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Как аккредитованный завод DSM Somos NanoForm™ 15120 Nanocomposite Resin for Stereolithography, UV & Thermal Postcure, мы соблюдаем строгие протоколы качества - каждая партия подвергается строгим испытаниям для обеспечения последовательных стандартов эффективности и безопасности.
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DSM Somos NanoForm 15120 is a mineral-filled nanocomposite stereolithography resin that reaches structural performance only after two sequential postcure stages: a UV exposure that immobilizes the green surface and a forced-air thermal cycle that drives conversion of residual acrylate. The application field is restricted to five downstream segments where elevated heat deflection, high modulus, and low elongation are functional requirements rather than incidental properties.
In turbine engine and turbocharger foundries, the resin acts as a sacrificial positive for investment casting because thin trailing-edge patterns survive ceramic shell coating without flexural distortion. Compliance standards: foundry acceptance typically references ASTM D638-14 for cured tensile validation and ASTM D648-18 for heat deflection, while castings are inspected by ASTM E192 reference radiographs or equivalent digital detector arrays. Formulation ratio: the vat is charged with 100 wt% NanoForm 15120 as supplied; no reactive diluent or post-added photoinitiator is introduced because changes in initiator concentration alter the green modulus and shell-coating adhesion. Downstream process: patterns are built at 50 µm layer thickness on a 355 nm scanning-laser stereolithography system, solvent-washed, UV-postcured on a rotating fixture, thermally postcured in a forced-air oven, and then hand-sealed with a shell-compatible primer. Ceramic shell build uses alternating zircon and alumina slurry with controlled humidity; dewax is performed in an autoclave at 150–170°C, followed by a burnout ramp to 900°C to remove residual carbon. Finished part types: rotating turbine blade positives, nozzle guide vane clusters, and turbocharger compressor wheel positives. The critical process conflict is ash residue after burnout; published data for this specific configuration is limited, so each foundry qualifies the resin against its own shell permeability and ash specification.
Field evaluation on injection moulding lines indicates that NanoForm 15120 inserts are viable for short-run PP and ABS validation when the cavity pressure is limited, but glass-filled engineering polymers are outside the demonstrated window. Compliance standards: insert stiffness is validated with ISO 178:2019 and ASTM D648-18, while mould trial capability is judged by Cpk >1.33 on critical dimensions. Formulation ratio: the resin is used undiluted at 100 wt% in the vat; no pigment dispersion or internal release agent is mixed in because light attenuation and polymerization kinetics would shift. Downstream process: tool inserts are printed at 50 µm layer thickness with 2–3° draft and shut-off walls above 2 mm; after washing, UV postcure and thermal postcure, surfaces are hand-polished to ISO 4287 Ra 0.4 µm. The inserts are mounted in steel or aluminium bolsters and then trialled on a press with injection velocity reduced and cavity pressure held below 40 MPa; published fracture limits for specific geometries are limited. Finished part types: PP battery covers, ABS electronic housing prototypes, PE snap-fit validation caps, and TPE overmoulding cores. Surface erosion and heat checking occur with short runs of glass-filled PA, so that material is excluded.
After full thermal postcure, the resin can be used for short-run underhood sensor brackets and connector backshells because the dense network provides dimensional stability during dyno testing, but continuous exposure to hot water-glycol is outside the validated range. Compliance standards: enclosure prototypes are screened against USCAR-2 Rev 7 mechanical shock and sealing requirements, and flexural data are generated according to ISO 178:2019; long-term glycol aging data at 120°C is not fully published. Formulation ratio: the material is processed as a one-part liquid at 100 wt% with storage between 5°C and 30°C; no additional monomer is introduced into the printing vat. Downstream process: components are printed at 75 µm layer thickness with mating features placed off the Z-axis, then solvent-dipped, UV-postcured on a rotating frame, and thermally postcured in a nitrogen-purged oven to reduce oxidative yellowing. Contact retention features are designed with a 0.2 mm minimum root radius. Finished part types: engine sensor bracket prototypes, coil bobbins, connector backshells, and ECU enclosure lids for thermal cycling and dyno tests. The operational boundary is sustained temperature above 150°C, where the polymer matrix may undergo further densification and dimensional shift.
When aerodynamic load testing demands a stiffer scale model with low surface waviness and minimal deflection under dynamic pressure, the mineral-filled network after cure reduces the need for metallic stiffening frames in subsonic sections. Compliance standards: surface finish after hand working is specified to ISO 4287 Ra 0.8 µm, flexural stiffness is verified with ASTM D790-17, and balance calibration follows the test facility’s internal six-component load cell protocol. Formulation ratio: sectional models are printed with 100 wt% NanoForm 15120 as the primary build material; where segments must be bonded, a low-viscosity photopolymer adhesive is kept below 5 wt% of total segment mass to avoid local density offsets. Downstream process: large CAD bodies are partitioned, printed at 100 µm layer thickness on a large-frame stereolithography system, UV-postcured with a rotating axis, thermally postcured using a stepped ramp to control warpage, then abrasive-jet cleaned and bonded. Wet sanding to Ra <0.8 µm is followed by urethane sealing and non-outgassing topcoat. Finished part types: half-wing test articles, air intake ducts, rotor wake survey probes, and scale missile bodies for subsonic tunnel operation. Leading edges above Mach 0.7 require metal sheathing according to facility-specific erosion protection criteria.
