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3D Systems RenShape SL 7820 Stereolithography Plastic

    • Название продукта: 3D Systems RenShape SL 7820 Stereolithography Plastic
    • Сайт Factroy: Округ Юду, Ганьчжоу, Цзянси, Китай
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    • Производитель: Ascent Petrochem Holdings Co., Limited
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    Код ТН ВЭД 816764

    Как аккредитованный завод 3D Systems RenShape SL 7820 Stereolithography Plastic, мы соблюдаем строгие протоколы качества - каждая партия подвергается строгим испытаниям для обеспечения последовательных стандартов эффективности и безопасности.

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    Применение 3D систем RenShape SL 7820 Стереолитография Пластик

    For polyurethane vacuum casting programmes where a short-run product launch depends on a dimensionally stable master, SL 7820 is introduced into the stereolithography vat undiluted; the resin is not compounded with reactive diluents, thixotropes, or inorganic fillers, and the working addition ratio is therefore 100% of the photopolymer as supplied, with fresh resin top-up limited to ≤20 vol% of the remaining vat volume per shift to control viscosity drift and cationic polymerisation by-product accumulation during continuous recoating. Layers are polymerized at 50 µm or 100 µm slice thickness depending on the component envelope; after drained build, the green master is washed with tripropylene glycol monomethyl ether or isopropanol, then exposed in a UV post-cure chamber calibrated to a total energy of 10–20 J/cm² per surface. The cured master is wet-sanded and coated with a solvent-borne polyurethane sealer applied at a dry film thickness of 5–10 µm before platinum-catalysed RTV silicone is poured. Dimensional verification is conducted against ISO 2768-1:1989 linear and angular general tolerances, and silicone Shore A hardness is recorded under ISO 868:2003. Machined reference tabs from the same vat are tensile-tested to ASTM D638-14 and flexural-tested to ASTM D790-17; heat deflection temperature is evaluated under ASTM D648-18. A recurring production-line failure mode is post-cure warpage when high-aspect-ratio drain channels retain solvent; drain apertures smaller than 2 mm have produced delayed release film formation and scrap during first silicone cure. The terminal outputs in this scenario are cast rigid and elastomeric polyurethane components used as automotive interior trim prototypes, functional snap-fit covers, and low-volume consumer equipment housings produced in 10–50-shot silicone mould campaigns.

    Does SL 7820 Burn Out Cleanly Enough for Shell Investment Casting?

    Because SL 7820 is a cationically polymerized thermoset, it does not melt during autoclave wax removal; instead, the pattern decomposes by thermal fragmentation and oxidative carbon burnout. Investment casting foundries using this material as a sacrificial pattern must therefore design the build with drain and vent apertures of at least 2 mm diameter and shell wall thickness of 0.5–1.0 mm around the QuickCast lattice; the resin itself remains undiluted at 100% vat concentration, and the lattice density is set by the SLA build style software rather than by post-build compounding. After printing, uncured resin is drained for 12–24 h and the pattern is solvent-washed before the ceramic shell is applied. Burnout profiles are to be established by differential scanning calorimetry under ASTM D3418-21 and thermogravimetric analysis under ISO 11358-1:2022; these methods quantify the decomposition onset and residual mass that determine whether a foundry-specific ramp can avoid shell cracking. In production, the shell is typically preheated to 150–180 °C, ramped at 1–2 °C/min to 350 °C, and held at 650–750 °C until carbon residue is below the foundry's acceptance criterion; however, published data for SL 7820-specific ash residue in this configuration is limited and must be verified on the specific shell system. Compliance is maintained under ISO 9001:2015 clause 8.5.1 for production process control and, where aerospace castings are involved, under AS9100 D clause 8.5.1.1. Terminal components are shell investment-cast aluminum, stainless steel, and cobalt-chrome parts for pump housings, turbine wheels, and structural brackets.

