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DSM Somos ProtoCast™ AF 19122 Antimony-free Liquid Photopolymer

    • Название продукта: DSM Somos ProtoCast™ AF 19122 Antimony-free Liquid Photopolymer
    • Сайт Factroy: Округ Юду, Ганьчжоу, Цзянси, Китай
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    • Производитель: Ascent Petrochem Holdings Co., Limited
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    Код ТН ВЭД 468149

    Как аккредитованный завод DSM Somos ProtoCast™ AF 19122 для жидких фотополимеров без антимона, мы соблюдаем строгие протоколы качества - каждая партия подвергается строгим испытаниям для обеспечения последовательных стандартов эффективности и безопасности.

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    Применение DSM Somos ProtoCast™ AF 19122 Жидкий фотополимер без антимона

    Foundries producing nickel-base superalloy turbine airfoils for gas turbine engines use DSM Somos ProtoCast™ AF 19122 as a sacrificial stereolithography pattern material where internal cooling passages and near-net wall sections exceed the practical limits of machined wax injection tooling. The liquid photopolymer is charged to the stereolithography vat at a 100:0 resin-to-diluent ratio by mass; no reactive diluent, photoinhibitor, or solvent is added to the formulation, because viscosity reduction with non-reactive solvents depresses gel fraction at the layer interface and creates localized undercure in side walls thinner than 1.5 mm. Commercial stereolithography platforms operating at 355 nm are used with layer thicknesses from 0.050 mm to 0.100 mm. For airfoil patterns shelled to 1.5–2.0 mm wall thickness with internal drainage channels, vat management is limited to replenishing the same undiluted resin rather than solvent adjustment. Compliance demonstration for foundry qualification commonly includes batch ash-content analysis under ASTM D5630 and thermogravimetric analysis under ISO 11358-1:2022, with ash determination after pyrolysis at 850°C in air. Because the formulation is antimony-free, the failure pathway associated with antimony transfer into nickel-base remelt stock is eliminated; Sb is otherwise treated as a tramp element in aerospace superalloy melt practice.

    The dominant processing risk in this application is thermal expansion mismatch between cured photopolymer and the fused-silica shell. Burnout from ambient to 180°C is held at 1–2°C/min so the pattern softens and drains before decomposition, then held at 180°C for 60–120 min. From 180°C to 600°C, the ramp is restricted to 2–3°C/min because decomposition gas pressure can cause longitudinal shell cracks along the airfoil pressure side if venting is insufficient. Final burnout at 850–950°C for 1–2 h removes carbonaceous residue before preheat and pouring. Terminal products are single-crystal or directionally solidified turbine blades and nozzle guide vanes with serpentine cooling passages.

    What Limits Burnout Ramp Rates for Automotive Turbocharger Wheel Patterns?

    Automotive turbocharger wheel patterns built from DSM Somos ProtoCast™ AF 19122 carry a geometry-driven thermal mass conflict: blade trailing edges may be as thin as 0.4 mm while the hub section reaches 6–8 mm in maximum cross-section. The resin is processed at a 100:0 resin-to-diluent ratio by mass, with no solvent cut, and the build layer thickness is typically restricted to 0.050 mm for trailing-edge definition. Process control documentation under IATF 16949:2016 and ISO 9001:2015 clause 8.5.6 treats burnout cycle changes as a production-change item requiring revalidation when pattern wall thickness, infill, or furnace loading is modified. The downstream process consists of stereolithography pattern generation, support removal, solvent-assisted surface finishing, assembly onto a vented runner, ceramic shelling with colloidal silica slurry, and burnout in a forced-air gas-fired furnace. Patterns are oriented with the wheel axis between 30° and 45° to the build plane to reduce stair-step surface defects on the blade suction side. The burnout ramp from 180°C to 600°C is the critical segment: thin trailing-edge sections decompose and vent before thick hub sections have fully softened, so ramp rates above 2–3°C/min can produce internal pressure spikes and shell cracking at the hub-to-blade transition. Final burnout at 850°C is held until no visible carbon remains on the shell interior. Terminal products are TiAl or Inconel 713C turbocharger turbine wheels for passenger and heavy-duty vehicle applications.

