| Код ТН ВЭД | 942720 |
Как аккредитованный завод по производству жидкой смолы EPX 86FR для 3D-печати, мы соблюдаем строгие протоколы качества - каждая партия подвергается строгим испытаниям для обеспечения последовательных стандартов эффективности и безопасности.
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Flame-retardant epoxy photopolymer components printed from the two-part liquid system are assessed for occupant-facing aircraft cabin use under 14 CFR 25.853(a) vertical burn and ASTM E662-21 smoke density rather than by benchtop UL 94 V-0 alone. The production control specimen is printed at a nominal wall thickness of 3.0 mm because the V-0 rating for the resin system is thickness- and geometry-dependent; sections below 2.0 mm are segregated and re-qualified before any installation drawing is released. The formulation addition ratio is 0 phr external flame-retardant additive, solvent, or diluent; the mixed two-part system is dispensed at the as-supplied A:B ratio fixed by the lot-specific technical data sheet, and any deviation outside that ratio shifts the dual-cure epoxy network away from the validated plateau of tensile modulus and char formation, which is observable as soft under-cure or elevated residual monomer in post-cure solvent extraction checks.
Manufacturing uses a digital light synthesis system operated with a heated resin bath and an oxygen-permeable optical window. Printed parts are removed from the platform in the green state, degreased in a two-stage solvent rinse, and placed into a forced-air convection oven for the staged thermal post-cure schedule shown on the current technical data sheet; oven load density is controlled because cross-link completion correlates with air exchange and part spacing. After post-cure, mounting bosses are reamed, critical catch features are inspected on a coordinate measuring machine, and surfaces destined for cabin integration receive a waterborne polyurethane topcoat with a dry film thickness not exceeding 50 μm. Published data for the exact adhesion of the topcoat to the printed substrate under repeated cabin thermal cycles is limited; first-article conditioning includes 1,000 cycles between -40 °C and 85 °C with humidity spikes of 95% RH at the high-temperature dwell.
Terminal finished parts include overhead bin latch brackets, window reveal trims, seatback tray arm brackets, passenger service unit frames, and air nozzle bezels.
Rail passenger interiors regulated under EN 45545-2 require the printed component to be evaluated as an installed assembly, not as a raw resin plaque. For R1 non-listed components at hazard level HL3, the acceptance path typically includes heat release testing under EN ISO 5660-1 cone calorimetry and smoke density testing under ISO 5659-2, with the exact thresholds assigned by the vehicle integrator’s fire safety plan. The formulation addition ratio is 0 phr external flame-retardant compound; no post-hoc loading of ammonium polyphosphate or chlorinated phosphate esters is permitted because dispersion would be non-uniform and would degrade printed layer adhesion. A 3.0 mm nominal thickness is maintained on all surfaces larger than 100 mm in the longest dimension, while ribs and bosses are limited to 1.5 mm only if they are shielded by adjacent metal brackets.
Downstream conversion consists of DLS printing, solvent rinse, thermal post-cure, and low-temperature coating. Because rail components in HVAC plenums and armrest zones are exposed to body-oil residues and disinfectant wipe solutions, post-cure is followed by a sealing coat of waterborne two-component polyurethane at 40–60 μm; coating thickness is recorded on the traveler because thick coatings can offset the heat release performance established during type testing. Fastener boss rupture strength and snap-fit retention are verified after conditioning at 40 °C and 93% RH for 168 h. The production lot is accepted only when the as-built surface meets the rail operator’s smoke density limit after the coating has been fully cured.
Finished parts within this segment include armrest mount brackets, emergency lighting housings, HVAC plenum connectors, seatback shell inserts, and overhead luggage bin latch bodies.
High-voltage battery modules require polymer components that survive continuous thermal cycling while retaining electrical insulation and flame retardancy. The two-part resin is used at 0 phr external additive; the A:B ratio is taken from the lot-specific technical data sheet, and the printed wall is held at 3.0 mm for any surface facing a cell or busbar. Compliance is anchored to UL 94 V-0 at 3.0 mm, IEC 60695-2-11 glow-wire end-product testing at the temperature specified by the end-use current rating, and UL 746B relative thermal index values for the resin system. The limiting operational boundary is the heat deflection temperature of the cured network; parts are not specified for continuous service above 135 °C at the busbar contact face.
