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Как аккредитованный DSM Somos Taurus Stereolithography (SLA) Polymer, UV Postcure завод, мы соблюдаем строгие протоколы качества - каждая партия подвергается строгим испытаниям для обеспечения последовательных стандартов эффективности и безопасности.
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When Taurus is used for silicone tooling masters, the primary process conflict is not dimensional growth but catalyst poisoning of addition-cure RTV silicone in contact with the photopolymer surface. Compliance gates for the master include ISO 2768-1:1989 general tolerances for printed features and ISO 4287:1997 surface texture verification, with Ra typically held at or below 3.2 μm on sealing faces after finishing. The formulation addition ratio is 100 wt% as-received Taurus; the master is built solid or with a closed-cell internal lattice at 100 μm layer thickness, and no talc, calcium carbonate, or metallic powder is added to the resin because particulate fillers induce laser scattering and reduce green strength at thin unsupported walls. Production begins with z-orientation of the parting line to avoid stair-step at shut-off edges, support generation only on non-molding surfaces, and a two-stage solvent rinse followed by UV postcure at 1.5–3.0 J/cm² UVA for 45–60 min. The post-cured master is then thermally conditioned at 40–50°C for 24 h to drive residual solvent and low-molecular-weight species from the surface; because sulfur-, phosphorus-, and nitrogen-containing residues can inhibit platinum-catalyzed silicone cure, the molding face is either sealed with a water-based acrylic barrier coat or the mold is poured with a tin-catalyzed condensation-cure RTV silicone. Terminal products are tin-catalyzed RTV silicone tools for low-volume polyurethane prototype casting, wax injection molds for lost-core testing, and vacuum casting blocks for soft-touch overmolded grips.
Under-hood fluid system prototypes produced from DSM Somos Taurus are evaluated for short-term exposure to hot ethylene glycol–water coolant blends, power steering fluid, and intermittent thermal soak at wall temperatures not exceeding 95°C. The compliance gate for such parts normally cites ASTM D543-20 for chemical resistance of plastics, ASTM D648-18 for HDT at 0.455 MPa, and ISO 175:2020 for immersion-related mass and dimensional change after 7 days at 70°C. Formulation addition ratio is 100 wt% as-received Taurus; no reactive diluent or tertiary amine accelerator is introduced because the viscosity at 30°C is already matched to the recoater blade clearing window, and amine contamination shifts photoinitiation kinetics toward premature gelation at the vat surface. On the production line, the resin is processed on a 355 nm solid-state laser SLA platform at 100 μm layer thickness, with a recoater dwell of 2–4 s and vat fill maintained above 60% of maximum capacity to prevent vortex entrainment at the recoater edges. After build, support removal is followed by a two-stage wash in 99% isopropanol or tripropylene glycol monomethyl ether for 10–15 min, then UV postcure in a chamber delivering 1.5–3.0 J/cm² UVA for 30–60 min, with part orientation rotated mid-cycle to reduce shadowing at deep clip recesses and fluid ports. Terminal articles include coolant overflow reservoir prototypes, EGR actuator mounting spacers, brake fluid reservoir necks, and harness stand-off brackets used for pre-production thermal validation; SAE J1455 full qualification of production under-hood electronics is outside the documented boundary of the unfilled photopolymer.
Cabin air distribution system prototyping with Taurus addresses the need for non-structural plenum mock-ups and duct flange prototypes that must hold hole-to-hole dimensions after 80°C dry airflow and repeated wipe-down with isopropanol or perchloroethylene-based cleaners. The documentation package for laboratory screening is aligned to ASTM D648-18 for heat deflection, ISO 291:2008 for standard atmosphere conditioning, and a preliminary vertical burn screen described in 14 CFR 25.853(a) Appendix F Part I; the unfilled photopolymer is not a qualified aircraft interior material in the as-printed state, so flying installation is outside the recorded boundary. Formulation addition ratio remains 100 wt% as-supplied Taurus because adding halogenated or phosphorus flame-retardant species would scatter the 355 nm laser beam, reduce critical exposure at 100 μm layer thickness, and create undercured interlayer boundaries. The manufacturing route begins with z-axis orientation of thin-walled duct shells to minimize trapped resin volume, followed by internal lattice venting where section thickness exceeds 6 mm; parts are then washed in a two-stage solvent line, post-cured under UV at 1.5–3.0 J/cm² UVA for 45 min, and hand-finished at mating surfaces. Terminal outputs include cabin plenum prototypes, drop-out panel mock-ups, and seat rail edge guards used only for form/fit/function studies and crew training fixtures.
