Tools · Reactive Metals

Reactive Metal Inerting & Oxidation Threshold Calculator

Check whether your shielding actually protects titanium, tantalum, niobium, or nickel alloys. The calculator works out the cup's gas flow regime, the oxygen and moisture reaching the weld, how far behind the arc the metal stays hot enough to contaminate, and the weld color you should expect.

⚠ Disclaimer: Use at Your Own Risk This tool is provided "as is," for general engineering reference and educational purposes only, with no warranty of any kind. Gas properties and Reynolds numbers are standard calculations, but the air-entrainment, oxygen-pickup, and weld-color estimates come from a simplified semi-empirical model and are indicative only. Weld temperatures use an idealized moving heat source. Jeffrium and Jeffrey Sowards assume no liability for decisions, designs, procedures, or outcomes based on this tool's output. Confirm shielding with an oxygen analyzer and qualify welds by color inspection, hardness, and bend testing to your governing specification (e.g. AWS D17.1, AWS G2.4). Use of this tool is entirely at your own risk.

Environment

Still indoor air: about 0.05-0.1 m/s. A fan or open door: 0.5-2 m/s.

Shielding gas and torch

A #8 cup is 12.7 mm (1/2 in) ID; #12 is 19 mm. 1 CFH = 0.472 L/min.

Weld thermal conditions

Net heat input includes arc efficiency (e.g. GTAW: 0.65 × V × I / v). Need it? Use the heat input calculator.

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Reynolds number at the cup
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Gas exit velocity
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O₂ at the weld (est.)
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H₂O at the weld
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Temp. leaving gas cover
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Trailing shield needed
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Re < 2000: laminar, coherent gas column. Above 2300: turbulent, pulls in air.

Shielding visualizer

Side view. Gas lines turn wavy and orange as flow goes turbulent, and gray arrows show air being drawn in.

Surface color scale

Each color shows its temperature threshold (titanium-based, scaled per metal) and its O-equivalent ppm threshold. The highlighted one is the prediction.

Risk flags and fixes

    How it works

    How shielding fails on reactive metals

    Titanium, tantalum, and niobium soak up oxygen, nitrogen, and hydrogen whenever they're hot, and that pickup embrittles the weld long before it looks burnt. Protection fails in two ways: air gets into the gas shield, or hot metal leaves the shield too soon.

    The math

    Exit velocityv = Q / (πd²/4)
    ReynoldsRe = ρ·v·d / μ
    Draft ratioρairu² / (ρgasv²)
    PurgeC = Cs + (C0 − Cs)·e−ηQt/V
    Hot lengthR where T(R) = Tshield (Rosenthal)
    ρ, μgas density, viscosity (Ar-He by Wilke's rule)
    udraft plus travel speed
    η, Vpurge mixing efficiency, chamber volume

    Worked example

    GivenTi-6Al-4V, 3 mm, argon at 15 L/min through a #8 cup, 0.35 kJ/mm at 2.5 mm/s
    Gasv = 1.97 m/s, Re = 1870 (laminar)
    Hot lengthabove 425 °C for about 68 mm
    No trailerleaves the cup still molten: white, brittle
    Result≥ 62 mm trailing shield needed

    Doubling the flow to 30 L/min pushes Re to about 3700 and makes shielding worse, not better.

    More detail

    Assumptions used in this calculator
    • Shielding gas at 20 °C and 1 atm: ideal-gas density and Wilke-rule viscosity for Ar-He mixes. Flow is treated as incompressible (flagged above Mach 0.3).
    • Re uses the cup inner diameter and mean exit velocity (laminar < 2000, turbulent > 2300). A gas lens is modeled as a longer coherent column with less shear mixing; it does not change Re.
    • Air entrainment is a semi-empirical index (jet core length, turbulent shear, draft momentum ratio, helium buoyancy) calibrated to typical shop practice, not CFD or measurements. A flat (down-hand) position is assumed.
    • Oxygen-equivalent = O₂ + ½H₂O. Nitrogen pickup is covered implicitly through the air fraction.
    • Chambers are treated as well-mixed purges with a mixing efficiency (0.4 / 0.6 / 0.8) and a leak and outgassing floor set by chamber type.
    • Weld temperatures use Rosenthal moving point (thick plate) and line (thin plate) sources with constant properties and a surface heat loss set by fixturing (40 / 150 / 600 W/m²·K), evaluated on the weld centerline behind the arc.
    • Shielding is needed until the metal is below: Ti 425 °C, Ta 300 °C, Nb 250 °C, Inconel 625 500 °C. The trailing shield is assumed to deliver the same gas quality as the cup. Root-side back-purge is not modeled.
    • Color thresholds (temperature and ppm) are indicative titanium-based bands, scaled per metal. Acceptance is per your specification (e.g. AWS D17.1, AWS G2.4).
    Why more gas can make it worse

    A laminar gas column leaves the cup as a coherent slug that pushes air aside. Once the Reynolds number passes about 2300, the column's edge breaks into eddies that pull surrounding air inward, the same way a fast jet entrains its surroundings. A gas lens straightens the flow with fine screens, so the column stays coherent at higher flows and longer standoffs.

    Argon, helium, and buoyancy

    Helium has about one tenth the density of argon, so at the same flow its Reynolds number is roughly ten times lower and it never goes turbulent. But it is also far lighter than air: in a down-hand weld it floats away from the joint, and a draft pushes it aside much more easily. That's why helium-rich mixes need 2-3 times the argon flow. The tool weights this with a Richardson number (buoyancy against jet momentum).

    Weld color and what it means
    ColorTypical meaning for titanium
    Bright silverWell protected
    Light strawThin oxide; usually acceptable
    Dark straw / goldRemove and re-inspect per spec
    Blue / violetContaminated; reject on most specs
    GrayHeavily contaminated, embrittled
    White / flakyThick oxide and alpha case, brittle

    Color comes from an oxide film whose thickness rises with temperature and with oxygen in the gas. Acceptance limits vary: check AWS D17.1, AWS G2.4, or your customer specification. Bright color doesn't prove the absence of contamination, so hardness or bend tests are still used to qualify procedures.

    What the model leaves out

    The entrainment model is a semi-empirical index built from jet-mixing physics and calibrated to typical shop experience. It isn't a CFD solution. It ignores arc-driven plasma jets, joint geometry, torch angle, hose permeation, and leaks in fittings. Root-side (back-purge) protection is not modeled; reactive-metal welds need it as much as the face. For production, measure oxygen at the weld with an analyzer and confirm the result on test coupons.

    References
    • AWS G2.4/G2.4M, Guide for the Fusion Welding of Titanium and Titanium Alloys.
    • AWS D17.1/D17.1M, Specification for Fusion Welding for Aerospace Applications.
    • F.P. Ricou and D.B. Spalding, “Measurements of entrainment by axisymmetrical turbulent jets,” J. Fluid Mech. 11, 1961, 21–32.
    • C.R. Wilke, “A viscosity equation for gas mixtures,” J. Chem. Phys. 18, 1950, 517.
    • D. Rosenthal, “The theory of moving sources of heat,” Trans. ASME 68, 1946, 849–866.

    Discolored titanium welds or a chamber that won't purge down?

    Jeffrium designs custom trailing shields and gas-delivery systems, optimizes chamber purge and oxygen monitoring, and builds oxidation models around your parts and specifications, so reactive-metal welds come out bright and pass inspection the first time.

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