    Gypsum-bonded vacuum casting of precious metal ornaments and high-surface-detail jewelry is a process in which DSM Somos ProtoCast™ AF 19122 functions as a positive burn-out pattern for filigree, micro-pavé, and hollow-form designs. The resin is used 100% undiluted with a layer thickness of 0.025 mm, allowing feature resolution down to 0.3 mm for retention of fine engraving and stone-setting geometry. Final article compliance for nickel release is tested according to EN 1811:2011+A1:2015, with release not exceeding 0.5 µg/cm²/week for post assemblies under EU REACH Annex XVII entry 27; the antimony-free photopolymer formulation does not introduce a further metallic contaminant pathway into recycled gold or silver melts. Downstream processing includes high-resolution stereolithography pattern production, assembly onto a wax tree, vacuum investment with gypsum-bonded powder, and programmed flask burnout with holds near 150°C, 350°C, and 750°C. Terminal products are rings, pendants, earring components, and decorative micro-castings for jewelry and accessories.

    ApplicationCritical section thicknessBurnout ramp constraintReference method
    Aerospace turbine airfoil1.5–2.0 mm shell20–180°C at 1–2°C/minASTM D5630
    Automotive turbocharger wheel0.4–8.0 mm variable section180–600°C at 2–3°C/minISO 11358-1:2022
    Jewelry gypsum flask pattern0.3 mm minimum feature20–150°C at 2°C/minEN 1811:2011+A1:2015
    Energy hot-section vane5–10 vol% lattice infill850–950°C final holdASTM E192

    When Thin-Walled Pump Impeller Patterns Are Substituted for Machined Wax Assemblies

    The substitution of stereolithography photopolymer patterns for machined wax assemblies in pump impeller production changes shelling requirements because the photopolymer has lower ductility than wax and cannot be reclaimed by melting. The resin is charged at a 100:0 resin-to-diluent ratio by mass; thin-walled impeller vanes are shelled to 2.5 mm with an internal honeycomb fill of 15–20 vol% to reduce resin mass without sacrificing pattern rigidity. Published data for this specific configuration is limited, so qualification is normally performed with a trial shell containing thermocouples at the hub and vane tips. Downstream processing includes stereolithography pattern production, support removal, ceramic shelling with a primary fused-silica slurry, controlled burnout, and casting of 17-4PH or CA-6NM martensitic stainless steel. Material certification for the final castings follows EN 10204:2004 type 3.1 inspection documents, and pressure-retaining components fall under PED 2014/68/EU when applicable. Terminal products are semi-open pump impellers, closed-channel impellers, and valve bodies for industrial flow control.

    Energy-Sector Hot-Section Casting: Pattern Density and Shell Drying Thresholds

    Heavy-duty gas turbine aftermarket foundries processing cobalt- and nickel-base hot-section hardware use DSM Somos ProtoCast™ AF 19122 for land-based turbine vane and shroud patterns where wax tooling is either unavailable or too slow for reverse-engineered replacement parts. The formulation addition ratio remains 100:0 by mass; large patterns are built with structural lattice infill between 5–10 vol% in load-bearing ribs and up to 20 vol% in non-structural bosses, which reduces resin consumption relative to solid sections by approximately 35–40%. Shell drying is controlled in humidity-regulated rooms at 22–24°C and 45–55% RH; drying time per coat is set by the shell thickness rather than by the pattern, because the photopolymer does not absorb water. The limitation in this application is burnout time: thicker energy-sector shells require longer low-temperature holds than aerospace shells to prevent retained carbon from transferring to the alloy surface. Radiographic acceptance of final castings follows ASTM E192 reference radiographs where specified. Terminal products are land-based gas turbine nozzle guide vanes, shrouds, and combustor-sector replacement castings.

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    DSM Somos ProtoCast™ AF 19122 Antimony-free Liquid Photopolymer is a vat-photopolymerization resin formulated for the production of sacrificial investment-casting patterns. The cured polymer article is used in an additive manufacturing workflow in which a ceramic shell is built around the pattern, after which the polymer is removed by thermal burnout and the cavity is filled with molten metal. The designation “antimony-free” identifies a compositional boundary: the formulation does not rely on antimony-based additives that are present in certain castable photopolymer systems. This boundary is relevant to foundries that restrict antimony oxide in combustion residues, to casting operations that experience surface inclusions from burnout residue, and to production sites that document metal-oxide emissions from shell removal.

