sour service materials qualificationHiduron 191 qualified to 286 HBW limit

EN 10204 Certification and Inspection

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.

Request a Quote on Hiduron Bolting

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

  • Hiduron 130 Datasheet: Consolidated chemistry, mechanicals and heat treatment.
  • Hiduron 191 Datasheet: NACE-qualified naval and subsea grade datasheet.
  • Bolt Dimensions: Imperial and metric thread, head and stress-area tables.
  • Torque Chart: Cu-Ni-Al fastener torque values, dry and lubricated.
  • FAQ: Consolidated questions on Hiduron specification, certification and supply.

Hiduron Heat Treatment FAQ

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.