| Код ТН ВЭД | 700884 |
Как аккредитованный завод Prodways PLASTCure Pattern 2500 Liquid Resin for 3D Printing, мы соблюдаем строгие протоколы качества - каждая партия подвергается строгим испытаниям для обеспечения последовательных стандартов эффективности и безопасности.
| Упаковка | Prodways PLASTCure Pattern 2500 Liquid Resin for 3D Printing comes in a 1 kg opaque plastic bottle with secure cap. |
| Погрузка контейнера (20-футовый контейнер) | 20′ FCL container loaded with palletized drums of Prodways PLASTCure Pattern 2500 Liquid Resin for 3D printing, secured for transport. |
| Доставка | Prodways PLASTCure Pattern 2500 Liquid Resin is generally shipped as a non-regulated liquid under DOT, IATA, and IMDG. It requires sealed, opaque, leak-proof containers, upright handling at ambient temperature, and protection from light, heat, and freezing. Always follow the SDS and local regulations. |
| Хранение | Store Prodways PLASTCure Pattern 2500 Liquid Resin in its original, tightly closed container in a cool, dry, well-ventilated area. Protect from direct sunlight, UV light, heat, sparks, and ignition sources. Keep away from incompatible materials, food, and children. Maintain recommended temperature, typically 15–25°C, and do not freeze. Follow SDS guidance. |
| Срок годности | Typical shelf life is 12 months when kept unopened in its original container, away from light, at 15–25°C. |
In lost-wax casting facilities producing fine jewellery under multi-shift batch schedules, the substitution of hand-carved or injected wax with DLP-printed pattern resin changes the failure mode from wax distortion to photopolymer thermal expansion. The resin is maintained at 100 wt% as-supplied concentration in the vat; no reactive diluent or plasticizer is added because dilution widens the thermal decomposition interval and increases residual carbon after burnout. On 405 nm DLP systems operating with recoat speeds of 5–7 mm/s, the pattern is produced at 25–50 µm layer thickness, rinsed in isopropanol, and post-cured in a 405 nm LED chamber until green strength is sufficient to survive centrifugal casting preparation. Compliance for finished articles under EU REACH Annex XVII Entry 27 requires nickel release testing by EN 1811:2023 with a non-piercing-article limit of 0.5 µg/cm²/week; this regulatory obligation falls on the casting alloy and finishing process rather than the polymer pattern, but the burnout must not leave ceramic-trapped residues that alter the metal surface. Patterns are assembled onto wax trees with sprue joints occupying 2–5 wt% of total assembly mass, invested in gypsum-bonded refractory, and de-waxed before programmed burnout. Terminal product types include rings, pendants, earrings, brooches, and hollow beads cast in 9–24 karat gold and sterling silver.
On production-scale DLP arrays, the highest scrap rate occurs during the transition from flash de-waxing to burnout when flask internal pressure increases faster than the gypsum-bonded refractory can vent. This condition is observed in flasks loaded above 60% pattern volume, where residual ash at the metal contact surface forms black carbon spots on filigree sections. The corrective protocol includes a de-wax pressure hold at 0.2–0.4 MPa before ramp and a burnout plateau at 650–750°C with a minimum air turnover of 6–8 flask volumes per minute; these values are specific to gypsum-bonded jewellery investment and may not transfer to phosphate-bonded dental equipment. When the printed pattern wall drops below 0.3 mm, copper or silver alloys with high thermal conductivity may also chill before filling fine details, so pattern mass is matched to flask size and alloy pour temperature rather than treated as a fixed variable.
Dental fixed prosthodontic workflows expose printed patterns to constraints that do not appear in jewellery casting, particularly the need to preserve the gingival margin sharpness after support removal and investment. The resin is charged at 100 wt% as-supplied with no powder filler, because dispersed filler raises viscosity beyond the recoat capability of a DLP vat and leaves ash in the cervical third of the casting. CAD compensation for the cement gap is set at 30–40 µm, while printed margins are specified at 0.2–0.3 mm to provide sufficient green strength without sacrificing burnout gas escape. Production begins with intraoral scan data, followed by CAD design and DLP printing at 25 µm Z-layer thickness; supports are removed under magnification, and the pattern is invested in a phosphate-bonded refractory. Burnout is ramped at 1–3 °C/min to a terminal temperature of 850–950°C, followed by induction or arc casting of cobalt-chromium or titanium. Compliance is governed by ISO 13485:2016 Clause 7.5.2 for production process controls and ISO 10993-1:2018 for biological evaluation; terminal product types include Co-Cr and titanium crown copings, three-unit bridge frameworks, and implant overlays where castable pattern resin replaces milled wax.
