| Код ТН ВЭД | 376054 |
Как аккредитованная DSM Somos ProtoGen™ 18120 эпоксидная смола для стереолитографии, UV Postcure на заводе HOC +3, мы соблюдаем строгие протоколы качества - каждая партия подвергается строгим испытаниям для обеспечения последовательных стандартов эффективности и безопасности.
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Under-hood validation units are printed from DSM Somos ProtoGen 18120 as a single-component epoxy stereolithography resin, charged at 100 wt% as supplied with no reactive diluent and no additional photoinitiator. Vat resin temperature is held at 28–30 °C to keep viscosity within the 250–330 mPa·s range required for stable recoater blade return. A layer thickness of 0.050 mm on a 355 nm solid-state stereolithography platform yields green parts with sufficient edge definition for snap-fit connector shells, wire retention clips, sensor housings, and ECU mounting brackets. After a two-stage tripropylene glycol methyl ether solvent rinse, parts are dried and subjected to the manufacturer-specified UV postcure at HOC +3 for 60 min in a conveyorized UV chamber equipped with simultaneous thermal hold. Dimensional and mechanical acceptance follows ISO 16750-4:2010, Clause 5.3.1.1 for temperature cycling from −40 °C to 85 °C at a ramp rate of 5 °C/min for 300 h; production connector validation under USCAR-2 is not claimed for SLA prototypes unless sealing, overmolding, and terminal retention are separately qualified. Because heat deflection temperature at 0.46 MPa for this resin class remains below 85 °C, under-hood parts must be shielded from direct exhaust contact or supported by metal brackets during engine-load simulation. Green parts stored above 60 % relative humidity for more than 24 h are pre-dried at 40 °C for 2 h before postcure to avoid surface dimpling and inconsistent tensile modulus measured under ASTM D638-14.
| Parameter | Test method or equipment | Reported operating range |
|---|---|---|
| Vat resin temperature | Digital probe in stereolithography vat | 28–30 °C |
| Layer thickness | 355 nm solid-state laser platform | 0.050–0.100 mm |
| UV postcure at HOC +3 | Conveyor UV chamber with thermal hold | 30–60 min |
| Pre-dry threshold for green parts | Forced-air oven | 40 °C for 2 h when RH > 60 % |
Investment casting patterns manufactured from ProtoGen 18120 for low-volume turbocharger bracket and small pump housing trials are built as monolithic patterns; the liquid resin is used at 100 wt% as supplied and is not blended with pattern wax, filler, or reactive diluent. Hollow pattern construction with internal drain holes is preferred to reduce thermal mass and limit gas volume during burnout. The ceramic shell is built with a zircon-based primary slurry and colloidal silica binder, then dewaxed at 150–170 °C before the pattern is eliminated in a forced-air burnout furnace. The critical thermal window for epoxy gas evolution occurs between 250 °C and 450 °C; ramp rates above 5 °C/min in this interval can crack the primary shell, especially at thin trailing edges. A qualified burnout profile uses a ramp rate of 2 °C/min from 300 °C to 800 °C, with a 3 h hold at 800 °C. Ash residue is checked under ASTM D5630; published ash data for ProtoGen 18120 under this specific bottom-injection furnace configuration is limited, so foundries pre-qualify the resin on a five-pattern lot and set an internal residue threshold of ≤0.1 wt% after combustion. The downstream process then proceeds with shell preheating, alloy pouring of stainless steel or cobalt-chrome, and knockout. Terminal finished product types include prototype stainless steel turbocharger actuator brackets and cobalt-chrome pump housings for non-certified flow validation.
After the manufacturer-specified UV postcure at HOC +3 is completed, vacuum casting master patterns produced from ProtoGen 18120 are wet-sanded with 800–1200 grit SiC paper to a surface roughness Ra of ≤0.4 µm, measured under ISO 21920-2:2021. Formulation addition ratio is 100 wt% of the as-supplied resin; no low-viscosity epoxy sealer or surface primer is incorporated into the liquid resin because post-cure dip coats alter silicone release and degrade fine-edge dimensional conformance under ISO 286-1:2010. The finished master is framed and a two-part platinum-cure silicone rubber with Shore A 25–35 is mixed at 10:1 by weight, vacuum-deaerated at −0.09 MPa for 5 min, and cured at 40 °C for 4 h to form the mold. Polyurethane vacuum casting follows with pattern dimensional compensation of 0.3–0.5 % to account for cast part shrinkage. Terminal products are non-certified polyurethane gearbox covers, sensor housings, and overmolded soft-touch tool grips used for assembly form and fit validation.
