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3D Systems VisiJet RCL-EBK-D70 Multi-Material Composites (VisiJet CR-CL 200** + VisiJet CE-BK)

    • Product Name: 3D Systems VisiJet RCL-EBK-D70 Multi-Material Composites (VisiJet CR-CL 200** + VisiJet CE-BK)
    • Factroy Site: Yudu County, Ganzhou, Jiangxi, China
    • Price Inquiry: admin@ascent-chem.com
    • Manufacturer: Ascent Petrochem Holdings Co., Limited
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    Specifications
    HS Code 954744
    Productname 3D Systems VisiJet RCL-EBK-D70 Multi-Material Composites (VisiJet CR-CL 200 + VisiJet CE-BK)
    Materialtype Multi-Material Composite
    Tensilestrength 35 MPa
    Tensilemodulus 1200 MPa
    Elongationatbreak 30%
    Flexuralstrength 45 MPa
    Flexuralmodulus 1100 MPa
    Hardness 70 Shore D
    Izodimpactnotched 80 J/m
    Heatdeflectiontemperature 50 °C
    Density 1.12 g/cm³
    Waterabsorption 0.5%
    Color Black
    Layerthickness 0.004 in (0.1016 mm)

    As an accredited 3D Systems VisiJet RCL-EBK-D70 Multi-Material Composites (VisiJet CR-CL 200** + VisiJet CE-BK) factory, we enforce strict quality protocols—every batch undergoes rigorous testing to ensure consistent efficacy and safety standards.

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    Application of 3D Systems VisiJet RCL-EBK-D70 Multi-Material Composites (VisiJet CR-CL 200** + VisiJet CE-BK)

    Within the VisiJet RCL-EBK-D70 multi-material composite build sequence, the rigid clear VisiJet CR-CL 200 matrix and black VisiJet CE-BK grip zones are deposited on a ProJet MJP 2500 Plus platform using independent piezoelectric inkjet channels and 32 µm layer thickness. The RCL-EBK-D70 designation carries a target digital hardness of Shore D 70; actual surface hardness is verified on co-printed plaques with ISO 868:2003 after 48 h at 23 °C ± 2 °C. The build envelope of 294 × 211 × 144 mm constrains batch orientation of multi-handle housings; the elastomeric grip plane is orientated away from the planarizer contact face to reduce wax entrapment at the rigid-to-elastomer transition. After build completion, sacrificial wax support is removed in a convection oven below 65 °C, followed by ambient stabilization at 50 % ± 5 % RH for 24 h. The modulus mismatch between the two phases is documented from co-printed tensile coupons conforming to ISO 527-2:2012; interfacial fracture must not occur before bulk elastomer tear, otherwise the mechanical interlock channel width is increased from 0.8 mm to 1.2 mm. Production inspection of similar dual-material hand tools repeatedly shows edge whitening in the clear phase after contact with ester-based cleaners; chemical immersion testing is therefore conducted according to ASTM D543-20 before release. The final handheld assembly retains a rigid transparent optical alignment housing and a black elastomeric grip formed without adhesive or post-mould overmoulding.

    Fluidic Manifold with Integral Black Compression Seal

    Leak-tightness in reagent delivery manifolds with clear fluid paths and black elastomeric sealing rings depends on the compression set of CE-BK after Luer engagement and on the dimensional stability of the CR-CL 200 channel after wax removal. Seal grooves are printed with a nominal elastomer height of 1.2 mm and assembled with axial compression of 12 % ± 2 %; compression below 10 % produces weeping at the Luer taper, while compression above 15 % can split the seal along the z-plane lamination boundary. Pressure-decay testing uses a transducer resolution of ±0.5 kPa and a hold pressure of 100 kPa for 30 min; records are maintained under ISO 13485:2016 clause 7.5.1. The clear phase requires visual verification of entrapped air or dye migration, with haze measured according to ASTM D1003-21 on polished coupons. Because the black elastomer contains pigment fillers, the manifold is flushed after post-cure with deionised water having resistivity not less than 18 MΩ·cm prior to installation in analytical instruments. The simultaneous jetting of both feedstocks eliminates adhesive bonding but introduces the requirement for a post-cure at 40 °C for 4 h to reduce surface tack before assembly.