    If a low-temperature composite tool is required for a prepreg system that cures below 70 °C, SL 7820 can be used as a dimensionally stable printed tool substrate if thermal gradients and room-temperature storage are controlled. The tool is built at 100 µm layer thickness from the undiluted resin; no additive is introduced into the vat, and the addition ratio is 0% for the photopolymer itself, while the release system is applied as a two-step semi-permanent sealer and release coat at a combined film mass of 0.1–0.3 g/m². After post-cure, the tool face is coated with an epoxy gel coat, sanded to Ra ≤1.6 µm, and checked for flatness against ASTM D5687/D5687M-20 composite panel preparation guidelines; the tool is then used in vacuum-bag-only layup cycles capped at 65 °C because the HDT of SL 7820 is below the threshold for high-temperature autoclave curing. The downstream process involves manual or automated fibre placement of carbon/epoxy prepreg into the printed tool, followed by vacuum debulk at 0.85–0.95 bar and cure at 50–65 °C for the resin system's specified cycle. Composite shop floor data indicate that tool surface temperature must be monitored with contact thermocouples at the laminate-tool interface, because radiation-cured SLA substrates can exhibit thickness-dependent thermal lag that shifts exotherm readings. Terminal products include carbon fibre-reinforced epoxy panels, UAV airframe fairings, and low-temperature composite ducts.

    Assembly Fixture Datum Surfaces and Thermal Drift Control in SL 7820 Production Support Tooling

    Tier-1 automotive and aerospace assembly lines using SL 7820 for coordinate-measuring-machine fixture bodies and go/no-go gauges typically specify post-cure at 40–60 °C for 1–2 h, followed by datum surface machining because the green-state substrate is not sufficiently stable for ±0.25 mm datum hole patterns under continuous handling. The resin is used as a 100% vat feedstock; no release agent, plasticizer, or filler is added to the photopolymer. Where multi-piece fixture plates are bonded, a structural methacrylate adhesive is applied at a bond line of 0.1–0.2 mm, and heat-set brass inserts are installed with engagement depth not less than the nominal screw diameter. Compliance for the measurement environment is verified under ISO 10360-2:2009 for CMM length measurement performance, and the production support tooling is documented under IATF 16949:2016 clause 7.1.5.1 where the customer's quality system requires traceable gauge R&R. The downstream process is fixture assembly, datum verification, and periodic recalibration at 20–23 °C; the polyurethane or stainless steel locating pins are inserted after reaming to H7 tolerance. Finished products in this application are dedicated assembly fixtures, CMM holding nests, and handheld drill templates used in Tier-1 interior and structural assembly cells.

    Electronics development groups requiring non-metallic housings for functional testing use SL 7820 as a rigid thermoset substitute for injection-moulded ABS or polycarbonate, provided that the prototype is not positioned as a UL-recognised production enclosure without additional testing. The photopolymer is printed undiluted at 100% vat concentration; for trial builds, no flame retardant or glass reinforcement is compounded into the resin. If an electromagnetic shielding layer is required, an acrylic conductive copper or nickel coating is applied over the post-cured surface at a dry film thickness of 10–25 µm, which corresponds to a wet-film addition of approximately 20–50 µm after adjusting for spray transfer efficiency. The build process uses 50 µm layers, solvent washing, and UV post-cure; threaded holes are then machined or fitted with heat-set brass inserts under a soldering iron set to 180–220 °C to avoid local surface degradation. Material compliance documentation for European downstream trials is evaluated against RoHS Directive 2011/65/EU Annex II and REACH Regulation EC 1907/2006 Annex XVII; however, UL 94 flammability classification is not automatically transferred from the liquid resin to a printed wall section and must be tested on the finished geometry. Terminal products are prototype switch panels, sensor enclosures, connector fit-check housings, and short-run test fixtures that are not intended for continuous high-current service.

    Low-Speed Aerodynamic Test Models Require Filled Surface and Balance Insert Precision

    Low-speed aerodynamic test programmes require rigid models with stable planform geometry and precise balance-insert alignment; SL 7820 is used for wind tunnel articles when the test-section stagnation temperature remains below 50 °C. The resin is processed at 100% vat concentration without thinning; after the hollow model is built, internal cavities are drained through 2 mm drain holes and the exterior is coated with an epoxy-based model filler at a dry film thickness of 20–40 µm to close stair-step surfaces. The filler addition ratio on the surface is controlled by mass, not by resin formulation; no internal filler is added to the photopolymer. The model is post-cured, wet-sanded to Ra ≤1.6 µm, and then painted with a polyurethane topcoat of 15–25 µm dry film thickness. Dimensional inspection for model symmetry and planform area is performed according to ISO 9001:2015 clause 8.5.1 and, where relevant, the test facility's own AS9100 D process control requirements; the metallic balance mounting interface is machined from an aluminum insert bonded with a structural epoxy adhesive at 0.1 mm bond line. The downstream process includes balance calibration, wind tunnel installation, and aerodynamic data collection at Mach numbers below 0.3. Terminal products are low-speed aerodynamic test articles, surface pressure models, and flow visualisation bodies used in subsonic tunnel campaigns.

