| Код ТН ВЭД | 205148 |
Как аккредитованный завод DSM Somos 7110 Epoxy Photopolymer, UV Postcure, мы соблюдаем строгие протоколы качества - каждая партия подвергается строгим испытаниям для обеспечения последовательных стандартов эффективности и безопасности.
| Упаковка | DSM Somos 7110 Epoxy Photopolymer, UV Postcure, in 1 kg opaque black plastic bottles with secure caps and labeled cartons. |
| Погрузка контейнера (20-футовый контейнер) | 20′ FCL loaded with DSM Somos 7110 Epoxy Photopolymer, UV Postcure, securely palletized, shrink-wrapped, and braced for safe chemical transport. |
| Доставка | DSM Somos 7110 Epoxy Photopolymer, UV Postcure is not regulated as dangerous goods for transport. No UN number, class, or packing group. Ship in original, tightly sealed, light-resistant containers, upright, away from heat, freezing, and ignition sources. Follow DOT, IATA, IMDG, and local rules. |
| Хранение | Store in a cool, dry, well-ventilated area away from direct sunlight, UV light, heat, sparks, and open flames. Keep containers tightly closed when not in use, protect from freezing, and maintain recommended temperature (typically 15–30°C). Avoid moisture and incompatible materials. Follow SDS and local regulations; use within shelf life. Store locked or in a designated chemical storage area. Ensure secondary containment. |
| Срок годности | Shelf life is not applicable for this UV-postcured epoxy photopolymer, as it is a stable solid under normal storage conditions. |
A low-pressure injection mold insert is built on a 355 nm stereolithography platform equipped with a Somos 7110 material file. The resin is a single-part epoxy photopolymer, so no mixing ratio is applied before transfer. The vat is stirred gently with a low-shear paddle at ≤20 rpm to reincorporate settled photoinitiator without whipping air into the bath. Layer thickness is held at 0.100 mm or 0.125 mm. After the build, the insert is cleaned in the manufacturer-recommended solvent, air-dried, and UV postcured in a 320–400 nm chamber with part rotation. Postcure time is determined by wall section. Thick gate regions require longer exposure to avoid green-state surface tack. Inserts are used for short-run unfilled polypropylene and low-density polyethylene prototype molding. Melt temperature must remain below 200°C. Clamp force on the vertical molding machine is limited to 50 tonnes because edge chipping has been observed in unfilled epoxy photopolymer tooling. Gate land edges are inspected with optical profilometry after every 100 injection cycles. Edge chipping at the gate and thermal fatigue at sharp shut-off corners are the dominant failure modes. Published data for specific cycle counts in glass-filled polypropylene is limited. The insert is not used with polycarbonate melt above 260°C or with glass-filled materials. Dimensional acceptance follows ISO 1101. Milled cooling channels are not included. Heating channels are avoided. The terminal product is a short-run injection molded clip or housing. Surface roughness is measured with ISO 21920-2. Shut-off surfaces must remain above 1.2 mm thickness to resist clamping deformation.
Solid SLA patterns are vulnerable to ceramic shell cracking during wax removal and flash-fire burnout. A hollow pattern with a wall thickness of 1.5 mm reduces expansion stress. Drain holes of 2 mm diameter are placed at the lowest point of each cavity. The epoxy photopolymer is burned out at 700°C for 2 h in an air furnace. Heating rate must not exceed 2°C/min between 200°C and 500°C. Higher rates cause shell spalling in thin trailing-edge sections. Ceramic slurry coating uses a zircon flour primary coat. Pattern expansion is controlled by comparing the resin CTE against the shell modulus. The actual CTE value must be taken from the current manufacturer datasheet. Published data for this specific configuration is limited. The foundry must validate residual ash below 0.1 wt% for alloy compatibility. Before burnout, the pattern is sealed with a water-based latex barrier to prevent solvent attack. No mixing ratio is applied. Finished terminal parts are 17-4 PH stainless steel brackets and impeller castings. Casting dimensional tolerance is checked per ISO 8062-3. Coupon hardness is verified with ASTM E384. Warpage in thin airfoil patterns is assessed with blue-light scanning after burnout. The main process conflict is not brittle pattern fracture but shell cracking caused by residual expansion during ramp. A heating ladder before standard burnout is mandatory.