    Process parameterStandard / methodBoundary condition for the two-phase part
    Interface tensile strengthISO 527-2:2012Co-printed coupon crosshead speed 1 mm/min; bond-line strength must exceed 80 % of CE-BK bulk tear strength measured under ASTM D624-00(2020)
    Surface hardnessISO 868:2003Measured on co-printed plaques after 48 h at 23 °C ± 2 °C; orientation and planarizer contact alter surface texture and indent geometry
    CytotoxicityISO 10993-5:2009Extract medium on fully post-cured parts; raw precursor MSDS data are not sufficient for multi-material ratios
    Leak tightnessISO 13485:2016 clause 7.5.1Pressure-decay fixture with ±0.5 kPa resolution; record for 100 kPa / 30 min
    Colour fastness to perspirationISO 105-E04:2013Wearable applications require grey scale rating ≥ 4 on clear phase after contact
    UV weatheringASTM G154-23200 h UVA-340; yellowness index increase 5 maximum as transition criterion

    During surgical phantom construction from CT-derived geometry, high-density cancellous structures are printed in clear CR-CL 200 while ligamentous and meniscal analogues are co-jetted in black CE-BK at the insertion zones. The rigid clear phase must remain free of wax residue above 5 µg/cm² because residues scatter light under fibre-optic endoscopic illumination. Large anatomical sections are divided across multiple builds within the 294 × 211 × 144 mm envelope, and a two-phase calibration coupon is embedded in each tray. Coupons are inspected at 10× magnification for voids and then sectioned with a diamond wire saw for bond-line width measurement. Secondary UV curing is performed at 40 °C for 4 h to minimize residual acrylate migration from the elastomer phase into the clear phase. Surface disinfection with 70 % isopropanol is validated under ISO 17664-1:2021 before reuse; repeated disinfection can etch the clear phase if contact time exceeds 30 min, so the phantom is limited to short wipe cycles. The final phantom combines transparent osseous structures and soft black tissue analogues in a single build without assembly adhesives.

    What limits the service temperature of an automotive interior latch housing with black elastomer return springs?

    Thermal soak in vehicle cabins causes dark interior surfaces to exceed 70 °C; the clear rigid phase of the composite is challenged when the latch housing must maintain spring-return function after long parking exposure. Supplier data for CR-CL 200 lists heat deflection temperature at 52 °C under 0.45 MPa according to ASTM D648-16, which places the clear phase close to its thermal limit in a dark cockpit. The black CE-BK return spring element is designed with a beam length of 8 mm, a width of 2 mm, and a flexural stroke of 2 mm; cyclic validation is performed for 10,000 cycles at 23 °C and then repeated after 72 h heat ageing at 80 °C under 50 % RH. Force decay is measured with a constant-rate tensile tester following ASTM D412-16 on die-cut co-printed slabs. Prototype failures occur when the transition radius between the clear housing and the black spring measures below 0.5 mm; increasing the radius to 1.0 mm and adding a 10° draft on the vertical sidewall reduces notch-induced tearing. Amine-containing plasticizers and PVC-insulated harness clips should not contact the black phase because they increase surface tack and can soften the elastomer; compatibility extraction follows ASTM D471-16a for 70 h at 60 °C.

    When a black elastomeric isolator is printed around a clear inspection window for industrial vibration fixtures

    When machine-vision inspection cells require a clear optical window surrounded by a black elastomeric isolator, the co-printed part eliminates the need for mechanical fastening and second-stage overmoulding. The clear window must maintain optical flatness within 3 fringes per 25 mm after elastomer cure shrinkage; flatness is measured against a fused silica reference flat under 589 nm sodium light before and after post-cure. The CE-BK isolator performs as a low-modulus damping rim; durometer measurement according to ISO 7619-1:2022 typically falls in the low Shore A range, although published data specific to the two-phase blend is limited. Perimeter bead width is set at 3 mm and clear window thickness at 0.8 mm to balance vibration isolation with impact resistance. Elastomer swell in cutting-fluid environments is a critical boundary; immersion in a reference water-soluble cutting fluid at 60 °C for 70 h under ASTM D471-16a produces measurable dimensional change, so fluorosilicone isolators are specified where glycol ether exposure is unavoidable. Post-build UV cure is extended to 6 h at 40 °C in a nitrogen-purged chamber to reduce surface tack. Acceptance testing includes ISO 527-2:2012 tensile pull of the clear-to-black boundary and ISO 868:2003 durometer measurements on the elastomeric rim.