Aerospace investment casting foundries using colloidal silica shell systems encounter a process conflict when photopolymerized patterns replace injected wax: the linear thermal expansion of the pattern can exceed shell strength during the first dewax phase. The resin is kept at 100 wt% as-supplied in the DLP vat, with no wax addition, because a two-phase wax-resin blend produces non-uniform expansion and shell cracks in 0.8–2.0 mm wall sections. Patterns for turbomachinery prototypes are printed at 25–50 µm layers, assembled onto central sprue logs, and coated in 8–10 colloidal silica slurry layers. Flash dewax is performed at 150°C; burnout then follows a ramp of 1–2°C/min to 1050°C with a hold of 2 h, after which vacuum induction melting introduces nickel-based superalloys such as Inconel 718 or titanium alloys such as Ti-6Al-4V. Compliance falls under AS9100D for aerospace quality management and ASTM E1131-20 for thermogravimetric ash assessment; terminal product types include prototype turbine blades, impellers, compressor vanes, and structural brackets produced as short-run investment castings.
Production-scale foundries record shell cracking when the thermal ramp from 150°C to 600°C exceeds 2°C/min, because the photopolymer expands before the sintered ceramic network develops microcracks for venting. The standard corrective cycle reduces ramp to 1°C/min and introduces a 300°C plateau for 1 h to volatilize residual acrylic components before the shell face coat reaches full rigidity. Published product-specific data for aerospace shell compatibility with this exact resin grade remains limited; the ramp rates and hold times above reflect standard colloidal silica shell practice for castable photopolymers rather than a resin-specific warranty. In the casting cell, vacuum induction melting requires the shell to be preheated to 1050°C before pouring, and the pattern burnout must deliver a clean internal surface with ash below 0.05 wt% to avoid inclusion defects in thin trailing-edge sections.
| Sector | Standard / Regulation | Test Method | Acceptance Threshold |
|---|---|---|---|
| Fine jewellery | EU REACH Annex XVII Entry 27 | EN 1811:2023 | ≤ 0.5 µg/cm²/week nickel release for non-piercing articles |
| Dental fixed prosthodontics | ISO 13485:2016 Clause 7.5.2 | ISO 10993-1:2018 biological evaluation | Printed margin retained at 0.2–0.3 mm without cervical distortion |
| Aerospace turbomachinery | AS9100D / ASTM E1131-20 | Thermogravimetric ash assessment | ≤ 0.05 wt% residue after 1050°C burnout |
| Micro-mechanical casting | EU REACH Annex XVII Entry 27 | EN 1811:2023 | ≤ 0.5 µg/cm²/week nickel release for finished metal parts |
| Removable partial denture casting | ISO 13485:2016 / ISO 22674:2016 | Phosphate-bonded investment burnout process validation | Pattern-to-investment volume ratio ≤ 70% |
Micro-mechanical component casting for watch cases, bezels, movement bridges, and decorative metallic hardware uses photopolymer patterns in mass ranges from 0.1 g to 2.0 g, where even small residual ash becomes a surface defect because finishing tolerances are tight. The vat is charged with 100% as-supplied resin; no solvent reduction is permitted because solvent residues reduce green strength and widen the burnout gas release window. Patterns are printed at 25 µm layer thickness with pattern walls held between 0.35 mm and 1.00 mm; thinner sections collapse during support removal, while thicker sections retain carbon at the core if the burnout soak is insufficient. Downstream, patterns are invested in fine-grained ceramic or phosphate-bonded molds, de-waxed, and burned out at a terminal temperature of 750°C before centrifugal or static vacuum casting of stainless steel, gold, or platinum. Compliance obligations include EU REACH Annex XVII Entry 27 and EN 1811:2023 for nickel release on finished metal parts; terminal product types include watch bezels, movement bridges, clasp bodies, and micro-mechanical levers.
Multi-cavity flask protocols for removable partial denture frameworks generate larger exothermic mass during burnout than single-unit crown flasks, because the volume of photopolymer in a single flask may exceed 30 mL and the gas channels through the phosphate-bonded investment become the limiting factor. The resin is used at 100% as-supplied concentration, with no added wax or filler, and the pattern-to-investment volume ratio is held at or below 70% to preserve continuous venting paths during dewax; clasp and major connector patterns are specified at 0.8–2.5 mm cross-section. Production begins with digital design of clasp assemblies and major connectors, followed by DLP printing at 25–50 µm Z resolution, support removal, and assembly onto preformed sprues. Investment is poured under vacuum, and burnout is ramped at 1–3°C/min to 900°C before induction casting of cobalt-chromium or titanium. Compliance is governed by ISO 13485:2016 Clause 7.5.2 and ISO 22674:2016 for metallic dental materials; terminal product types include removable partial denture frameworks, implant-supported bars, and hybrid framework substructures.