Wind tunnel test hardware printed from Taurus is employed for surface pressure measurement models and aerodynamic load bodies that are not exposed to direct sunlight or long-duration soak above 90°C. Dimensional verification follows VDI/VDE 2630-2.1:2015 for computed tomography coordinate measurement and ISO 4287:1997 for surface roughness, while mechanical screening uses ASTM D638-14 for tensile modulus and ASTM D648-18 for HDT at 0.455 MPa. The formulation addition ratio is 100 wt% as-supplied photopolymer; no reactive diluent is added because a viscosity shift above or below the specified 30°C band changes recoat thickness and produces visible build-line offset at 100 μm layer increments. On the production floor, large models are sectioned into segments bounded by the vat platform size, printed with self-supporting span limits not exceeding 6 mm, washed in a two-stage solvent line, and UV post-cured for 60 min under rotating fixtures to deliver 1.5–3.0 J/cm² across all free surfaces. Because published data for this specific configuration is limited, Z-axis compensation factors are established per machine by measuring a printed calibration bar before committing to the full model; typical corrections are applied in the Z axis only, while X and Y dimensions remain tied to the laser scan field calibration. Terminal articles include half-span and full-span wind tunnel test models, surface pressure-tap wing sections, and underbody aero shields used in low-speed aerodynamic campaigns.
Taurus parts configured as electrical connector housings are typically built at 50 μm layer thickness so that snap-fit beam depths and latch retention faces approach injection-molded part geometry; after UV postcure, the material is evaluated for dielectric strength per IEC 60243-1:2013, volume resistivity per ASTM D257-14, and HDT per ASTM D648-18. The supplier documentation may list a UL 94 HB classification at a specified thickness; this is not equivalent to UL 94 V-0, and the current yellow card must be confirmed because formulation changes can alter flame response after postcure. The formulation addition ratio is 100 wt% as-received photopolymer; no conductive filler or antistatic additive is introduced because low-viscosity ionic additives bloom after UV exposure and contaminate contact surfaces. The production process includes shelling of thick housings to reduce wash solvent entrapment, a two-stage solvent rinse, UV postcure at 1.5–3.0 J/cm² UVA for 45–60 min, and a dry-air anneal at 60–70°C for 2 h to reduce residual stress before thread-forming and contact insertion. Terminal articles include connector housing prototypes, potting shells, sensor bracket insulators, and harness retainer bodies used in pre-production electrical packaging studies; continuous live insulation under IEC 60664-1:2020 requires end-user requalification because microcracks at layer interfaces can reduce creepage resistance over thermal cycling.
For electronics assembly benches, Taurus is converted into board support nests and stencil alignment trays where the process temperature remains below the 0.455 MPa HDT boundary of approximately 90–96°C; the material is not specified for reflow pallets, wave-solder carriers, or any continuous contact with molten solder above 180°C. Compliance boundaries include ANSI/ESD S20.20-2021 as a process document, with the explicit note that unfilled Taurus is not an ESD-dissipative material and must not be used as a replacement for conductive-filled polymer fixtures where static discharge protection is mandatory. The formulation addition ratio is 100 wt% as-received photopolymer; no antistatic agent is added because common ionic antistatic compounds migrate to the surface after UV postcure and contaminate bare board assemblies. Production uses 50 μm layer thickness for fine lead locators and 100 μm for larger support bodies, followed by a two-stage solvent rinse and UV postcure at 1.5–3.0 J/cm² UVA for 60 min to minimize residual tack. Terminal outputs include stencil alignment trays, selective soldering tooling for low-temperature preheat zones, conformal coating masking frames, and board support nests used only in manually loaded assembly cells.
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DSM Somos Taurus is an unfilled acrylate–epoxy hybrid photopolymer formulated for stereolithography platforms operating with 355 nm solid-state laser sources. The material is supplied as a low-viscosity liquid intended for layer thickness settings from 0.10 mm to 0.15 mm, although the actual slice thickness must be validated against the specific recoater configuration and build platform thermal conditions. Green-state parts are removed from the support structure, cleaned in a two-stage solvent process using isopropyl alcohol or tripropylene glycol monomethyl ether, and transferred to a UV postcure chamber. The postcure step is not an ancillary drying operation; it drives residual conversion of acrylate and oxirane groups and determines the final mechanical envelope, including tensile modulus, flexural strength, and heat deflection temperature. On galvo-driven 355 nm Nd:YVO4 laser systems, the resin exhibits sufficient green strength for support removal without collapse, but unsupported thin walls below 0.8 mm are at risk of warpage during solvent immersion and thermal postcure.