    The material is supplied in liquid form and requires stereolithography equipment with a compatible wavelength and recoating system. Typical uses include jewelry investment casting, dental framework patterns, and low-volume industrial castings where complex geometry or small lot sizes do not justify wax injection tooling. Because the pattern is generated additively, the process eliminates the need for pattern-specific tooling and permits gate-and-riser geometry to be produced directly with the part.

    What Process Constraints Follow from Antimony-Free Photopolymer Chemistry?

    Antimony compounds, when present in castable photopolymers, can act as flame-retardant synergists, thermal stabilizers, or opacifiers. During burnout they may be converted to antimony trioxide, Sb2O3, or other non-volatile oxides. Sb2O3 has a melting point near 656 °C and can persist as a fused residue in ceramic shell pores. If the residue is entrapped in blind passages or narrow cores, the metal front can displace it and create a surface defect or non-metallic inclusion. The antimony-free formulation removes that specific residue class at the material level.

    The absence of antimony compounds is not a direct drop-in replacement for antimony-containing resins in all cases. Antimony additives influence refractive index, optical scattering, and thermal decomposition behavior. The photoinitiator package and cure response in ProtoCast AF 19122 therefore require machine-specific validation. The working-curve constants critical exposure, Ec, and depth penetration, Dp, should be re-established for the actual laser spot size, resin temperature, and chamber atmosphere. Published data for alternative machine configurations is limited, and first-article inspections are required after any change in build orientation, layer thickness, or post-cure protocol.

    Specification Fields for Lot Acceptance and Process Control

    Lot acceptance for a liquid photopolymer of this class typically includes viscosity, density, cure response, and cured mechanical properties. The values are post-cure dependent, so test specimens should be processed according to the manufacturer’s post-cure protocol and not mixed with specimens from other resin families. Table 1 lists the characterisation fields and the standards commonly applied to antimony-free castable photopolymers. The actual nominal values applicable to the current lot must be taken from the manufacturer’s technical datasheet and certificate of analysis because specification limits vary by formulation revision.

    Property or attribute Standard designation Application in evaluating ProtoCast AF 19122
    Density of cured solid ISO 1183-1:2019 Buoyancy method for pattern mass and thermal expansion calculations
    Tensile properties ASTM D638-14 or ISO 527-1:2019 Tensile strength, tensile modulus, and elongation at break on post-cured bars
    Flexural properties ISO 178:2019 or ASTM D790-17 Three-point bending for pattern rigidity during shelling
    Liquid viscosity ISO 2555:2018 or ASTM D2196-20 Rotational viscometry at controlled vat temperature
    Ash content ASTM D2584-18 Ignition loss and residue after combustion of cured specimen
    Glass transition temperature ISO 11357-2:2020 DSC determination for post-cure verification
    Water absorption ASTM D570-22 Percent mass gain after immersion for dimensional stability assessment

    Cured mechanical values are also influenced by post-cure irradiance and total exposure dose. A calibrated radiometer should be used to confirm the UV source delivers the dose specified in the resin datasheet, expressed in J/cm². Under-post-cured patterns can retain unpolymerized monomer that exotherms during shell burnout, while over-post-cured patterns can become brittle and crack during shell handling. Therefore, the post-cure step is considered part of the material specification envelope, not a secondary operation.

    Production-scale stereolithography platforms for castable resins commonly use solid-state lasers operating at the wavelength specified by the resin manufacturer. The vat temperature is maintained at the manufacturer’s recommended set point because viscosity and cure kinetics are coupled. Recoat blade speed and wait times are adjusted so that each slice receives a uniform liquid layer before laser scanning. For thin-walled patterns, build orientation should place shell drainage paths in the direction of furnace venting. If the pattern contains closed internal cavities, decomposition gas pressure during burnout may be sufficient to crack the ceramic shell.

    When Low Residual Ash Is a Critical-to-Quality Parameter in Shell Burnout

    The burnout cycle for ProtoCast AF 19122 is a process-critical operation. Furnace burnout of the photopolymer pattern follows a staged heating profile. In the first stage, the ceramic shell is heated slowly through the glass transition and thermal expansion region of the polymer. An excessive ramp rate produces thermal stress at the polymer-shell interface and can initiate shell cracking. In the second stage, the temperature is held to allow volatile decomposition products to escape through the sprue and vent channels. In the third stage, the furnace is brought to the shell firing temperature and held to oxidize carbonaceous residue. Antimony-free chemistry changes the ash composition but does not eliminate the need for oxygen access.