    Within wearable exoskeleton research builds, a transparent CR-CL 200 dorsal pad is co-printed with black CE-BK contact wings that flex during treadmill walking tests at 1.5 m/s. Build orientation places the clear pad face-up to prevent wax pooling and the black wings at 20° from the X-Y plane to preserve near-isotropic elastomer properties. Support removal below 45 °C and UV post-cure at 40 °C for 3 h are followed by skin-contact testing under ISO 10993-10:2021 for sensitization and ISO 10993-5:2009 for cytotoxicity; the black pigmentation in CE-BK does not remove the need for full extractables assessment. Cyclic flexion of the co-printed interface is run on a servo-hydraulic tensile machine at 1 Hz for 50,000 cycles with strain amplitude of 20 %; delamination at the transition occurred in pre-production samples only when the interface footprint was reduced below 2.5 mm². Chemical compatibility with perspiration simulant is evaluated according to ISO 105-E04:2013 for colour fastness to perspiration, and staining of the clear dorsal pad must remain below grade 4 on the grey scale. The final prototype merges flexible black contact elements with a transparent structural shell without solvent bonding or stitching.

    Autoclave Cycling Exceeds the Heat Deflection Ceiling of the Clear Rigid Phase

    Laboratory-scale single-use bioreactor adapters use CR-CL 200 as the clear probe window and CE-BK as the black sealing gasket around the sensor port. The gasket is printed with a thickness of 1.0 mm and compressed to 20 % ± 3 % against a polycarbonate vessel flange; over-compression above 25 % creates radial tear cracks at the z-layer fusion lines. Sterilization by gamma irradiation is not automatically transferable to the clear phase because rigid acrylate photopolymers can undergo discolouration and embrittlement; electron-beam sterilisation at 25 kGy is evaluated by exposing co-printed samples and then measuring tensile properties under ISO 527-2:2012. The black elastomer phase is restricted to indirect contact with cell culture media under ISO 10993-4:2017 haemocompatibility and ISO 10993-5:2009 cytotoxicity testing. Autoclave cycles at 121 °C for 15 min exceed the heat deflection temperature of the clear phase and are not recommended; alkaline detergent cleaning at 45 °C for 20 min is preferred. The terminal bioreactor adapter combines transparent probe ports and an integral black gasket, eliminating separate silicone O-rings and mechanical retainers.

    Across consumer-grade controller prototype builds, co-printed faceplates use CR-CL 200 as a transparent display window and CE-BK as dark tactile button returns beneath a 1.2 mm clear cover. The black domes are printed with a diameter of 4 mm and a nominal wall of 0.6 mm; actuation force is measured with a force gauge at 1 mm/min and acceptance is set at 0.8 N ± 0.2 N for initial build runs. Because the clear cover must transmit LED outputs without haze, transmission haze is measured according to ASTM D1003-21 after support removal and post-cure at 40 °C for 3 h. Key cycle durability is evaluated with a pneumatic actuator at 3 Hz for 300,000 cycles; surface cracking near the dome base occurs if the draft angle is below or if the CE-BK dome wall is reduced below 0.5 mm. The material pair is restricted to proof-of-concept and short-run human-machine interface parts due to limited UV stability of the clear phase under direct sunlight; UV exposure testing follows ASTM G154-23 for 200 h UVA-340 and records yellowness index increase above 5 as a transition criterion. The final prototype merges a transparent display window and dark tactile domes in one build without adhesive film lamination.

