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Как аккредитованный завод DSM Somos 7110 Epoxy Photopolymer, Green Parts, мы соблюдаем строгие протоколы качества - каждая партия подвергается строгим испытаниям для обеспечения последовательных стандартов эффективности и безопасности.
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In lost-resin investment casting of nickel-based superalloy turbocharger impellers and titanium aluminide turbine wheels, the green part printed from Somos 7110 epoxy photopolymer is employed as a sacrificial pattern around which ceramic shells are constructed. The resin is charged into the stereolithography vat at 100 wt% as-received basis; no reactive diluent, solvent, or filler is recommended by the material supplier, because dilution of the hybrid epoxy-acrylate network shifts green-part dimensional stability outside the ±0.15 mm tolerance band that aerospace foundries commonly apply under AS9100D clause 8.5.1 for production process control. The printing operation is conducted on 355 nm stereolithography equipment with galvanometer scanning, commonly a 3D Systems Viper si2 or equivalent platform, using 100 μm slice thickness, a vat temperature held at 28–32 °C, and a recoater blade speed that maintains resin film thickness without entrapping air. After the green part is removed from the build platform, it undergoes solvent washing, removal of support structures, and a two-stage post-cure: 60 min UV exposure followed by 2 h at 80 °C in a forced-air oven to drive conversion of residual oxirane groups and stabilize the part before shell coating. The ceramic shell is built by alternating slurry dipping and stuccoing for 7–8 coats, with each coat dried at 22–25 °C and 45–55 % relative humidity; the cured shell is then dewaxed in an autoclave and fired to 900–1,100 °C to combust the epoxy pattern. Ash content testing per ASTM D5630 is used to verify complete burnout, with residual ash below 0.02 wt% considered acceptable in aerospace foundry practice, though published data for this specific configuration of Somos 7110 is limited. The dominant process conflict occurs during thermal expansion of the green part between 20 °C and the epoxy glass transition temperature; uncontrolled heating above 2 °C/min below 300 °C causes shell cracking from pyrolysis gas pressure, so multi-step burnout ramps with holds at 150 °C, 300 °C, and 600 °C are employed on production lines. Terminal product types include Inconel 718 compressor wheels, titanium aluminide low-pressure turbine blades, and cobalt-chromium dental copings produced by vacuum casting into the fired shells.
| Property | Green part (as-printed) | Post-cured (UV + 80 °C, 2 h) | Test method |
|---|---|---|---|
| Tensile strength | Not typically measured due to incomplete network formation | 45–54 MPa | ASTM D638-14 |
| Flexural modulus | Lower than post-cured; published data limited | 2,400–2,600 MPa | ASTM D790-17 |
| Elongation at break | Higher than post-cured; published data limited | 12–16 % | ASTM D638-14 |
| Heat deflection temperature at 0.46 MPa | Below final HDT; published data limited | 58–68 °C | ISO 75-2:2013 |
| Viscosity at 30 °C | 300–400 cps in vat | Not applicable | ASTM D2196 or equivalent |
The use of Somos 7110 green parts as positives for RTV silicone tooling requires a master pattern with smooth vertical walls and no detectable build lines; the resin is used without formulation adjustment, and the printed geometry constitutes 100 % of the master pattern body, while the silicone itself is typically mixed at a base-to-catalyst ratio of 10:1 by weight, a parameter that does not involve the photopolymer but determines the mold’s tear resistance and dimensional recovery during successive casting cycles. Compliance for the tooling workflow is anchored to ASTM D412-16 for tensile properties of the vulcanized silicone and to ISO 9001 for traceability of the master pattern’s dimensional inspection report. The downstream process begins with SLA printing at 100 μm layer thickness, followed by support removal, isopropyl alcohol washing, and progressive sanding from 400 to 1,200 grit to reduce stair-step surface artifacts; a polyester filler may be applied to low spots, but the photopolymer itself is not compounded with any filler. The master is then mounted on a splitting plane and coated with a solvent-based mold release that is cured for 15–20 min at 25 °C before the silicone is poured under vacuum at -0.98 bar to eliminate entrapped air bubbles from high-aspect-ratio cavities. A practical failure mode observed in tooling shops is silicone inhibition caused by residual uncured acrylate or photoinitiator migrating from the master surface; therefore some processors extend the post-cure step by 30 min beyond the standard protocol and wipe the surface with ethanol before release application, though published data for this specific configuration is limited. Terminal product types from this route include polyurethane instrument housings, short-run elastomeric gaskets, and functional prototypes for consumer electronics that require Shore A 40–70 rubber-like parts produced in silicone molds.