    Shell permeability, pattern cross-section, and the number of shell coats determine the maximum safe ramp rate. Foundries often validate burnout by sectioning fired shells and inspecting for carbon deposits or oxide residues before pouring. The absence of antimony compounds reduces the probability of a specific non-volatile oxide residue, but carbon residue can still form if the furnace atmosphere is stagnant or if the shell is inadequately vented. Burnout profiles must therefore be validated for each shell system and part family; published data for all shell configurations is limited.

    Use of a castable photopolymer differs from conventional foundry wax in a key operation. Wax patterns are often removed by steam autoclave dewaxing, but a crosslinked photopolymer cannot be melted out in that manner. Direct thermal burnout is used instead. This changes vent design, shell formulation, and furnace loading. Compared with antimony-containing castable stereolithography resins, the principal distinction is compositional: the formulation does not generate antimony oxide during shell firing. This can reduce the analytical burden for facilities that track antimony in process residues and can simplify waste stream documentation where customer specifications prohibit antimony-bearing additives. It does not automatically satisfy every restricted-substance list because the formulation contains other organic and inorganic components; material compliance documentation should be requested from the supplier for customer-specific requirements.

    Compared with general-purpose SLA resins, a castable resin must balance green-part strength with complete decomposition. A resin that leaves silica, glass-fiber, or mineral filler residues is unsuitable for investment casting because the residue cannot be readily removed from the shell cavity. ProtoCast AF 19122 is positioned for the castable category rather than for direct-use engineering parts. Compared with heavily filled or pigmented castable resins, the antimony-free formulation is intended to leave a lower total residue under controlled incineration. Low-residue behavior is nevertheless dependent on shell permeability, furnace airflow, and part mass. Residual carbon from incomplete burnout remains possible if oxygen access is restricted during the heating profile.

    Pattern Storage Must Control Moisture Uptake and Dimensional Drift

    Moisture uptake in cured patterns is a dimensional risk. If patterns are stored before shelling under high humidity, water absorption can produce small dimensional changes and can contribute to shell cracking if trapped moisture expands during burnout. Pre-shelling operations should verify that the pattern has been conditioned in a low-humidity environment. For production areas above 60 % RH, sealed containers or desiccated cabinets are typically used. Liquid resin is sensitive to ambient light and should be stored in opaque containers. The vat temperature should be allowed to stabilize before the build start; cold resin can increase viscosity and produce layer-thickness variation. The production area should avoid airborne dust that can contaminate the vat and cause surface defects or localised cure inhibition.

    Water absorption is evaluated according to ASTM D570-22, but the acceptance criterion is application-specific and should be set from casting trials rather than from generic polymer limits. Patterns that have absorbed moisture beyond the validated threshold should be reconditioned before shelling. Drying temperature and time must remain below the thermal distortion limit of the cured pattern; uncontrolled heating can cause dimensional drift and distortion.

    Managing Viscosity During Long Build Campaigns

    Long build campaigns require periodic viscosity checks with a calibrated rotational viscometer. The spindle geometry and rotational speed should match the manufacturer’s method because liquid photopolymers can show non-Newtonian behavior at low temperatures or high shear. If viscosity drifts upward, the cause is often partial polymerization in the vat due to stray light, excessive heat, or inadequate filtration after a previous build. The vat should be filtered through the mesh size specified in the equipment manual, and recovered resin should be blended with fresh material only in the proportion permitted by the manufacturer.

    Solvent thinning is generally prohibited. Solvent addition alters photopolymerization kinetics, reduces crosslink density, changes the burnout residue profile, and can introduce volatile contaminants into the build chamber. If the vat is left idle, the resin should be recirculated or stirred according to the machine supplier’s recommendation to avoid sedimentation or localised polymerization. Lot-to-lot viscosity variation should be tracked because a shift in viscosity at constant vat temperature changes recoating dynamics and can produce layer-thickness error. If viscosity exceeds the manufacturer’s upper limit, the material should be quarantined and dispositioned through the lot-review process rather than returned to the vat without filtration.

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