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Prodways PLASTCure Pattern 2500 is a filled liquid photopolymer formulated for vat photopolymerization systems operating at a nominal 405 nm wavelength. The resin is classed as a burnout-grade material for investment-casting pattern production. It is supplied as a low-to-medium-viscosity suspension in which an organic wax-type filler phase is dispersed in a reactive acrylate or methacrylate matrix. During printing, the filler remains homogeneously distributed under shear; after solidification, the green pattern is a rigid solid with dimensional stability suitable for ceramic shell investment. The 2500 designation does not by itself establish mechanical performance; batch-specific viscosity, filler content, and cured modulus are given on the manufacturer certificate. The material is intended for use in jewellery, dental-cast frameworks, and small precision-casting work where the final part is obtained by burning out the polymer pattern at intermediate furnace temperatures and pouring a metal or ceramic slurry into the negative cavity. Unlike a standard rapid-prototyping resin, Pattern 2500 is not selected for long-term polymer end parts because its oxidative degradation pathway is engineered to leave low residue rather than to retain strength.
The resin is imaged by a 405 nm digital light projector or mask-projection engine. Such a filled suspension scatters light more intensely than an unfilled transparent model resin; consequently, the Jacobs working curve for batch release shows a lower penetration depth Dp and a higher critical exposure Ec at the build surface. On production systems with a calibrated radiometer at the vat surface, irradiance values for DLP casting resins of this class are commonly set between 2 mW/cm² and 5 mW/cm², but the usable value depends on the projector optics, vat base film, and pigment package. Process engineers should not transfer exposure recipes between machine models or resin batches without a cure-depth test. A 50 µm layer thickness on an aluminium build platform often requires a minimum wait period after blade pass for the filled resin to recover from shear; the interlayer delay is established from dynamic viscosity measurements per ASTM D4287-19 at a shear rate of 10 s⁻¹.
Recoating failure is the primary processing limit. Unlike unfilled resins that return quickly to a uniform film, a filled resin can develop a visible wave pattern or matte islands when the vat temperature is below 24 °C. Vat heaters are typically set to 28–30 °C for products in this category to reduce dynamic viscosity and improve leveling. Temperatures above 32 °C may shorten the dark stability of the bath, especially in systems with a heated projector or unsealed vat. Suspensions settle during idle periods, so the resin should be stirred or recirculated after 8 h or before new builds. Batch-to-batch variation in filler loading is more severe than in homogeneous photopolymers and can shift the required exposure by 10–15 %. Incoming resin should be inspected both for viscosity and for a small cure-depth witness using a multi-step exposure tile.
The dominant failure mode on manual production lines is green-state cracking of filigree shanks, prong tips, and gallery sections during support removal. Because the cured network contains a high fraction of sacrificial filler and a reduced ductile-to-brittle threshold, sections thinner than 1.5 mm fracture at lower bending strain than neat model resins. Support cutters should be sharp and should not twist perpendicular to the shank. Residual stress from over-post-curing contributes to delayed cracking after cleaning. Cured patterns should be examined under 10× magnification for microcracks before investing; if a microcrack is present, investment slurry can penetrate the pattern, anchor it to the shell, and increase the stress generated during thermal expansion. The pattern can be solvent-welded to a wax sprue, but excessive solvent exposure softens the acrylate matrix and causes surface whitening. Unlike thermoplastic injection wax, Pattern 2500 cannot be re-melted and re-used for gating; removed support scrap is chemical waste.
Dimensional stability after printing is not determined by pixel resolution alone. A filled casting resin undergoes green shrinkage immediately after removal from the build plate and then additional stress relaxation over the following hours. On a flat granite surface, a ring or flat pattern may change by up to 2 % in free length over 24 h if it was heavily overexposed or post-cured too aggressively. Dimensional acceptance for small jewellery casting patterns is often expressed as a linear tolerance of ±0.1 mm over a 25 mm reference length, verified with a profile projector or coordinate measuring machine. Foundries apply a tooling offset that accounts for polymer green shrinkage, ceramic shell expansion, and metal casting contraction. Any residual shrinkage from Pattern 2500 must be included in this offset; it cannot be eliminated by adjusting furnace temperature alone because the ceramic shell also expands on heating.