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    Certification & Compliance
    More Introduction

    3D Systems VisiJet RCL-EBK-D70 Multi-Material Composites is a two-resin digital composite comprising the rigid clear photopolymer VisiJet CR-CL 200** and the elastomeric black photopolymer VisiJet CE-BK. The product designation RCL-EBK-D70 identifies the rigid clear/elastomeric black feedstock pair and a nominal composite hardness of 70 Shore D when evaluated according to ASTM D2240-15 or ISO 868:2003. This material is not a melt blend but a spatially controlled photopolymer network produced through MultiJet Printing, in which the two feedstocks are co-deposited in separate printhead channels and cured by UV exposure within the build layer. Published vendor data for this exact composite configuration is limited; the following technical description therefore distinguishes between manufacturer-specific values and equipment-class observations applicable to multi-material jetting systems.

    Compositional Role of the Rigid Clear and Elastomeric Black Fractions

    VisiJet CR-CL 200** functions as the high-modulus rigid clear fraction, providing the composite with dimensional stability, low rubbery compliance, and reduced gross deformation under load. VisiJet CE-BK contributes a low-modulus elastomeric black phase with higher elongation and energy-absorbing behavior. The final mechanical response of the D70 composite is governed by the voxel ratio of the two resins, the spatial arrangement of the phases, UV exposure per layer, and the post-jetting thermal history during support removal. Because the product is a digital composite, local stiffness can be altered without introducing mechanical fasteners or secondary bonding operations. Tensile properties for the final printed material should be reported using ASTM D638-14 Type IV or ISO 527-2:2012 1BA specimens, with the build orientation stated explicitly. Hardness is reported on the Shore D scale per ASTM D2240-15, with both 1 s and 15 s readings recorded if the material exhibits creep or surface relaxation.

    What Limits the Co-Jetting Stability of VisiJet CR-CL 200** and VisiJet CE-BK?

    In piezoelectric MultiJet Printing, jetting stability is controlled by viscosity at the jetting temperature, surface tension, printhead waveform synchronization, and the resistance of the resins to partial cure on the nozzle plate. A viscosity mismatch between the rigid clear and elastomeric black fractions can generate droplet volume variation across the build; this commonly appears as durometer drift in the final part rather than as gross delamination. Production-scale MJP equipment has been reported to exhibit nozzle dropout when stagnant resin in idle channels undergoes partial polymerization, when cartridges are loaded before reaching room temperature, or when printhead wipe cycles are insufficient. The manufacturer-specific handling documentation for CR-CL 200** and CE-BK should be followed when switching between single-material builds and composite D70 builds because lot-specific printhead waveform settings may be required. Published data for the exact jetting viscosity and waveform parameters of this composite is limited.

    The co-deposition process is further constrained by oxygen inhibition at the photopolymer surface. Acrylate-based MJP resins cure by free-radical polymerization, and the topmost layer remains sensitive to oxygen until the next layer is deposited. An insufficient UV dose at the rigid-elastomer interface can leave uncured monomer that migrates during support-removal heating and produces surface tack or local softening. Users may track cure conversion by Fourier transform infrared attenuated total reflectance at the acrylate C=C absorbance bands near 810 cm⁻¹ and 1635 cm⁻¹, but vendor-specific kinetic data for RCL-EBK-D70 is not publicly available.

    When Mechanical Acceptance Testing Is Applied to a 70 Shore D Composite

    Mechanical verification of this multi-material composite requires specimen conditioning at 23 ± 2 °C and 50 ± 10 % relative humidity according to ASTM D618-21 or ISO 291:2008. Hardness tests are performed on Shore D durometers per ASTM D2240-15 or ISO 868:2003. Tensile testing may follow ASTM D638-14 Type IV or ISO 527-2:2012 1BA specimen geometry; because the material contains a rigid-elastomer distribution, the gauge section should not contain a hard-soft interface unless that interface is the specific object of the measurement. Flexural modulus is determined by ASTM D790-17 or ISO 178:2019 three-point bending, with the span-to-depth ratio reported. Density may be measured by ASTM D792-20 Method A or ISO 1183-1:2019. Heat deflection temperature is evaluated under 0.455 MPa using ASTM D648-18 or ISO 75-2:2013, but a single HDT value may misrepresent the composite because the elastomeric black phase and the rigid clear phase have different thermal responses.