Sealed enclosure prototypes for edge-node sensors are printed in ProtoGen 18120 at 100 wt% neat resin and post-cured under the manufacturer-specified UV postcure at HOC +3 before humidity ageing. No flame-retardant additive is introduced because halogen-free FR fillers can scatter the actinic laser and reduce green-part edge definition; the bare photopolymer is therefore not claimed as a production flame-rated enclosure material. Damp heat exposure follows IEC 60068-2-78:2012, Clause 7, at 85 °C / 85 % RH for 1,000 h. Water absorption measured under ASTM D570-98 is tracked for each lot; if 24 h water uptake exceeds 0.5 wt%, the batch is dried at 40 °C before dimensional measurement. For a 3 mm uniform wall section, x–y dimensional drift typically remains below 0.1 %; bosses, snap hooks, and ribs with local wall sections under 1.5 mm exhibit higher relative creep at condensation temperatures and require fillet radii of at least 0.8 mm. The downstream process includes vat photopolymerization, postcure, damp heat ageing, then installation of an EPDM or silicone gasket; no ingress protection rating is assigned unless the assembled enclosure passes a separate IP67 test. Terminal finished product types include edge-node enclosure shells, sensor caps, and battery housings for low-energy non-flammable devices.
In non-potable fluid manifold sections for pilot-scale chemical dosing equipment, ProtoGen 18120 is used as a 100 wt% single-component photopolymer without internal lubricant, PTFE, or graphite filler because dispersed particles scatter the laser and create under-cured zones at the vat floor. The downstream process includes vat photopolymerization at 0.100 mm layer thickness, the manufacturer-specified UV postcure at HOC +3, and three-axis CNC milling of sealing faces to a flatness tolerance of 0.05 mm per ISO 1101:2017. Hydrostatic pressure testing is run at 2.0 bar for 30 min in water at 23 °C; no production leakage rating is claimed beyond this prototype evaluation. The service window is limited to non-oxidizing aqueous streams at pH 4–10 and temperatures below 40 °C. NSF/ANSI 61 certification is not claimed, and the material is not recommended for potable water contact or strong oxidizing environments. Terminal finished products are manifold bodies, valve bodies, and pump casing prototypes installed on pilot-scale dosing skids for flow distribution verification.
Non-implantable surgical instrument handles and cutting-guide prototypes printed from ProtoGen 18120 are pre-screened under ISO 10993-5:2009 for cytotoxicity using an L929 mouse fibroblast cell line. Formulation addition ratio is 100 wt% as supplied; no plasticizer, radiopaque filler, or impact modifier is added unless a full extractables study under ISO 10993-12:2021 demonstrates that the additive does not alter the leachate profile. After the manufacturer-specified UV postcure at HOC +3, parts are rinsed in a 70 % isopropanol / 30 % deionized water solution for 10 min, then stabilized at 23±2 °C for 24 h before packaging. Surface roughness after post-processing is specified at Ra ≤0.8 µm to reduce bioburden entrapment. Contract manufacturing traceability is maintained under ISO 13485:2016. Gamma sterilization at 25 kGy may shift color and reduce impact; any sterilized lot is validated under ISO 11137-1:2006 before clinical simulation. Terminal products are trial sizers, non-implantable instrument handles, and surgical guide prototypes used for pre-operative contour verification.
Конкурентоспособная эпоксидная смола DSM Somos ProtoGen™ 18120 для стереолитографии, UV Postcure по ценам HOC +3, которые соответствуют вашему бюджету - гибкие условия и индивидуальные котировки для каждого заказа.
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DSM Somos ProtoGen™ 18120 is an epoxy-based liquid photopolymer supplied for vat photopolymerization stereolithography using 355 nm solid-state laser scanning. The material designation includes UV postcure at HOC +3, identifying a postcure protocol offset of +3°C relative to the baseline HOC reference. The resin does not follow free-radical acrylate polymerization. Photoacid generation under laser exposure initiates cationic ring-opening of epoxide groups, and the network continues to propagate during dark cure and thermal postcure. This mechanism gives the material a strong dependency on postcure temperature control and produces rigid, opaque parts after full cure.