For wind tunnel test articles requiring dimensional conformity to ISO 1101:2017 and surface roughness values below Ra 0.8 μm per ISO 4288:1996, Somos 7110 green parts are printed, post-cured, and hand-finished into scale models of airfoil sections, wing-body fairings, and motorsport aerodynamic devices. No resin-side addition is made; the photopolymer is processed at 100 % as-supplied solids, and internal lattice drainage holes are designed into the STL build preparation to remove uncured resin from hollow sections, because trapped liquid resin can exude during post-cure and cause surface defects that compromise laminar flow testing. The stereolithography build uses 50 μm or 100 μm layers depending on surface curvature, with the finer layer setting reserved for leading-edge radii below 5 mm to minimize chordwise stair-stepping. After support removal and washing, the model is sanded with progressively finer abrasives, filled with a two-part epoxy putty at the support attachment points, and primed with a high-solids polyurethane primer before final wet sanding; the primer layer adds 15–25 μm to the surface, which is compensated in the CAD offset. The post-cured Somos 7110 model exhibits a flexural modulus in the range of 2,400–2,600 MPa per ASTM D790-17, sufficient to resist bending deformation under wind loads up to 120 m/s in subsonic tunnels, but published data for this specific aerodynamic configuration is limited. Terminal product types include 1:50 scale aircraft models, full-scale motorcycle fairing sections, and UAV airframe components evaluated for drag coefficient and flow separation behavior.
Clinically, when hospital-based additive manufacturing labs and contract device design firms convert CT or MRI data into surgical planning aids under ISO 13485:2016, the single-component Somos 7110 resin is not blended; each manufacturing batch is used at 100 wt% as-supplied, and residual monomer content is minimized through the standard UV post-cure plus a forced-air thermal cure at 80 °C for 2 h, which also raises the heat deflection temperature to 58–68 °C per ISO 75-2:2013 so that models withstand brief exposure to steam autoclave conditions during indirect handling. The downstream production sequence involves segmentation of CT or MRI DICOM data, conversion to a closed STL mesh, printing at 100 μm layers, solvent washing to remove uncured resin from trabecular-like internal structures, and UV post-cure for 60 min. Models intended for ethylene oxide sterilization are processed with the same resin but packaged in gas-permeable pouches; the effect of ethylene oxide on cured epoxy photopolymer mechanical properties has not been extensively published, so procedural validation under FDA 21 CFR Part 820 design controls is required before clinical use. Terminal product types include mandibular reconstruction planning models, orbital floor fracture guides, and dental implant placement templates used in a pre-operative setting, not as long-term implantable devices.
Design verification of glass-filled nylon intake manifolds and air cleaner housings uses Somos 7110 green parts to check mounting boss torque retention, seal groove geometry, and hose barb interference before tool steel is cut. The resin is processed at its supplied composition; no plasticizer, flexibilizer, or flame-retardant package is added, because the application requires dimensional stability during torque testing at 8–12 N·m on M6 brass inserts. Compliance testing follows IATF 16949:2016 for automotive production part approval, with mechanical property verification per ASTM D638-14 for tensile strength and ISO 75-2:2013 for heat deflection temperature under 0.46 MPa flexural load. The build is executed on a 355 nm laser SLA system at 100 μm layer thickness, with the vat temperature controlled to ±1 °C to keep resin viscosity within 300–400 cps and ensure consistent recoating over large flat sections. After post-cure, the prototype manifold is assembled with production gaskets and clamps, then subjected to a thermal soak at 60 °C for 4 h to screen for creep under clamping pressure; if relaxation exceeds the design tolerance, the post-cure schedule is extended in 30 min increments, although published data for this specific configuration is limited. Terminal product types include intake manifold prototypes for 1.5–2.0 L turbocharged engines, air cleaner housing covers, and HVAC duct adapters evaluated on vehicle-level test mules.