Underhood exposure to gasoline vapor, engine oil mist, and ethylene glycol coolant creates combined chemical and thermal aging. Single-step UV postcure leaves residual reactive oxirane groups in thick flanges. These groups can continue to react during engine heat cycling. Dimensional creep appears near bolt bosses. A mixed postcure sequence of UV exposure followed by thermal soak at 80°C for 2 h reduces residual stress. Chemical resistance is screened in ASTM D543-21 immersion tests. Test fluids include ASTM Reference Fuel C, SAE 5W-30 oil, and 50/50 glycol-water. Specimens are weighed before and after 168 h immersion at 60°C. Mass change and hardness retention are recorded. Published data for this specific Somos 7110 fluid aging is limited. Prototype manifolds are fabricated with 0.100 mm layers. Wall thickness is kept over 2.5 mm at runner joints. Threaded inserts are installed after postcure with an epoxy adhesive. The adhesive must be resistant to glycol. Leak testing uses ASTM E515-11 bubble leak method. Dimensional inspection follows ISO 1101. The terminal product is a validation intake for cold-side charge air systems. This application is not used for continuous immersion in hot coolant at 100°C.
Wind tunnel model shells built from Somos 7110 are used for aerodynamic validation of airfoil sections and intake ducts. The dominant process issue is stair-step roughness on low-angle leading edges. A layer thickness of 0.050 mm is selected for surfaces with slope below 15° from horizontal. This reduces sanding time but lengthens build time. Filled epoxy primer is applied in thin coats. Hand sanding with 240-grit abrasive is followed by 400-grit wet sanding. Coordinate measuring machine inspection after primer verifies profile deviation. Pressure taps are installed by drilling after postcure. Tap edges are sealed with cyanoacrylate. Model halves are bonded with a structural methacrylate. The bond line is placed on the symmetry plane to avoid load-bearing areas. UV postcure is done before bonding to prevent residual stress. Surface waviness is measured with ISO 25178-2 areal parameters. Final painted shells are used in subsonic wind tunnel campaigns. Test section speed is usually below 80 m/s. Published data for specific aerodynamic load limits is limited. Vibration from buffeting can initiate cracking at trailing edges thinner than 0.8 mm.
Connector body prototypes are built to check terminal retention and harness routing before production tooling. The unfilled epoxy photopolymer has dielectric stability that depends on absorbed moisture. Parts are conditioned at 23°C and 50% RH for 48 h before testing. Dielectric strength is measured per ASTM D149-20. Comparative specimens are conditioned at 85°C and 85% RH for 96 h. Dielectric shift is recorded, not assumed. Surface leakage is checked after condensation cycling. Terminal insertion force is compared with molded production connectors. The resin is used for low-release harness validation only. High-voltage connectors above 600 V require additional creepage and clearance studies. Flammability classification should be verified against the current UL 94 data sheet. RoHS conformity is screened against RoHS 2011/65/EU Annex II restricted substances by X-ray fluorescence. REACH SVHC conformity is documented by the material supplier. Published data for this specific configuration is limited. No mixing ratio is required. Vat temperature is maintained at 30°C during builds to stabilize layer recoating. Finished terminal parts are connector housings, backshells, and wire dress fixtures. IP protection rating is not assigned to SLA prototypes unless gasketed. Mating cycles are limited to 20 because latch arms may abrade. Assembly torque on screw terminals is limited to 0.5 N·m to prevent boss cracking.