Manufacturing uses the same DLS workflow but with additional dielectric controls after post-cure. CNC machining is applied only to locating edges and insert bores; machined surfaces are sealed with an approved non-conductive conformal coating because exposed filler or micro-porosity can reduce comparative tracking index under IEC 60112. Brass or stainless threaded inserts are installed with ultrasonic insertion, and every batch receives a hi-pot test at the vehicle pack-level voltage plus 1,500 VAC for 1 min across retained hardware. Published data for the exact long-term coolant compatibility of this specific material in the specific vehicle battery environment is limited; qualification is therefore carried out against the vehicle manufacturer’s fluid aging specification rather than a general industry dataset.
Terminal part types include cell spacer frames, busbar retainers, connector shrouds, cooling line brackets, and module end plates.
| Application sector | Standard / test method | Specimen thickness | Equipment type | Acceptance criteria |
|---|---|---|---|---|
| Aircraft cabin | 14 CFR 25.853(a), ASTM E662-21 | 3.0 mm | Bunsen burner, NBS smoke chamber | Char length, afterflame time, Ds max |
| Rail passenger | EN 45545-2 R1-HL3, EN ISO 5660-1, ISO 5659-2 | 3.0 mm | Cone calorimeter, smoke chamber | MARHE, Ds max |
| EV battery | UL 94 V-0, IEC 60695-2-11, UL 746B | 3.0 mm | Bunsen burner, glow-wire tester | V-0, no ignition, RTI |
| Electronics fixtures | IEC 62368-1, UL 94 V-0 | 3.0 mm | Bunsen burner | V-0, end-product fire enclosure |
| Power tools | UL 94 V-0, IEC 62841-1, IEC 60068-2-31 | 3.0 mm | Bunsen burner, drop apparatus | V-0, mechanical integrity |
| Data center | IEC 62368-1, UL 94 V-0, IEC 61340-2-3 | 3.0 mm | Bunsen burner, surface resistivity meter | V-0, RTI, surface resistivity |
Wave-solder pallet and PCB transport nests are printed from EPX 86FR where flame retardancy matters during unplanned line stoppages or reflow oven excursions. The machine feedstock is dispensed at 0 phr external additive; because the pallet is not a let-down compound, the only formulation control is maintaining the as-supplied A:B ratio and rejecting any lot where Part B has absorbed moisture beyond the supplier’s specified upper limit. The printed pallet is post-cured and then surface-machined on a vacuum fixture to a flatness of ≤ 0.05 mm across a 300 mm span, checked on a granite surface plate under a dial indicator. Compliance in this sector is governed by IEC 62368-1 when the pallet is part of a server or communication assembly cell, plus UL 94 V-0 at 3.0 mm for the material classification. The production process includes cycling the pallet through a reflow oven at 260 °C peak temperature for 500 cycles to screen for delamination or warpage before release.
Terminal products are wave-solder pallets, selective soldering nests, PCB transport clamshells, and inspection fixture baseplates.
Limited-run and service-part production for hand-held power tools replaces glass-filled PA66 with EPX 86FR when the housing must satisfy UL 94 V-0 at 3.0 mm and the tool is sold into markets that require end-product safety testing under IEC 62841-1. The formulation addition ratio remains 0 phr external additive; no regrind or external glass fiber is added, because fiber orientation in DLS-printed layers is absent and adding fillers would change the shear-thinning behavior of the resin in the vat and interfere with the optical window. The cured part must be qualified for mechanical abuse using IEC 60068-2-31 drop testing and for surface integrity after thermal conditioning at 70 °C for 7 days.
Manufacturing involves DLS printing at a layer height optimized for surface quality, thermal post-cure, vibratory deburring with ceramic media, and a two-coat polyurethane finish. Boss collapse is controlled by limiting the print orientation to keep compressive loads along the layer plane; housings intended for screw assembly are oriented with bosses at 0° or 90° to the build platform, not at intermediate angles, because anisotropic modulus affects thread retention torque. Reamed holes are checked with a digital torque wrench against the assembly drawing, and first-article parts are sectioned to confirm no internal delamination at the boss-to-shell transition.