Because handheld device prototypes must reproduce snap-fit latch geometry with wall thicknesses from 1.0 mm to 2.5 mm, Somos 7110 green parts are built at 50 μm layers to capture fine latch geometry and then post-cured to stabilize the epoxy network before assembly trials. The unfilled resin is used at 100 % as-supplied; no flame-retardant additive is introduced, so the material’s UL 94 classification per IEC 60695-11-10 is not assumed, and the finished prototype is considered a non-production-representative housing for thermal and flammability testing purposes. The downstream process includes support removal from blind snap features, isopropyl alcohol washing, UV post-cure for 60 min, thermal cure at 80 °C for 2 h, and light sanding on parting lines before trial assembly with molded polycarbonate inserts. Electrical continuity testing of EMI shield spring contacts is performed on the resin housing to evaluate contact force retention; because the post-cured epoxy exhibits a flexural modulus of 2,400–2,600 MPa per ASTM D790-17, it provides sufficient stiffness for this purpose at room temperature, but published data for elevated-humidity conditions above 85 % RH is limited. Terminal product types include smart meter faceplates, IoT sensor node housings, and USB-C connector bodies used in engineering fit-check evaluations.
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DSM Somos 7110 Epoxy Photopolymer, Green Parts is a cationically cured epoxy resin for vat photopolymerization. The descriptor “green parts” refers to the as-built, pre-post-cure condition in which the laser-exposed resin has undergone gelation but has not reached full epoxide conversion. The material is not a filled or composite resin and does not derive its primary identity from a separate green colorant package; any visible green tint in the uncured or partially cured state should be verified against the current supplier lot documentation. The chemistry is supplied under the legacy DSM Somos trade designation and is currently addressed through Covestro’s additive manufacturing resin portfolio following the 2021 asset transfer. Procurement specifications should reference the current safety data sheet, technical data sheet, and lot-specific certificate of analysis for epoxide equivalent weight, photoinitiator concentration, and viscosity before production runs.
The resin is intended for 355 nm solid-state laser stereolithography equipment using a scanning galvanometer system and a recoating blade. Build platforms with resin temperature maintained at 28 °C–32 °C permit stable recoat dynamics without requiring aggressive heating. In this operating window the liquid viscosity is low enough to allow drainage from thin walls and reflow into recoated layers, while high enough to maintain a uniform layer thickness between passes. The material is compatible with standard vat-photopolymerization post-processing sequences: solvent wash, support removal, and UV post-cure. However, the green-state part is not a final-use article; it retains unreacted epoxide groups and must be handled as a chemically active intermediate until post-cure is complete.
The differentiating mechanism of Somos 7110 lies in acid-catalyzed ring-opening polymerization. In contrast to multifunctional acrylate or methacrylate resins that cure by free-radical chain addition and are inhibited by atmospheric oxygen at the surface, the epoxide groups in Somos 7110 continue to react after the laser has moved to the next layer. The photo-acid generator releases a Brønsted acid upon exposure to the 355 nm laser; the acid initiates epoxide ring opening and propagates through cationic species that are not terminated by oxygen. This permits dark-cure conversion to proceed for minutes to hours after build completion. The consequence is that green-state dimensions and green-state hardness are not fixed at the moment of removal from the vat. Build trials should therefore record time-to-solvent-wash and temperature during this interval, because dimensional drift and embrittlement can occur if the part is left in a warm environment with residual surface resin. Unlike acrylate systems that show surface tack due to oxygen inhibition, Somos 7110 surfaces generally cure without a sticky inhibition layer, provided the laser dose and photo-acid generator concentration remain within the supplier’s specified envelope.