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    Более подробное введение

    3D Systems RenShape SL 7820 is an unfilled liquid photopolymer formulated for vat photopolymerization on 355 nm stereolithography systems, including the SLA-7000, Viper Pro, iPro 8000, and ProX 800 platforms. The resin produces opaque, off-white parts with ABS-like mechanical response and is specified for functional snap-fit enclosures, jigs, fixtures, investment casting patterns, and master patterns that require dimensional stability after solvent cleaning and UV post-cure. Processing is performed with vat temperatures maintained at 28–32 °C and layer thicknesses typically between 0.050 mm and 0.100 mm. The uncured resin has a dynamic viscosity near 330–400 mPa·s at 30 °C, which requires controlled recoat blade speed and stable vat heating on large-area builds. Because stereolithography resins retain unreacted acrylate and epoxy groups in the green state, mechanical values are not realized until the part receives sufficient post-cure UV fluence; incomplete post-cure produces creep under load, reduced heat deflection temperature, and solvent susceptibility.

    What Published Mechanical and Thermal Values Govern Design Allowables?

    Representative cured-state values from publicly available supplier literature are compiled in Table 1. These values should not be treated as guaranteed minimums. Stereolithography specimens are anisotropic, and the reported results depend on build orientation, layer thickness, laser energy dose, and post-cure duration. Test specimens prepared in the x-y plane at 0.100 mm layering typically exhibit higher tensile elongation than z-axis specimens because the interlayer boundary creates a preferential failure path when the part is loaded normal to the build plane.

    Representative published properties of RenShape SL 7820 after UV post-cure
    PropertyTest methodPublished typical value
    Liquid density at 25 °CASTM D792-131.12 g/cm³
    Solid densityISO 1183-1:20191.18 g/cm³
    Tensile strength at yieldASTM D638-1448 MPa
    Tensile modulusISO 527-2:20122.7 GPa
    Elongation at breakASTM D638-148.0%
    Flexural strengthASTM D790-1774 MPa
    Flexural modulusISO 178:20192.5 GPa
    Notched Izod impactASTM D256-1030 J/m
    HardnessASTM D2240-1584 Shore D
    Heat deflection temperature at 0.46 MPaASTM D648-1858 °C
    Heat deflection temperature at 1.82 MPaASTM D648-1853 °C

    The difference between liquid density at 1.12 g/cm³ and solid density at 1.18 g/cm³ corresponds to volumetric contraction during photopolymerization and contributes to internal stress accumulation when parts are under-cured or built with excessive section thickness. The heat deflection temperature at 0.46 MPa of 58 °C is a short-term thermomechanical ranking, not a continuous service ceiling. Under sustained load, the thermoset network exhibits creep and stress relaxation; design allowables should therefore be reduced when the service environment exceeds 40 °C for load-bearing features. The notched Izod result of 30 J/m under ASTM D256-10 is sensitive to notch radius, moisture conditioning, and post-cure time. Published data for this specific configuration is limited when the build is interrupted and resumed after vat cooling; users should prepare witness coupons on each build plate to capture lot and orientation effects.

    Production-scale stereolithography with SL 7820 on dual-laser platforms requires the vat resin to remain within 28–32 °C. At temperatures below 28 °C, recoat quality degrades because viscosity rises and the recoat blade drags or entrains air. On a 0.100 mm layer thickness build, scan path overlap and laser drawing line width should be verified after approximately 200 build hours. Large cross-section parts require longer recoat times; if recoat time falls below the resin leveling threshold, blade marks and interlayer delamination appear. Resin stored below 20 °C should be allowed to equilibrate before starting a build, and partially polymerized gel particles must be filtered from the vat because they increase local viscosity and can create hot spots on the optical window.

    When Snap-Fit and Living-Hinge Geometries Demand Ductility

    The tensile elongation of 8.0% and notched Izod impact of 30 J/m position SL 7820 as a candidate for cantilever snap-fit features in low-cycle assembly. For snap-fit design, the allowable outer-fiber strain must be set below the published elongation at break. A conservative design limit of 4.0% outer-fiber strain is recommended for repeated assembly, and 6.0% for single-event assembly. These limits derive from stress-strain data generated under ASTM D638-14 in the build plane. Snap-fit features built along the z-axis should be derated by approximately 1 percentage point because the interlayer boundary acts as a crack initiation plane under bending. Wall thickness below 1.0 mm is feasible in vertical orientation but requires support tuning to avoid post-removal pitting at the snap-fit root.