Manufacturer-published representative values for fully postcured specimens are listed in the following table. The values are typical results obtained with the test methods shown, not specification limits. Batch-to-batch variation on production platforms is controlled primarily by resin age, vat humidity, laser energy calibration, and postcure temperature uniformity.
| Property | Typical value | Test standard |
|---|---|---|
| Liquid density at 25°C | 1.14 g/cm³ | ISO 1183-1 |
| Viscosity at 30°C | 260 mPa·s | ASTM D2196 |
| Tensile strength | 60 MPa | ASTM D638-14 Type I |
| Tensile modulus | 2900 MPa | ASTM D638-14 Type I |
| Elongation at break | 5% | ASTM D638-14 Type I |
| Flexural strength | 90 MPa | ASTM D790-17 Method A |
| Flexural modulus | 2700 MPa | ASTM D790-17 Method A |
| Notched Izod impact | 25 J/m | ASTM D256-10 Method A |
| Heat deflection temperature at 0.46 MPa | 110°C | ASTM D648-18 Method B |
| Heat deflection temperature at 1.82 MPa | 68°C | ASTM D648-18 Method A |
| Glass transition temperature, DSC | 82°C | ISO 11357-2 |
The two heat deflection temperature values define the practical thermal design envelope. The 0.46 MPa HDT of approximately 110°C indicates tolerance for short-duration contact with heated fixtures, silicone cure cycles, and low-pressure autoclave processes. The 1.82 MPa HDT of approximately 68°C is the more restrictive limit for load-bearing service because it approximates the temperature at which the network softens under structural stress. The tensile modulus near 2900 MPa places ProtoGen 18120 in the rigid structural prototyping class, distinct from elastomeric SLA materials and from filled epoxies that sacrifice elongation for higher heat resistance.
Specific gravity near 1.14 is typical for unfilled epoxy formulations; filled grades may be denser but introduce settling and viscosity penalties. The notched Izod value of 25 J/m is lower than many impact-modified acrylate resins, so design rules must account for notch sensitivity at sharp corners and gate vestiges.
Postcure temperature is not a secondary step for ProtoGen 18120. The HOC +3 offset moves the chamber thermal condition +3°C above the standard HOC reference to compensate for heat loss from part fixturing and to raise segmental mobility in partially converted epoxy domains. In a chamber equipped with 365 nm fluorescent or LED lamps and convective heating, the thermal setpoint should be verified with a contact thermocouple placed on a sacrificial control part. Air-temperature readings alone do not capture the exothermic rise from continued cationic propagation inside thick sections.
Published data for HOC +3-specific postcure performance is limited to equipment manufacturer process documentation rather than a formal ASTM protocol. The narrow processing window is nevertheless clear from epoxy SLA process experience. Local part surface temperature should remain within ±3°C of the HOC +3 target during the first 15 min of postcure. Deviation beyond ±5°C can create differential conversion between thick and thin walls, producing after-cure bow and heat deflection temperature scatter. Production-scale SLA service operations have reported that controlled thermal soak is more effective than UV dose alone in reducing residual epoxide in this resin class, because dark-cure propagation is diffusion-limited at ambient temperature.
High-output UV chambers vary in spectral output and fluence rate. A radiometer calibrated at 365 nm should be placed at the part location because reflective walls, part shadowing, and lamp age create local fluence differences. The HOC +3 offset does not compensate for inadequate UV dose; photoacid generation depends on absorbed UV energy, while the thermal offset drives subsequent dark-cure propagation. Both parameters are coupled: insufficient UV dose produces a low acid concentration, and no practical thermal soak can fully polymerize an under-exposed green part. Differential scanning calorimetry of partially postcured parts typically shows a residual exotherm that declines below 5% of total reaction enthalpy after complete HOC +3 curing. Prolonged HOC +3 exposure beyond 120 min can over-advance the network and reduce notched Izod impact, especially in thin sections. The postcure recipe should therefore be qualified with both HDT and impact specimens on the actual chamber, not transferred from another machine without radiometric and thermal mapping.
Vat handling and recoating parameters control scrap rate before postcure. At 30°C, the liquid viscosity is approximately 260 mPa·s, which permits stable recoating at layer thicknesses between 0.05 mm and 0.15 mm on standard 355 nm SLA platforms. At ambient relative humidity above 60%, the uncured resin surface absorbs moisture and green-part dimensions can shift before postcure. Build chambers should be maintained with dry air purge or the resin surface blanketed with inert gas when the vat remains open for extended runs. Storage temperature should remain between 15°C and 30°C, and the resin should be protected from stray 405 nm light to preserve photoacid generator stability.
