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Material Specification

Alloy 36

Alloy 36 Fasteners
Fe-36Ni Controlled Expansion Alloy – Cryogenic to 260°C Dimensional Stability

I Alloy 36 (Invar 36) Fasteners

Buy I Alloy 36 (Invar 36 / Nilo 36 / UNS K93600 and K93603 / Werkstoff 1.3912 / ASTM F1684) bolts, stud bolts, nuts, precision fasteners and custom machined components from Exotic Alloy. Alloy 36 is the original low-expansion alloy — a nickel-iron alloy containing 35–37% nickel that maintains nearly constant dimensions across the range of normal atmospheric temperatures and holds a low coefficient of expansion from cryogenic temperatures up to about 260°C.

Exotic Alloy manufactures Alloy 36 fasteners to ASTM F1684 and AFNOR NF A54-301 in metric M3–M48 and imperial #4–2" sizes, machined and threaded before the final stabilising treatment, with full EN 10204 3.1 material test certificates for composite forming tooling, cryogenic and LNG hardware, laser and optical components and precision instruments.

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Product Range

Alloy 36 Fasteners Available

Alloy 36 Hex Bolts
Alloy 36
Hex Bolts
Alloy 36 Heavy Hex Bolts
Alloy 36
Heavy Hex Bolts
Alloy 36 Stud Bolts
Alloy 36
Stud Bolts
Alloy 36 Threaded Rods
Alloy 36
Threaded Rods
Alloy 36 Anchor Bolts
Alloy 36
Anchor Bolts
Alloy 36 Hex Nuts
Alloy 36
Hex Nuts
Alloy 36 Washers
Alloy 36
Washers
Alloy 36 Cotter Pins
Alloy 36
Cotter Pins
Alloy 36 Springs
Alloy 36
Springs
Alloy 36 Circlips
Alloy 36
Circlips
Alloy 36 Coated Fasteners
Alloy 36
Coated Fasteners
Alloy 36 Custom Spacers
Alloy 36
Custom Spacers
Technical Data

Alloy 36 Specifications

Chemical Composition — I Alloy 36 (Invar 36) (wt. %)
ElementFeNiMoCuCrMnSiC
Min %Balance35.0––––––
Max %Balance37.00.50.50.50.60.350.1
Mechanical Properties — I Alloy 36 (Invar 36)
ConditionUTS (MPa)YS 0.2% (MPa)Elongation (%)Hardness
Annealed at 20°C (Typical)49024142–
Annealed at 200°C (Typical)42711045–
Annealed at 300°C (Typical)4079048–
Annealed at 500°C (Typical)2909059–
Physical Properties
Density8.11 g/cm³ (0.293 lb/in³)
Melting Point1429°C (2605°F)
Thermal Expansion1.4 µm/m·°C (20–100°C)
Thermal Expansion2.5 µm/m·°C (20–200°C)
Thermal ConductivityApproximately 10 W/m·K at 20°C
Useful Low-Expansion RangeCryogenic to approximately 260°C (500°F)
Equivalent Grades & Standards
UNSWerkstoff / DINASTM SpecificationCommon Name
K93600 / K93603 1.3912 ASTM F1684 Invar 36 / Nilo 36

Key Specifications: ASTM F1684 (Iron-Nickel and Iron-Nickel-Cobalt Alloys for Low Thermal Expansion Applications) / AFNOR NF A54-301 (chemistry only) / Werkstoff 1.3912. A free-machining variant carrying a small selenium addition is designated UNS K93050 under the same ASTM specification. Composition is held to tight tolerances under F1684 because the low-expansion behaviour is highly sensitive to nickel content.

Machinability: Alloy 36 can be hot and cold formed and machined using processes similar to those used for austenitic stainless steels. It work-hardens and produces stringy chips, so use sharp tooling, rigid setups, positive feeds and generous coolant. Where machinability is the governing constraint, the free-machining selenium-bearing variant UNS K93050 is available under the same specification and cuts considerably more freely at the cost of a small penalty in cleanliness.