The UV postcure response of DSM Somos Taurus is controlled by irradiance, wavelength distribution, part thickness, and the thermal rise generated inside the postcure chamber. In unfilled acrylate–epoxy systems, photocure conversion progresses from the exposed surface inward, and thick walls develop a conversion gradient if the dose is too low. Process validation usually requires a calibrated radiometer to measure irradiance at the part plane. Postcure protocols commonly operate in the 365–405 nm UV-A band with irradiance levels from 5 mW/cm² to 20 mW/cm² for durations of 30–90 min, depending on section thickness and the uniformity of the chamber reflectors or LED array. Underexposed parts may exhibit reduced tensile modulus and lower heat deflection temperature even when the outer surface appears fully hardened. Therefore, production-scale postcure cells should be qualified with thermal probes and exposure mapping rather than by time alone.
Residual conversion can be monitored by Fourier transform infrared spectroscopy. The disappearance of the acrylate absorption near 1,620 cm⁻¹ and the oxirane absorption near 910 cm⁻¹ provides a quantitative indication of cure state. In practice, many molding and fixture suppliers use ASTM D648 heat deflection temperature as a release criterion after postcure because it integrates the effect of incomplete network formation. Lot-to-lot variation in postcure response is measurable when the vat temperature changes by more than ±3 °C; lower vat temperatures increase viscosity and reduce recoater leveling speed, while higher vat temperatures shorten gel time and can produce overcure artifacts on down-facing surfaces. Published data for this specific configuration under production-scale LED postcure arrays is limited, so qualification is recommended with the actual chamber geometry used for manufacturing.
DSM Somos Taurus occupies a specific position among SLA polymers. Representative supplier-published values after UV postcure place tensile modulus in the 2,200–2,500 MPa range, tensile strength between 42 MPa and 50 MPa when tested to ASTM D638M, and flexural modulus in the 2,000–2,400 MPa range under ASTM D790M. Elongation at break is typically below 3%, which distinguishes the material from high-elongation ABS-like SLA resins. Heat deflection temperature at 0.46 MPa is generally reported in the 60–70 °C class, while the 1.82 MPa value is lower. These values constrain continuous service under load. The material is therefore best described as a stiff, moderate-temperature photopolymer rather than a high-heat SLA grade.
Compared with Somos WaterShed XC 11122, Taurus displays increased tensile modulus and reduced elongation, making it more suitable where dimensional stability under mechanical load is more important than impact absorption. Compared with ceramic-filled grades such as Somos PerFORM, Taurus has a lower modulus and a lower heat deflection temperature, but it is easier to finish, less abrasive to machining tools, and less prone to brittle edge chipping during post-processing. These differences are not grading defects; they define the processing and application envelope. The resin is not a true thermoplastic, despite its rigid mechanical response, and it should not be exposed to aggressive solvent immersion, strong amine-containing coatings, or service temperatures above the published heat deflection threshold unless the application is validated by part-specific testing.
In laser-exposed vat photopolymerization, working curve parameters determine the depth of cure and the accuracy of vertical walls. For unfilled acrylate–epoxy resins, the critical exposure at the 355 nm laser wavelength is typically adjusted on the build platform by measuring cured thickness across a range of energies. The working curve is then used to set laser draw speed and hatching overlap for each layer. On systems with a 0.10 mm layer thickness, the nominal cure depth is adjusted to exceed the layer thickness by 1.3–1.6× to ensure layer adhesion without excessive undercutting. If the exposure is too high, down-facing surfaces develop rounded edges and dimensional accuracy decreases. If the exposure is too low, interlayer adhesion fails and parts may delaminate during solvent cleaning or postcure.
Cleaning is a critical process boundary. Residual liquid resin retained in blind holes and deep channels can continue to polymerize during UV postcure and cause dimensional distortion or surface haze. Two-stage solvent rinses with agitation are preferred: a first stage to remove bulk uncured resin and a second stage to remove residual solvent-diluted resin. Solvent temperature should be controlled below 30 °C because prolonged exposure of green-state parts to warm solvent increases solvent uptake and can reduce final tensile modulus. After cleaning, parts should be dried with filtered compressed air at low pressure to avoid depositing solvent-borne resin on critical surfaces. The maximum permissible solvent contact time is a function of wall thickness; thin walls below 1.0 mm should receive shorter immersion cycles than solid bulk parts.
A UV postcure chamber used for Somos Taurus should be configured to provide uniform irradiance across the full build envelope. Rotating platforms, multi-lamp reflector arrays, or high-density LED panels reduce anisotropic cure. Thermal management is also relevant: the exotherm released during final conversion can raise part temperature above the chamber set point, particularly in solid sections thicker than 25 mm. If the part temperature exceeds the heat deflection temperature during postcure, sagging or stress relaxation can occur. Thermal probes placed inside representative parts are more informative than chamber air temperature. The postcure step should therefore be treated as a controlled thermal and photochemical process, not as a simple drying operation.