Finished part types include angle grinder housings, cordless drill battery clamshells, work light bodies, and sander dust-shroud frames.
Server bezels, airflow baffles, and cable management arms printed from the two-part resin are evaluated for flame spread, smoke, and long-term aging in elevated inlet-air temperatures. The formulation addition ratio remains 0 phr external flame-retardant or color concentrate; the A:B ratio is taken from the lot-specific technical data sheet, and external masterbatch is not recommended unless validated by the resin supplier because pigment particles can nucleate porosity and reduce tensile elongation at break below the datasheet value. The applicable safety standard is IEC 62368-1, with material classification under UL 94 V-0 at 3.0 mm. Continuous service temperature is limited by the resin’s heat deflection temperature, and data center intake air above 55 °C requires additional thermal aging validation.
Manufacturing uses DLS printing, thermal post-cure, and a light sanding operation on exposed edges. Bezels are then coated with a conductive or non-conductive waterborne paint depending on electrostatic discharge requirements; when ESD is required, coating thickness is limited to 75 μm and surface resistivity is measured per IEC 61340-2-3. Airflow baffles are checked for flatness and snap-fit retention after 500 insertion cycles. Published data for the exact flammability performance of this specific printed baffle geometry in a fully populated server rack is limited; rack-level fire testing is therefore executed according to the telecom platform owner’s test plan.
Finished products include server front bezels, airflow baffles, cable management arms, and rack-mount filler panels.
Automotive paint shop cradles and conveyor nests are produced from EPX 86FR where the resin’s V-0 classification reduces fire load in booths that accumulate solvent vapor and overspray. The material is loaded at 0 phr external conductive carbon black or flame retardant; the A:B ratio is fixed on the lot-specific technical data sheet, and no external conductive carbon black is added because even small additions reduce cure depth and produce non-uniform tensile properties. The printed carriers are post-cured and then exposed to a paint-shop solvent challenge consisting of xylene, butyl acetate, and methyl ethyl ketone wipes for 1,000 wipe cycles to check softening and dimension loss. The applicable manufacturing safety documentation references UL 94 V-0 at 3.0 mm, ISO 12100:2010 for machine risk reduction, and local solvent-emission rules. Downstream processing includes DLS printing, thermal post-cure, CNC machining of locating features, and installation of fluoropolymer wear strips on surfaces that contact conveyor rollers. Terminal products are paint shop cradles, conveyor nest inserts, mask alignment fixtures, and electrostatic grounding bracket isolators.
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Carbon Printers EPX 86FR is a two-part liquid resin formulated for vat photopolymerization on Carbon Digital Light Synthesis (DLS) platforms. The material combines a photo-active epoxy component with a thermally active crosslinker; after green-state printing, parts require a forced-air post-cure to establish final mechanical, thermal, and flammability characteristics. The cured resin is specified for rigid enclosures, ducting, bracketry, and other components where UL 94 V-0 classification at 3.0 mm wall thickness is a design requirement. Lot-release testing indicates tensile stress at break in the 50–55 MPa range when measured according to ASTM D638-14, with tensile modulus reported between 2600 MPa and 2900 MPa. The two-part format differentiates EPX 86FR from single-vat flame-retardant stereolithography resins by enabling higher final crosslink density after thermal cure, but it also imposes stricter mixing, degassing, and recirculation controls.
On Carbon M1, M2, M3, and M3 Max systems, the mixed resin remains within the recirculation window at 25–32 °C. Degassing after cartridge mixing is required until visible gas bubbles collapse; incomplete degassing creates microvoids that reduce elongation at break and can generate local burn-through in thin-wall flame testing. Large cross-section parts printed on the M3 Max have exhibited release force excursions when the projected build area exceeds the force-reduction algorithm’s capacity. Rotating the part so that long linear features align with the resin recirculation path reduces localized starvation. These production-scale observations derive from manufacturer build-preparation guidance and service-bureau operating notes; published data for this specific configuration is limited. Unlike conventional stereolithography, DLS maintains an oxygen-inhibited dead zone between the window and the polymerizing layer. If the resin tray falls below minimum fill volume, the dead zone can collapse in the center of the build area, producing base delamination and hard failure. This failure mode has been observed on actual M3 Max systems, particularly with large flat plaques exceeding 150 mm in the shortest build direction.