On 355 nm laser systems, working curve parameters must be established on the target machine. For this resin class, critical exposure Ec is typically below 10 mJ/cm², and depth of penetration Dp is near 0.15 mm for a 0.10 mm layer, but exact values vary with laser spot size, scan spacing, and resin age. Published data for ProtoGen 18120-specific working curves across all machines is limited, so iterative window-pane exposures are required after vat replenishment. Green parts should be rinsed in isopropyl alcohol or the machine manufacturer's recommended solvent for less than 15 min under air agitation, followed by forced-air drying at 30°C before HOC +3 postcure. Prolonged solvent immersion can plasticize the partially cured network and reduce final flexural modulus.
Unlike free-radical acrylate systems, cationic epoxy cure is not strongly inhibited by ambient oxygen, so surface cure is less sensitive to nitrogen blanketing. The primary environmental interference is moisture, not oxygen. Water reacts with the propagating cationic species and can reduce polymer chain growth. This is why uncontrolled humidity in a production vat appears as lower peak HDT in postcured parts, even when laser energy remains constant.
ProtoGen 18120 is selected when acrylate SLA materials fail by creep or distortion at moderate heat. Acrylate systems cure by free-radical propagation that is largely complete after laser exposure, while ProtoGen 18120 requires thermal postcure to achieve its published HDT and modulus. The epoxy network exhibits lower volumetric shrinkage and better resistance to moisture-driven dimensional change after cure, but it demands longer postcure and tighter humidity control before the build. The 0.46 MPa HDT of approximately 110°C exceeds that of many unfilled acrylate SLA grades, which commonly deflect below 70°C under the same stress; however, comparisons should be based on datasheets using the identical ASTM D648-18 test condition.
The material is not a drop-in replacement for transparent acrylate grades. ProtoGen 18120 is opaque and cannot be used where optical clarity is required. Within the epoxy SLA family, it is positioned below higher-temperature filled systems in 1.82 MPa HDT but offers lower viscosity and easier recoating. Published direct comparison data is limited, so selection should be governed by end-use thermal stress, impact requirements, and build chamber capacity. The resin should not be combined with amine-based additives or acid-scavenging fillers, because both interfere with cationic propagation and can reduce final conversion.
Impact-modified acrylate grades may show higher notched Izod values and faster room-temperature property development, but they often exhibit lower HDT and higher linear shrinkage. The dimensional stability advantage of ProtoGen 18120 is most visible in long, thin features that would otherwise accumulate shrinkage stress across a build platform. ProtoGen 18120 should not be blended with other SLA resins, especially acrylates, because phase separation and localized inhibition can produce uncured pockets.
Postcured ProtoGen 18120 stock is rigid enough for secondary machining on three-axis CNC equipment with carbide or diamond tooling. Spindle speeds above 18000 rpm combined with low feed rates can generate frictional heat that locally exceeds the 1.82 MPa HDT, causing edge smearing or rounding. Coolant or compressed air is required for thin walls below 1.0 mm. Because the resin has low thermal conductivity relative to metal, heat concentrates in the chip and workpiece surface; vacuum fixtures are preferred over mechanical clamps for thin sections. The material is used for investment casting patterns and silicone tooling masters because it can be sanded, primed, and bonded without the layered delamination common in some low-strength acrylate models.
Electrical connector housings and short-run functional enclosures introduce notch-sensitivity constraints. The notched Izod impact of 25 J/m per ASTM D256-10 indicates limited resistance to sharp-corner impact; design rules should specify 0.5 mm minimum internal fillet radii where loading is dynamic. Assembly with adhesives requires surface abrasion and solvent wipe. Cyanoacrylate and two-component epoxy adhesives are commonly used, but published lap-shear data for ProtoGen 18120 is limited. Designs requiring threaded inserts should use heat-staking or ultrasonic insertion only after verifying that local frictional heating does not exceed the 1.82 MPa HDT.
For fluid-contact applications, the cured network is generally resistant to mild aqueous solutions and aliphatic hydrocarbons, but polar solvents such as methyl ethyl ketone or dichloromethane can swell the part. Published data for specific fluid resistance is limited; immersion screening per ASTM D543-21 is recommended before use in fuel or brake fluid environments. Long-term outdoor exposure can yellow the unpainted epoxy surface and reduce surface hardness. Parts exposed to sunlight should be coated with an opaque UV-blocking primer. Accelerated weathering data for ProtoGen 18120 under ASTM G154 is limited, so end-use qualification is required.
Regulatory compliance under REACH and RoHS must be confirmed against current supplier declarations, because formulation additives can change without notice. Cured parts intended for indirect food-contact or medical use require separate extraction testing under applicable ISO standards; the standard technical datasheet does not establish biocompatibility. Resin stored beyond 24 months should be re-qualified for viscosity and working curve before production use.