Because epoxy polymerization involves ring opening, the volumetric shrinkage on cure is lower than that of many radical acrylate resins. Published shrinkage values for this specific formulation are limited; comparative epoxy systems typically report linear shrinkage below 0.5% after offset compensation, while unoptimized radical acrylate formulations may exceed 1.0%. These values are not universal and must be established by measuring a calibrated reference coupon on the target machine. The low shrinkage and comparatively low moisture expansion of cured epoxy networks support use in tooling or master patterns where dimensional fidelity is more important than ultimate toughness.
During removal of the build platform, the green parts remain attached to supports and contain unpolymerized resin within internal cavities and surface films. Cleaning is typically performed in a two-stage solvent bath. Tripropylene glycol monomethyl ether (TPM) is the primary wash solvent for many epoxy SLA resins; isopropanol may be used for short contact times, but prolonged immersion can induce solvent uptake into the partially cured network and should be controlled. Aggressive ketone, chlorinated, or aromatic solvents are not recommended because they can soften the green part and release residual photo-acid generator. After solvent washing, compressed air drying at pressures below 30 psi removes residual solvent from fine features; heated drying above 40 °C before UV post-cure should be avoided unless specified by the manufacturer, because it may prematurely advance thermal crosslinking and distort unsupported geometry. Supports are removed before final post-cure when possible, because green-state removal produces less chipping than post-cured removal in small-batch trials. However, thin-walled sections may require support retention during post-cure to prevent creep deformation.
Post-cure is carried out in a UV chamber with UV-A output between 350 nm and 405 nm, typically delivering 30 J/cm²–60 J/cm² total energy to each surface, followed by thermal post-cure at 60 °C–80 °C for 1–2 h when the supplier’s cure schedule specifies it. The exact dose is a function of part wall thickness, optical density, and whether a rotating fixture is used inside the chamber. Under-curing leaves residual epoxide groups that can react during service with humidity or amines; overcuring can increase crosslink density to the point of reduced elongation and increased notch sensitivity. Equipment without controlled intensity feedback should be validated with a calibrated radiometer at the part plane before production batches.
Mechanical performance depends strongly on build orientation, layer thickness, post-cure schedule, and test condition. The values in the following table are representative ranges collected from supplier technical literature for post-cured test specimens; they are not a certificate of analysis and must not be used for design allowables without lot-specific testing. All specimens were tested according to the cited ASTM methods after conditioning at 23 °C and 50% relative humidity for at least 24 h unless otherwise noted. Green-state mechanical properties are typically 30%–50% of post-cured values for similar epoxy SLA systems, but published green-state data for this specific formulation is limited and should be confirmed on the target machine.
| Property | Test standard | Reported range |
|---|---|---|
| Liquid viscosity at 30 °C | ASTM D2196 rotational rheometer | 250–350 mPa·s |
| Cured part density | ASTM D792 | 1.15–1.18 g/cm³ |
| Tensile strength | ASTM D638 | 45–55 MPa |
| Tensile modulus | ASTM D638 | 2,400–2,900 MPa |
| Elongation at break | ASTM D638 | 5%–10% |
| Flexural strength | ASTM D790 | 65–75 MPa |
| Flexural modulus | ASTM D790 | 2,200–2,700 MPa |
| Notched Izod impact | ASTM D256 | 20–30 J/m |
| Hardness | ASTM D2240 | 82–87 Shore D |
| Heat deflection temperature at 0.46 MPa | ASTM D648 | 55–65 °C |
| Glass transition temperature | ASTM D3418 differential scanning calorimetry | 55–65 °C |
The table reveals the material’s position within the epoxy SLA resin class: it is stiff and relatively hard but not an impact-grade engineering polymer. The notched Izod range of 20–30 J/m places it below many thermoplastic polyolefins and nylons, so any application involving snap fits, repeated bending, or high-rate loading should be prototyped under service conditions before commitment. The heat deflection temperature range of 55–65 °C means that functional parts should not be exposed to sustained temperatures above 50 °C without mechanical shielding or geometry-specific derating. Moisture conditioning can shift the glass transition temperature downward by several degrees; this is a known behavior of epoxy networks and should be included in design validation when parts are intended for humid environments.