Welding: Alloy 36 is readily weldable using Filler Metal CF36, available as bare wire for both GTAW and GMAW. This is a genuine advantage over most controlled-expansion alloys. Note that welding introduces localised stress that disturbs the expansion coefficient, so a stabilising treatment after welding is recommended wherever dimensional precision is the reason for the material choice.

Forging & Forming: hot work in the 1150–870°C range and cold form freely; the alloy behaves much like an austenitic stainless steel and takes heavy cold reduction without intermediate annealing.

Heat Treatment: for maximum dimensional stability the normal sequence is to anneal at approximately 830°C, then stress relieve and age at low temperature on the finished part. As with all alloys in this family the final stabilising treatment should be carried out at or as close to finish size as possible, because machining stresses alter the expansion coefficient. The alloy also retains good strength and toughness at cryogenic temperatures, so no low-temperature embrittlement allowance is needed.

Alloy 36 holds a coefficient of expansion around 1.4 µm/m·°C between 20 and 100°C — roughly a tenth that of carbon steel — and keeps that behaviour from cryogenic temperatures upward. The low expansion is a magnetic effect and it disappears as the alloy passes its magnetic transition. Published data shows the mean coefficient climbing from 1.4 µm/m·°C at 100°C to about 2.5 at 200°C, 5.6 at 300°C and 8.5 at 400°C, by which point there is no low-expansion advantage left at all. Approximately 260°C (500°F) is the practical ceiling; above it, specify Alloy 42 if a moderately low and more nearly constant coefficient is wanted to 300°C, or accept a conventional alloy.

Unlike Alloy 32-5, Alloy 36 remains stable and tough at cryogenic temperatures, which makes it the correct choice of the two for LNG, liquid-gas and deep-cryogenic hardware. It is also widely used for composite forming tooling because its expansion is close to that of carbon fibre laminates, so a tool and the part cured on it move together.

Machining and forming stresses change the expansion coefficient. This is the single most important processing fact about this family, and Carpenter states it explicitly for Super Invar: machining, forming and deep drawing introduce stresses that promote variation in thermal expansion behaviour, so parts should be heat treated at or as close to finish size as possible. For a threaded fastener that matters a great deal, because thread rolling is heavy local cold work. Exotic Alloy therefore machines and threads first and performs the stabilising heat treatment on the finished part — if a component is machined after its final stabilising treatment, the expansion coefficient it was bought for is no longer guaranteed.

These alloys are not corrosion resistant. Chromium is an incidental residual rather than an alloying addition — 0.5% maximum in Invar 36, 0.25% maximum in Alloy 42, and not specified at all in Super Invar — so there is no passive film and these materials rust in damp air much like plain carbon steel. Nickel, cadmium, tin or dry-film coating is required for any exposed or humid service, and components are commonly supplied plated. Passivation is not an option because there is nothing to passivate.

These are property alloys, not strength alloys. All three grades are soft iron-nickel austenites with room-temperature tensile strengths around 480–490 MPa and yield strengths of 240–280 MPa — roughly comparable to annealed 304 stainless and well below any structural bolting material. Nobody specifies Invar for load. They are specified because they barely move when the temperature changes, and a fastener in one of these alloys is there to hold a dimensionally stable assembly together without introducing thermal mismatch of its own.

Invar is a registered trademark originating with Imphy Alloys, and Nilo is a trademark of the Special Metals Corporation group. Exotic Alloy is an independent manufacturer and is not affiliated with or endorsed by either; the designations are used here solely to identify the alloy chemistry, which is defined by the UNS number and ASTM specification given above.

Key Characteristics

  • Coefficient of expansion around 1.4 µm/m·°C from 20 to 100°C.
  • Low expansion retained from cryogenic temperatures to approximately 260°C.
  • Retains good strength and toughness at cryogenic temperatures.
  • Readily weldable with Filler Metal CF36 by GTAW and GMAW.
  • Expansion closely matched to carbon fibre laminates for composite tooling.

Typical Applications

  • Composite forming: tooling and die fastener assemblies.
  • Cryogenic and LNG plant: tank, pipework and membrane fixings.
  • Laser and optical systems: mount and bench hardware.
  • Precision instruments, metrology frames and length standards.
  • Aerospace structures requiring matched thermal movement.