CFRP panel manufacturing lines use printed NanoForm 15120 fixtures for drilling and trimming because the cured network does not soften during an autoclave dwell at 180°C, provided the thermal postcure ramp has reached full conversion. Compliance standards: fixture geometry after thermal soak is qualified by coordinate measuring according to ISO 10360-2, and compressive creep is screened with ISO 604:2002. Formulation ratio: the build vat operates at 100 wt% NanoForm 15120 with no diluent; hollow shell designs use 4 mm wall thickness to reduce thermal gradient distortion. Downstream process: fixtures are printed as hollow shells with internal honeycomb ribs, washed, UV-postcured for green handling, thermally postcured in an air-circulating oven with a stepped ramp, and then fitted with metal drill bushings press-fitted into printed bores. Finished part types: CFRP panel drill templates, autoclave indexing jigs, edge trimming fixtures, and assembly alignment gauges. Direct contact with uncured epoxy resin in the autoclave is avoided by using a sacrificial release film because solvent absorption may soften the surface.
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DSM Somos NanoForm™ 15120 is a nano-reinforced stereolithography resin supplied for solid-state laser vector scanning at 354.7 nm and intended for use with both UV and thermal postcure. The 15120 model designation is associated with a nominal heat deflection temperature in the 120 °C range under 0.46 MPa after full postcure; the 1.82 MPa value is lower and is the appropriate reference for load-bearing selection. The material is opaque, filled, and exhibits higher viscosity than unfilled acrylate or epoxy SLA resins. This characteristic affects recoat behaviour, resin temperature control, long-idle re-homogenization, and the need for machine-specific working curves. Fully postcured parts show higher tensile and flexural modulus, reduced elongation at break, and improved dimensional stability at elevated temperature compared with general-purpose unfilled SLA materials. The grade should be considered for parts where stiffness and moderate thermal resistance outweigh toughness and optical transparency. Representative property values, process limitations, and comparative differences are provided below.
Representative postcured property values are summarized in Table 1. These values are typical and assume complete UV and thermal postcure per the resin supplier’s schedule; individual batches and machine exposure conditions may shift the results by several percent.
| Property | Test method | Typical value |
|---|---|---|
| Liquid viscosity at 25 °C | ASTM D2196-20 | 1000–1500 mPa·s |
| Cured density | ASTM D792-20 | 1.15–1.18 g/cm³ |
| Tensile strength at break | ASTM D638-14 | 55–62 MPa |
| Tensile modulus | ASTM D638-14 | 3100–3400 MPa |
| Elongation at break | ASTM D638-14 | 2–3% |
| Flexural strength | ASTM D790-17 | 90–105 MPa |
| Flexural modulus | ASTM D790-17 | 2900–3200 MPa |
| Notched Izod impact | ASTM D256-10 | 14–18 J/m |
| Heat deflection temperature at 0.46 MPa | ASTM D648-18 | 115–120 °C |
| Heat deflection temperature at 1.82 MPa | ASTM D648-18 | 90–95 °C |
| Durometer hardness | ASTM D2240-15 | Shore D 87 |
In unfilled SLA resins, large elongation at break is achieved through segmental mobility between crosslinks. NanoForm 15120 restricts that mobility with a dispersed nanofiller phase and shifts the stress-strain response toward higher stiffness and lower strain. Tensile modulus values of 3100–3400 MPa and flexural modulus values of 2900–3200 MPa are typical in fully postcured specimens tested under ASTM D638-14 and ASTM D790-17. Elongation at break falls to roughly 2–3%, and notched Izod impact values under ASTM D256-10 are in the 14–18 J/m range, which is lower than tough unfilled SLA formulations. The reduction in ductility means that holes, sharp corners, and snap-fit features become crack-initiation sites more readily than in high-elongation SLA grades. The reinforcement also reduces creep at temperatures approaching the 0.46 MPa heat deflection threshold, but continuous load should be evaluated against the 1.82 MPa HDT of approximately 90–95 °C. The exact filler loading and surface treatment are not disclosed in the public technical data sheet; the term nanocomposite indicates a sub-micron dispersed solid phase rather than a fully homogeneous network. This phase composition improves modulus but can lower optical penetration and requires careful mechanical finishing with sharp carbide tooling.