| Application | Key test | Condition | Verification target |
|---|---|---|---|
| Low-pressure mold insert | ISO 21920-2 | Surface roughness after 100 cycles | Gate land edge chipping |
| Investment casting pattern | ISO 8062-3 | Burnout and shell ramp | Dimensional tolerance and ash content |
| Underhood manifold prototype | ASTM D543-21 | 168 h at 60°C | Mass change and hardness retention |
| Wind tunnel model shell | ISO 25178-2 | Primed airfoil surface | Areal waviness and profile deviation |
| Electrical connector body | ASTM D149-20 | 23°C/50% RH and 85°C/85% RH | Dielectric strength shift |
| Orthotic master pattern | ISO 10993-5 | Extract dilution | Cytotoxicity screening |
| Compressor rig vane pattern | ASTM D648-18 | Heat deflection under flexural load | Rig hub interface temperature |
Anatomical master patterns are built for vacuum-forming corrective orthoses. The pattern must withstand repeated drape-forming at 140°C to 160°C. UV postcure is followed by thermal annealing at 80°C for 2 h. This improves heat resistance. Pattern surface is sealed with a solvent-resistant clear coat before plaster mold transfer. Cytotoxicity screening uses extract dilution. The material is not implantable. It is used only as a master pattern that contacts the final orthotic material indirectly. Skin sensitization risk is screened with ISO 10993-10. Published data for this specific Somos 7110 medical configuration is limited. The terminal product is a custom-contoured ankle-foot orthosis. Vacuum-forming is done with 3 mm to 5 mm polypropylene sheet. The pattern must be preheated to 60°C before forming to reduce thermal shock. No mixing ratio applies. The build orientation places the ankle region away from the support side. Support nibs are removed and polished with 600-grit abrasive. Warpage during postcure must be checked by scanning. Acceptance is ±0.5 mm over 200 mm. This application avoids steam autoclaving. The pattern is disinfected with 70% ethanol wipes. Ethanol contact must not exceed 2 min because solvent crazing may occur.
Compressor rig vane patterns are used for aerodynamic testing in low-speed rotating rigs. The patterned blades are bonded to a metallic hub. Creep occurs at the dovetail root if postcure is incomplete. A combined postcure of UV exposure plus 2 h at 80°C reduces residual reactive species. The resin is built at 0.060 mm layer thickness for thin trailing edges. Support structures are placed away from the leading edge. After postcure, vane surfaces are hand-polished to remove layer lines. The root is potted with a high-temperature epoxy. Balance is checked on a static balancing mandrel. Imbalance is corrected by removing material at the tip. The assembled rig is run below the resin heat deflection temperature. Heat deflection is measured per ASTM D648-18. Temperature at the hub interface is monitored with thermocouples. Published data for specific rotational speed limits is limited. Final terminal parts are polymer vane patterns for flow visualization. The pattern is not used in the hot section. Dimensional inspection follows ISO 1101. Surface profile is verified with a coordinate measuring machine. Vane chord dimension is held within ±0.1 mm. No mixing ratio is needed. Resin viscosity drift is checked by recoating blade corners. If the vat sits longer than 72 h, the resin is stirred at low speed before use.
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DSM Somos 7110 Epoxy Photopolymer, UV Postcure, is a cationic epoxy-based liquid resin for vat photopolymerization, classified within process category VP-P under ISO/ASTM 52900:2021. The material is formulated for laser-based stereolithography platforms operating at 355 nm, where the green part is built layer-by-layer and subsequently exposed to UV postcure to complete oxirane conversion and stabilize final mechanical properties. Because polymerization proceeds by photoacid-initiated ring-opening of epoxide groups rather than free-radical acrylate propagation, the system exhibits different shrinkage, moisture sensitivity, and postcure response than acrylate-based stereolithography resins. It is supplied as a single-component, opaque liquid; the cured surface and opacity are employed in master patterns, casting models, and dimensional test articles, but the material is not intended for optical transmission parts. Lot-specific viscosity, reactivity, and post-cured mechanical data are controlled through certificates of analysis and should be verified on the target production equipment rather than assumed from generic published values.