Burnout of a filled acrylate pattern is a multi-stage process. The low-temperature stage involves melting and volatilization of the organic wax-type filler, usually in the region between 150 °C and 300 °C, while the crosslinked polymer matrix degrades at higher temperatures in the presence of oxygen. If the furnace ramp is too steep, gas evolution can exceed the gas permeability of the freshly set phosphate-bonded shell and cause internal pressure cracking. Manufacturers of similar filled resins often specify a hold near 250 °C and a controlled ramp toward 700–750 °C; the exact schedule for Pattern 2500 must be taken from the current Prodways burnout guide and matched to the measured shell permeability. Ignition residue is determined after furnace oxidation at 750 °C in air using ISO 3451-1:2019. Foundry acceptance limits for high-polish precious-metal castings are commonly below 0.1 % by mass, but published data for this specific resin configuration is limited to batch certificates and the technical data sheet; no alternative figure should be used for release.
Post-cure and cleaning also affect burnout behaviour. The build platform is drained for at least 10 min, and parts are washed in two stages of fresh isopropanol or a dedicated solvent. Each stage is usually limited to 3–5 min; prolonged immersion extracts filler and produces pits or frosted surfaces. Air-drying is followed by a UV post-cure dose commonly in the range of 1–3 J/cm² depending on section thickness and chamber uniformity. Over-post-cure raises stiffness but also increases internal stress, causing warping in long shanks or thin ring shoulders. Support nibs are removed before post-cure where possible. If wet sanding is performed, a drying period of at least 2 h at 22 ± 2 °C is required before investing. The surface should be cleaned with a non-solvent debubblizer; alcohol-based debubblizers may etch the resin if left longer than 5 min.
Production diagnostics show that a castable pattern is not defined by surface quality alone. Unfilled acrylate model resins can print with high resolution, yet during burnout they may leave a continuous carbonaceous film that is not detected until metal pitting occurs on polished surfaces. The defect is especially costly in filigree or hollow sections where air passages are narrower than 1 mm. Furnace ignition residue per ISO 3451-1:2019 is therefore a release test for casting-pattern substitution. If the residual ash of a candidate material exceeds the foundry rejection limit, the material is not a drop-in replacement even when it prints on the same machine. Compared with such unfilled model resins, Pattern 2500 is designed with sacrificial filler pathways that lower the mechanical strength of the green part but improve the decomposition pathway. The trade-off is intentional: the material is chosen for cavity cleanliness, not for prototype durability.
Compared with injection-moulded investment wax, Pattern 2500 eliminates the aluminium or steel injection tool and permits direct digital production of hollow or lattice structures. It is, however, a rigid thermoset-like solid and does not exhibit the same melt-viscosity behaviour as a filled wax pattern. Runner assembly and pattern repositioning are performed by adhesive bonding or solvent welding, not by wax melt joining. Compared with quartz-filled or ceramic-filled high-temperature stereolithography resins, Pattern 2500 is not formulated to remain as a fired ceramic skeleton during casting; it is intended to be removed before metal introduction. This distinction matters because a residue-free cavity requires an oxidizing atmosphere and adequate dwell time at the peak burnout temperature. The product should not be combined with strong amine or thiol additives, which can trigger premature gelation or interfere with photoinhibition in the vat.
| Characteristic | Test designation | Process-control relevance |
|---|---|---|
| Dynamic viscosity at 25 °C, shear rate 10 s⁻¹ | ASTM D4287-19 | Determines vat heater setpoint and recoating wait time |
| Ignition residue after 750 °C furnace oxidation | ISO 3451-1:2019 | Checks burnout residue against casting acceptance limits |
| Tensile modulus of cured specimen | ASTM D638-14 | Indicates rigidity during support removal and investment |
| Flexural strength of cured specimen | ISO 178:2019 | Measures resistance to bending fracture in thin sections |
| Linear thermal expansion via thermomechanical analysis | ASTM E831-19 | Evaluates expansion mismatch with ceramic shell |
Uncured resin absorbs moisture in high-humidity cells. Water uptake changes viscosity, reduces green strength, and introduces bubbles during recoating. Vats and containers should be sealed when not in use, and the production room should be held at 22 ± 2 °C and 40 % relative humidity in accordance with ISO 291:2018 conditioning guidance. Before a build, the batch number, date of first opening, and vat temperature are recorded. Resin that has been in an open vat for more than 72 h should be strained through a 190 mesh sieve to remove cured fragments. Mixed batches should be avoided on critical castings because minor differences in filler content alter the exposure response and can produce visible banding in the cured pattern. Metal tools made from copper or brass should be minimized; leached metal ions can affect the photopolymerization kinetics of some acrylate systems. The product should not be used for direct food-contact or implant applications unless the current Prodways safety data sheet and REACH registration explicitly authorize the end use. Disposal of uncured resin and solvent wash liquor must follow local regulations for reactive photopolymers.