    Living-hinge geometries are constrained by the resin’s heat deflection temperature and low-cycle fatigue behavior rather than by monotonic elongation alone. Published data for living-hinge endurance in SL 7820 is limited. Post-cure annealing near 50 °C for 1 hour can improve hinge recovery, but excessive UV fluence or thermal exposure increases brittleness and reduces elongation at break. For applications requiring repeated hinge deflection above 5,000 cycles, a polypropylene-like stereolithography resin with higher elongation is generally specified, while SL 7820 is reserved for hinges requiring only occasional assembly. The material should not be used in continuous service above 50 °C for load-bearing snap features because the onset of thermal softening reduces retention force.

    Uncured resin should be stored between 20 °C and 30 °C in opaque containers because UV and blue-light exposure initiate premature polymerization. Resin from different lots should not be mixed without recording batch numbers and verifying viscosity at 30 °C remains below 400 mPa·s. If mixing is unavoidable, the resulting blend should be conditioned in the vat for at least 30 minutes before the build begins to eliminate temperature gradients. These controls reduce batch-to-batch variation in snap-fit retention force and outer-fiber strain capacity.

    Solvent Contact, Moisture Uptake, and Post-Process Machining

    Green SL 7820 parts should be cleaned with tripropylene glycol monomethyl ether or 99% isopropanol. Prolonged immersion beyond 20 minutes can soften the surface, propagate microcracks at layer boundaries, and reduce the flexural modulus by disrupting the partially cured network. Compressed air drying after solvent cleaning is not sufficient; parts should be allowed to dry at 23 °C and 50% relative humidity before dimensional inspection. Moisture uptake is measurable in thin walls below 1.0 mm if parts are stored in humid environments, and this moisture can affect electrical testing of conformal coatings. The cleaning protocol is governed by the solvent supplier’s flash point and local ventilation requirements; no universal ISO cleaning cycle applies across all stereolithography service bureaus.

    Post-cure is performed in a UV chamber with controlled irradiance. Insufficient post-cure leaves residual monomer that migrates to the surface and reduces surface hardness, while excessive post-cure can cause yellowing and embrittlement. For complex geometry, the UV dose should be applied in staged increments to avoid thermal warpage from exothermic cure. Parts should be supported during post-cure if wall thickness is below 1.5 mm, because unrestrained thin sections can curl under residual stress. After post-cure, SL 7820 can be machined, sanded, tapped, and painted. Conventional machining feeds and speeds for rigid thermoplastics apply, but test pieces should be cool after machining because frictional heat near the HDT can produce local softening and smearing.

    Differences from Accura 25 and Accura 60 Must Be Evaluated by Tensile Modulus, Not Solely by Color

    RenShape SL 7820 occupies an intermediate stiffness range between Accura 25 and Accura 60. Accura 25, a polypropylene-like resin, typically exhibits lower tensile modulus near 1.5 GPa and higher elongation above 13%, making it better suited for impact-absorbing clips and living hinges. Accura 60, a clear polycarbonate-like resin, typically exhibits tensile strength above 58 MPa and higher optical transparency, but lower notched Izod impact than SL 7820 in some orientations. The selection of SL 7820 is therefore justified when the application requires a balance of stiffness, impact resistance, and opaque surface finish while the continuous service temperature remains below 50 °C.

    Compared with high-temperature stereolithography resins such as Accura 48HTR, SL 7820 cannot be used for under-hood temperature exposure. The heat deflection temperature at 1.82 MPa of 53 °C is below the typical engine-bay component requirement, whereas high-temperature resins are formulated for short-term exposure above 100 °C. For chemical-resistant tooling masters, SL 7820 should be sealed with a chemically resistant coating if the master will contact aggressive release agents or amine-based epoxies. Unreacted surface species can interfere with platinum-cure silicone molding; a post-cure bake and barrier coat are required to prevent cure inhibition at the pattern surface.

    For regulatory documentation, the uncured resin is supplied with safety data sheets and should be assessed under CLP Regulation (EC) No 1272/2008. The cured polymer is not automatically food-contact compliant under FDA 21 CFR 177; a barrier coating is required if the end-use part contacts food or skin for extended periods. No claim of biocompatibility under ISO 10993-1 is made for direct wound contact. These operational boundaries are part of the material selection review when SL 7820 is compared with alternative stereolithography resins in regulated production programs.

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