Following green-state build, the part is removed from the platform, drained, and washed in a solvent compatible with partially cured epoxy. Drainage channels are positioned in hollow regions to prevent trapped resin pockets from leaching during downstream handling. Wash time is limited because solvent uptake plasticizes the partially cured network and can produce surface crazing after postcure. Supports are removed before final UV exposure; postcured support structures require higher mechanical force and can leave fracture marks on thin walls. Vat temperature during recoating is maintained within the range specified by the equipment manufacturer, typically 28–32 °C for low-viscosity epoxy resins, to stabilize layer thickness. Layer height is commonly fixed at 0.050 mm or 0.100 mm, and laser-beam compensation is set in the build processor so that final dimensions fall inside inspection tolerance after postcure. On production lines, dimensional capability is verified by measuring a three-axis test coupon with a coordinate-measuring machine rather than relying on nominal laser diameter alone. Because the green state has limited strength for aggressive clamping, vacuum chucks and low-pressure workholding are preferred during finishing.
Failure modes encountered on production-scale stereolithography equipment include resin carry-over on the recoater blade, loss of platform vacuum during layer separation, and local overcure from laser power drift. The liquid resin is conditioned in the vat before the job; bubble entrainment after pouring is removed by a waiting period or slow blade travel. Resin temperature is allowed to stabilize, because a thermal gradient between the top surface and bulk vat changes effective viscosity and layer geometry. Operators record recoating parameters, beam-spot ellipticity, and vat temperature for each lot. When a lot change occurs, the first build is restricted to qualification coupons; tensile and flexural specimens are built across the entire platform to detect edge-to-centre variation. This procedure is required because photoacid concentration and resin age can shift sensitivity to laser energy. No solvent is introduced into the vat; a separate wash station prevents contamination that would alter polymerization kinetics.
The green article produced by the stereolithography laser contains a substantial fraction of unreacted monomer and low-molecular-weight oligomers. The laser dose is selected to fix geometry and attach layers, not to saturate all oxirane groups. The subsequent UV postcure operation, performed in a chamber or conveyor unit with UVA fluorescent lamps, supplies additional photon energy and thermal mobility to propagate the cationic reaction. Postcure effectiveness is thickness-dependent because UVA fluence attenuates through cured polymer; thick sections can retain a conversion gradient after a fixed surface dose. That gradient contributes to residual stress and can be released as distortion when the part is machined or exposed to thermal cycles. Process control therefore includes radiometric mapping of the postcure chamber, recording surface dose per face, and repositioning parts to reduce lamp shadowing. No single universal dose is specified because lamp spectrum, irradiance, part thickness, and chamber temperature vary; a dose matrix should be qualified by testing tensile bars per ISO 527-2 and deflection-temperature specimens per ISO 75-2. When postcure is insufficient, final heat-deflection temperature and tensile modulus remain below the supplier-reported values. When chamber temperature approaches the glass transition or UV dose is excessive, colour shift and warpage can occur. The glass-transition temperature is measured by differential scanning calorimetry per ISO 11357-2, and a residual cure exotherm should be absent after a complete postcure cycle. Because cationic epoxy polymerization is moisture-sensitive, postcure at relative humidity above 60% is not recommended without dry-air purge; water vapour competes with propagation and can depress surface hardness. Operators must not stack parts in front of lamps or block the shortest-wavelength UVA emission lines; reflective aluminium chamber surfaces are used to improve fluence uniformity.
| Property/Requirement | Method/Standard |
|---|---|
| Process classification | ISO/ASTM 52900:2021 |
| Tensile properties | ISO 527-2 |
| Flexural properties | ISO 178 |
| Deflection temperature | ISO 75-2 |
| Notched impact | ISO 180/A or ASTM D256 |
| Water absorption | ISO 62 |
| Ash content for burnout process | ASTM D2584 or ISO 3451-1 |
| Linear expansion during burnout | ISO 11359-2 |
| Chemical regulation | REACH (EC) No 1907/2006; RoHS Directive 2011/65/EU |
In material-selection decisions, DSM Somos 7110 is evaluated against polypropylene-like and water-clear stereolithography resins using identical post-cured coupons. Polypropylene-like systems typically show higher elongation and lower flexural modulus under ISO 178, while water-clear systems are optically transparent and may have lower initial viscosity but require stricter postcure to prevent colour shift. The epoxy photopolymer is selected when lower linear shrinkage and dimensional stability after postcure are more important than high impact-energy absorption. Nevertheless, cationic polymerization of epoxy systems can be slower than acrylate formulations, and exposure energy per layer may be higher on some 355 nm platforms; build-speed comparisons must use the same orientation and layer thickness. Differences between products are documented with a matrix of tensile modulus, elongation, deflection temperature, water absorption, and notched-impact values measured on post-cured coupons using the standards identified above.