The cured epoxy network of Somos 7110 exhibits better barrier and solvent-resistance behavior than many unfilled acrylate SLA resins because the crosslinked epoxy network contains no residual unsaturated carbon-carbon backbone from acrylate polymerization. In service, short-term contact with aliphatic hydrocarbons, mineral oils, and dilute aqueous solutions can be tolerated, but concentrated acids, oxidizing agents, and polar aprotic solvents such as N-methyl-2-pyrrolidone can attack the network. No universal chemical-resistance rating can be assigned without specifying the test fluid, temperature, exposure duration, and stress state. For applications requiring immersion or continuous chemical exposure, resistance should be confirmed using ASTM D543 immersion coupons or ISO 2812-1:2017 equivalents. The material is not marketed as a sterilization-grade or implantable resin; any medical application must be supported by end-user ISO 10993-1 biological evaluation rather than supplier literature alone.
Compared with high-speed digital light processing (DLP) photopolymers formulated for 385 nm or 405 nm LED exposure, Somos 7110 is matched to a 355 nm solid-state laser. This wavelength selectivity means that cure depth and critical exposure are tuned to a narrow emission line; using the material in a non-approved broadband LED system without spectral filtering can produce inconsistent gelation and poor interlayer adhesion. Compared with water-clear epoxy SLA resins, Somos 7110 does not prioritize optical clarity; surface haze or green-state tint may be present and should not be interpreted as product degradation unless the supplier’s QC specification states otherwise. Compared with high-temperature SLA resins in the same family, the heat deflection temperature is moderate, which favors room-temperature dimensional stability without requiring aggressive thermal post-cure. Users who require a heat deflection temperature above 100 °C should evaluate other resin chemistries rather than over-curing Somos 7110, because excessive post-cure may raise crosslink density but introduce internal stress and brittle failure.
Green-part handling is most stable in a controlled environment. When relative humidity exceeds 60%, the partially cured epoxy network absorbs atmospheric moisture from the vat room and during storage. This uptake can plasticize the green part, increase cleaning solvent retention, and reduce the glass transition temperature of the final post-cured article. Production environments above this threshold should include a dry-air storage cabinet for green parts and a pre-drying step of 40 °C–50 °C for 2–4 h before UV post-cure. The liquid resin should be protected from contamination by amine-based materials, strong Lewis bases, and sulfur-containing compounds; these species can deactivate the photo-acid generator or prematurely crosslink residual epoxide groups in the vat. Batch-to-batch variance in photo-acid generator concentration is controlled by the supplier, but mixing old and new resin without recording the epoxide equivalent weight can shift the working curve. Recoat failures such as dewetting, orange peel, or layer tearing are often caused by insufficient resin temperature, degraded recoating blade edges, or contamination with secondary photopolymers. The equipment should have temperature control within ±2 °C of the validated setpoint, and the recoating blade should be replaced according to the machine manufacturer’s maintenance interval to avoid transient viscosity gradients across the build area.
The material is not approved for food-contact use unless the end-user completes compliance testing under FDA 21 CFR 175.300 or equivalent migration testing, because residual epoxide groups and photo-acid generator by-products can migrate from incompletely cured surfaces. REACH and RoHS status must be confirmed through the current supplier safety data sheet; changes in formulation stewardship for a legacy product can affect the stated registration status. The green-state surface should be treated as an incompletely reacted chemical intermediate and disposed of according to local regulations for uncured epoxy resin. Users must verify lot-specific behavior with current supplier documentation and their own production equipment rather than relying solely on representative property ranges.