    Applicable Standards for VisiJet RCL-EBK-D70 Composite Verification
    PropertyPrimary Test MethodAlternative/Related MethodSpecimen Note
    HardnessASTM D2240-15ISO 868:2003Shore D, 1 s and 15 s readings
    Tensile propertiesASTM D638-14ISO 527-2:2012Type IV or 1BA; state build orientation
    Flexural modulusASTM D790-17ISO 178:2019Three-point bending; report span-to-depth ratio
    Heat deflectionASTM D648-18ISO 75-2:20130.455 MPa; report edgewise or flatwise
    DensityASTM D792-20ISO 1183-1:201923 °C; liquid resin and cured solid should be distinguished

    Compared with single-material VisiJet CR-CL 200**, the RCL-EBK-D70 composite replaces uniform rigid clear fracture behavior with locally controlled compliance distribution. Compared with VisiJet CE-BK alone, the composite raises hardness to 70 Shore D and reduces bulk elastomeric elongation. The wax support used in MultiJet Printing differs from gel-like support processes: wax removal is thermal rather than water-jet-based, and low-molecular-weight oil fractions can absorb into the elastomer-rich domains if cleaning temperature is excessive. Users transitioning from fused filament fabrication or vat photopolymerization should not assume isotropic mechanical behavior; tensile values should be compared at , 45°, and 90° build orientations according to ISO 527-2:2012.

    Shore D 70 Application Boundaries and Incompatibilities

    The composite is typically evaluated for soft-touch overmolding prototypes, seals, gasketing, flexible snap features, and vibration-damping mounts where a single 70 Shore D node is required. Cyclic loading applications should specify compression set according to ISO 815-1:2019 or ASTM D395-18 Method B. Stress relaxation may be evaluated by ISO 3384-1:2019. Thermal aging of the elastomeric black fraction should be checked using ASTM D573-04 or ISO 188:2011, while the rigid clear fraction may be assessed for heat deflection using ASTM D648-18. Published long-term aging data for this specific RCL-EBK-D70 composite is limited; users requiring service-life prediction should generate lot-specific aging curves under the intended thermal and chemical exposure conditions.

    No biocompatibility claim is inferred from this product description. Materials intended for medical use require separate evaluation under ISO 10993-5 and ISO 10993-10, and adhesive bonding or skin-contact applications should be verified for extractables and leachables according to the relevant regulatory pathway. The product should be stored away from UV light and protected from temperature extremes specified in the Safety Data Sheet. Cold resin cartridges should be equilibrated to the manufacturer-specified loading temperature before insertion; low-temperature resin increases viscosity and can produce missing jets. Do not add alcohols, ketones, or amine-containing solvents to the feedstocks; these materials may precipitate the photopolymer or inhibit free-radical cure. The elastomeric black phase can swell in certain hydrocarbon and chlorinated solvent environments, so process fluid compatibility should be assessed by gravimetric immersion testing according to ASTM D543-21 before deployment.

    Production acceptance should include hardness coupons printed at the same build location as the final part because durometer can vary with proximity to the UV lamp and with local resin aging in the printhead. A build acceptance protocol using ASTM D2240-15 hardness testing on a 6 mm-thick coupon and dimensional verification according to ISO 286-1 can detect source variation without requiring destructive testing of the final component. If the nominal D70 value is contractual, the acceptable Shore D tolerance should be derived from process capability data rather than from a single vendor nominal.

    Support removal for multi-material composites is more demanding than for single-material rigid clear builds. The wax-like support matrix fills cavities and undercuts during printing. Cleaning involves elevated-temperature melting followed by oil or rinse cycles. Internal channels with diameter below 2 mm and length-to-diameter ratio above 3:1 can retain wax if oven residence time is insufficient or if the channel is not oriented for drainage. Wax residue can plasticize the elastomer phase and alter the effective Shore D at the surface. Published data for this specific composite configuration is limited; users should validate support removal by mass change and hardness before serial production.

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