For dimensional inspection, parts should be conditioned at 23 °C ± 2 °C and 50% ± 5% relative humidity before measurement. This follows standard practice under ISO 291 or ASTM D618 and minimizes reversible moisture-related changes. Unfilled SLA resins can absorb low levels of moisture during post-processing and service; a temporary dimensional change of less than 0.3% is typical for short-term humidity exposure, but continuous immersion should be avoided. If the part is to be scanned on a coordinate measuring machine, the supporting fixture should not induce bending loads that exceed the material modulus. For a rigid unfilled resin with an elastic modulus in the 2,000–2,500 MPa range, thin spans may deflect measurably under probe contact, so support spacing must be specified by the metrology plan.
In production-scale service, one observed failure mode is cracking of sharp internal corners after repeated thermal cycling. The low elongation at break below 3% provides limited strain accommodation. Internal radii below 0.5 mm should be increased where feasible, and stress concentrations at insert bosses or threaded features should be reinforced. The material can be drilled, tapped, and machined with standard carbide tooling, but brittle edge chipping can occur if feed rates are excessive. For parts requiring threaded inserts, heat-stake insertion or adhesive-bonded inserts are preferred over aggressive interference fits. If inserts are pressed into undersized holes, cracking can initiate at the hole edge because of the low fracture strain of the highly crosslinked network.
When replacing traditional machined tooling or polyurethane casting resins with Somos Taurus, the selection must be governed by thermal load, mechanical load, and environmental exposure. The material is suitable for short-run injection molding fixtures, assembly jigs, and locating nests that experience moderate clamping pressures and temperatures below the 0.46 MPa heat deflection limit. For mold trials involving glass-filled or mineral-filled engineering resins with melt temperatures above 200 °C, published data for this specific configuration is limited and the thermal mass of the printed fixture may not provide sufficient insulation or heat resistance. In such cases, Taurus can be used for prototype tooling only if the mold inserts are thermally isolated or if the trial is limited to a small number of shots.
For wind tunnel or fluid-flow test articles, Somos Taurus offers the geometric accuracy and surface finish expected from stereolithography. Surface roughness after postcure is controlled by layer thickness, build orientation, and downstream finishing. Parts built at 0.10 mm layer thickness exhibit less pronounced stair-stepping than those built at 0.15 mm. Critical aerodynamic surfaces are typically sanded and filled to remove layer lines, after which the part must be re-inspected for contour deviation. Because the resin has a rigid unfilled matrix, sanding is slower than for softer ABS-like resins but produces a stable surface that does not load abrasive paper as heavily. Dimensional stability of the finished surface under moderate airflow and elevated ambient temperature should be verified if test conditions exceed 50 °C.
The application of Taurus to injection molding fixtures requires an explicit evaluation of clamping force distribution and cavity temperature. For a small prototype mold insert built entirely from the resin, the limiting factor is not always the peak melt temperature but the accumulation of heat over repeated cycles. In a short-run trial with fewer than 25 shots using polypropylene at melt temperatures near 190 °C, localized surface softening may occur if the part is not cooled between cycles. A metal sprue bushing, water lines, or conformal cooling channels are generally not present in a printed resin insert, so cycle time must be extended to dissipate heat. The available published information from production-scale tooling trials using this specific photopolymer is limited; therefore, end users should run process capability studies with the intended material and cycle count before committing to pre-production use.
For assembly jigs and locating fixtures, the stiffness of Taurus supports pick-and-place repeatability when the jig is bolted to a rigid subplate. The material’s tensile modulus in the 2,200–2,500 MPa range provides a stable locating face, but torque on threaded fasteners must be limited. Fastener bosses should include generous wall thickness and should not be loaded above 0.5 N·m without a metal insert. If the jig is exposed to cutting fluids, release agents, or mild alkaline cleaners, the supplier should be consulted for chemical compatibility. Strong solvents, including ketones and chlorinated hydrocarbons, can attack the crosslinked matrix and produce surface softening or cracking over repeated exposure. No general-purpose SLA resin of this class should be assumed resistant to all industrial cleaners without immersion testing under ASTM D543 or an equivalent material compatibility procedure.
Electrical housings and enclosures printed in Taurus may be considered when the operating temperature is below the heat deflection threshold and the mechanical loads are primarily static. The unfilled resin is not electrically conductive and does not provide EMI shielding; coatings or inserts must be specified separately. If the part is to be painted, a primer system free of aggressive amines should be selected, and adhesion should be verified by cross-cut testing under ISO 2409 or ASTM D3359. Because the photopolymer network is sensitive to UV and moisture over long service life, external-use parts should be coated with an opaque UV-blocking topcoat to reduce surface degradation. No conclusion regarding long-term outdoor durability is incorporated in the standard datasheet, and weathering performance should be evaluated under ISO 4892-3 or ASTM G154 if the component is deployed outside a controlled environment.