Recoating a filled suspension is not equivalent to recoating a clear, unfilled resin. NanoForm 15120 has a liquid viscosity generally reported in the 1000–1500 mPa·s range at 25 °C, which is high enough to require longer recoater wait states and lower wiper speeds on large cross-sections. Production-scale solid-state laser systems have shown short-fill defects, entrapped air, and wavy surfaces when the vat is below approximately 22–25 °C; a vat temperature of 25–30 °C is a practical operating range for this resin class. After extended idle periods, filler settling can produce vertical segregation that changes optical penetration depth and working curve parameters. Operators should not carry over a standard transparent-resin window-pan exposure file; instead, the working curve should be regenerated for each vat fill on the target machine using the installed laser power and beam diameter. Nanofiller scattering reduces cure depth per unit exposure relative to clear resins, so the critical exposure and penetration depth values will differ from the platform’s default unfilled-resin dataset. The product is designed for 354.7 nm scanned-laser stereolithography and is not validated for masked-projection or DLP systems operating at 385–405 nm. Layer thickness for structural parts is commonly 0.100 mm; thinner 0.050 mm layers are possible but require exposure and recoat re-characterization. A typical failure mode on large-frame machines is delamination at the interface between a slowly scanned heavily exposed layer and a faster-scanned layer when the resin temperature drifts during the build.
Postcure is not optional and cannot be reduced to a UV-only exposure. A UV flood station completes near-surface polymerization, but the thermal stage is required to drive conversion of residual reactive groups and to relax internal stress. UV-only parts typically exhibit lower modulus, higher creep, and dimensional movement at temperatures well below the published HDT values. In process qualification, the oven load, air circulation, and local part thickness must be mapped with thermocouples because a loaded curing oven can show temperature variations large enough to alter the 1.82 MPa HDT by more than 3–5 °C. Thin unsupported features should be fixtured during thermal postcure to prevent slump deformation. For thick sections, heating and cooling ramps in this resin class are usually limited to prevent transient thermal gradient cracking; abrupt removal from the oven should be avoided. The manufacturer supplies UV dose and thermal time–temperature guidance, but published data for this specific configuration is limited, so each facility should verify property development with witness coupons rather than relying solely on machine or oven timers. Witness coupons should be built in the same orientation, thickness, and down-facing surface area as production parts because accumulated UV dose during the build influences final conversion.
The principal differences from other SLA resins are visible in modulus, elongation, HDT, and optical state. Compared with clear, unfilled engineering SLA resins such as the Somos Watershed class, NanoForm 15120 provides higher stiffness and higher thermal resistance but considerably lower elongation and no optical clarity. Compared with highly filled high-HDT SLA grades such as the Somos PerFORM class, NanoForm 15120 has lower modulus and lower HDT but is less brittle and less viscous, making it easier to recoat on some platforms. Table 2 summarizes representative values from manufacturer technical literature across these classes; values are typical, not direct specification equivalents.
| Property | Somos NanoForm 15120 | Unfilled high-elongation SLA (Watershed class) | Highly filled high-HDT SLA (PerFORM class) |
|---|---|---|---|
| Tensile modulus | 3100–3400 MPa | 2000–2400 MPa | 9000–10000 MPa |
| Elongation at break | 2–3% | 15–20% | Less than 1% |
| Notched Izod impact | 14–18 J/m | 30–45 J/m | 10–15 J/m |
| HDT at 0.46 MPa | 115–120 °C | 50–60 °C | Greater than 260 °C |
| HDT at 1.82 MPa | 90–95 °C | 45–55 °C | Greater than 250 °C |
| Optical state | Opaque | Transparent or translucent | Opaque |
Typical usage includes high-stiffness wind tunnel test articles, short-run injection mold inserts for low-pressure processes, thermally exposed fixtures, and electronic connector housings that require dimensional stability after postcure. For short-run mold inserts, cavity surface temperature should remain below the 1.82 MPa HDT of approximately 92 °C if injection loads impose sustained stress; short excursions toward the 0.46 MPa HDT may be acceptable only after process trials. In wind tunnel work, the higher modulus reduces deflection under aerodynamic load, but the low elongation makes the material susceptible to handling damage at mounting points; bonded or inserted metallic bushings are preferred over direct threaded assembly. The grade is not represented in public literature as a food-contact material under FDA 21 CFR 177 or as a long-term implantable medical material. Aggressive polar solvents, strong alkaline immersion baths, and concentrated amine-based strippers can attack the network and should be avoided. Compliance status under REACH Article 33 and RoHS Directive 2011/65/EU is supply-region dependent and must be verified against the current safety data sheet. Machining, drilling, and reaming should use sharp carbide tooling with moderate feed and air cooling to limit edge micro-cracking. Dimensional compensation factors for laser overcure, thermal postcure shrinkage, and batch-to-batch viscosity variation are higher than for transparent unfilled resins and must be established per machine, per batch, and per part-wall thickness.