For investment casting pattern production, the cured pattern must burn out inside the ceramic shell without generating excessive gas pressure or shell fracture. Epoxy photopolymers have a higher coefficient of linear expansion than the surrounding alumina-silicate shell under burn-out heating; the heating ramp is therefore staged to allow gas transport before full oxidizing burnout. Hollowing or an internal lattice is used to reduce solid cross-sectional area, and drainage paths are confirmed by weighing the pattern before and after staining or by CT inspection of internal cell walls. Residual ash is then governed by pattern mass, furnace atmosphere, and shell permeability. Because epoxy formulations can leave carbonaceous residue when oxygen is restricted, burn-out cycles are developed with the specific shell system and binder chemistry. Production foundries using primary slurries based on zircon and colloidal silica report that dimensional tolerance and shell cracking are the primary constraints, while ash mass is a secondary control for non-critical alloys. Published data for this specific resin in production foundry configurations are limited; qualification should be conducted on the candidate shell system with instrumented pyrometry rather than inferred from generic epoxy behaviour.
Ceramic shell cracking in investment casting is frequently caused by the pattern exerting diametric strain during the preheat segment of the burn-out cycle. For DSM Somos 7110, the relevant material property is the linear expansion of the post-cured epoxy network measured by thermomechanical analysis under ISO 11359-2. The measurement must be performed on specimens cut from the actual build orientation and layer thickness because vat photopolymerization produces anisotropy in thermal expansion and glass-transition behaviour. A pattern with thick flanges or sharp internal corners can concentrate expansion stress at the shell mould-parting line; shell failures observed on production lines are often intermittent because they depend on layer thickness, shell dewax ramp, and ambient humidity before dipping. The corrective action is to hollow the pattern, add compliant internal structure, or increase shell permeability by modifying primary slurry rheology.
In process engineering terms, the green pattern is not stable enough to be used as a master after aggressive solvent cleaning; final dimensions are specified only after UV postcure and thermal conditioning. Conditioning can include a postcure oven step at a controlled temperature with a residence time scaled to wall thickness. Thicker sections require longer time for thermal equilibration, but the maximum temperature must remain below the glass transition to avoid warpage. After conditioning, parts are inspected on a coordinate-measuring machine; inspection protocols should include datum features that are preserved from the build orientation. Dimensional comparisons across multiple lots are used to track batch-to-batch variation in low-viscosity epoxy lots, which can shift with photoacid concentration and resin age. Because operational boundaries include humidity during storage, resin containers must be sealed and brought to room temperature before use; condensation on cold resin surfaces can introduce water into the cationic reaction and produce soft layers.
Secondary finishing of post-cured DSM Somos 7110 includes wet sanding, bead blasting, and machining. The cured epoxy network responds to high-speed tooling with heat generation that can soften local material if spindle speed and feed rate are excessive. Carbide end mills are preferred over high-speed steel because the polymer matrix is moderately abrasive. Machining is performed after a stabilization period following postcure, typically 24 h, so that short-term residual-stress relaxation does not invalidate final dimensions. Dust extraction is required; cured epoxy dust is treated as a particulate exposure hazard and controlled through engineering controls and SDS-defined limits. The material is not compatible with strong oxidizing acids and certain ketone-based solvents under prolonged immersion; swelling and surface attack follow the general behaviour of cured epoxy networks. If a silicone tool is poured against a Somos 7110 master, the release agent must be selected to avoid poisoning platinum-cured silicones; tin-cured systems may be less sensitive but have different mould-release characteristics and dimensional fidelity.