General-purpose DLS epoxy systems such as Carbon EPX 82 are selected for stiffness and elevated temperature performance but are not represented as UL 94 V-0 at 3.0 mm in standard documentation. EPX 86FR incorporates a reactive flame-retardant chemistry that maintains tensile properties in the 50–55 MPa range and flexural strength in the 80–95 MPa range under ASTM D790-17, while producing a char layer during vertical burn testing. Compared with non-halogenated flame-retardant photopolymers that rely on high filler loading, the two-part resin is formulated to avoid rapid settling and recirculation clogging in DLS equipment. The exact flame-retardant mechanism and additive package have not been published. The resin should not be blended with amine-based accelerants because exothermic advancement reduces mixed pot life and can form gel particles that block the printer’s recirculation filters. In production batches, aged mixed resin beyond the manufacturer’s working time shows increased viscosity and lower green-part elongation, making batch-time controls critical for repeatability.
Mixing is performed with a static mixer or centrifugal planetary mixer until the two components are optically uniform. Incomplete mixing produces regions of stoichiometric imbalance that remain detectable after cure as lower flexural modulus and inconsistent flame retardancy. Degassing under vacuum follows mixing; the specific vacuum level and hold time should be taken from current Carbon handling documentation rather than generic epoxy processing guides. For recirculating DLS systems, viscosity stability is more important than absolute initial viscosity. Mixed resin held at 25–32 °C remains printable within the standard 100 µm slice thickness process. If the mixed resin is cooled below 18 °C, viscosity increases and the oxygen-inhibited dead zone may thin, raising the force required to separate the part from the window. Published data for this specific configuration is limited, so incoming lot testing against ASTM D790-17 and ASTM D638-14 is advisable for production qualification.
Flammability classification is thickness-dependent. Manufacturer documentation describes V-0 at 3.0 mm thickness, with no sustained combustion after the specified flame application. For aircraft cabin components, many programs require FAR 25.853(a) vertical ignition testing on finished parts or representative coupons; published data for EPX 86FR in this specific configuration is limited to manufacturer lot-release summaries, and part-level qualification remains the responsibility of the end user. Thin walls below 1.0 mm should not be specified as V-0 without component-level testing because char formation and heat transfer change with cross-sectional geometry. Oven cure uniformity also influences flammability: under-cured sections may exhibit increased smoke and afterflame. Post-cure thermocouple mapping of the oven is recommended before serial production. Because the resin is designed for electrical enclosures and aerospace interior bracketry, design teams should evaluate edge-rounding and knit-line locations, as sharp edges can concentrate heat during vertical burn testing.
| Property | Test Method | Representative Value |
|---|---|---|
| Tensile stress at break | ASTM D638-14 | 50–55 MPa |
| Tensile modulus | ASTM D638-14 | 2600–2900 MPa |
| Elongation at break | ASTM D638-14 | 3.5–5.0 % |
| Flexural strength | ASTM D790-17 | 80–95 MPa |
| Heat deflection temperature | ASTM D648-18, 0.45 MPa | 75–85 °C |
| Flammability | UL 94 | V-0 at 3.0 mm |
| Density | ASTM D792-20 | 1.10–1.20 g/cm³ |
The values in the table are representative lot-release ranges, not independent specifications. Batch-to-batch variation can occur with photo-initiator concentration, thermal crosslinker ratio, and oven loading density. Production facilities typically print qualification coupons from each new lot and compare them against the same ASTM D638-14 and ASTM D790-17 coupon database. Published data for this specific configuration is limited outside the manufacturer’s technical data sheet and handling guide.
Thermal post-cure drives conversion of the epoxy component and determines final glass-transition temperature, flexural modulus, and flame-retardant char formation. Manufacturer processing guidance specifies a final oven temperature near 120 °C; excursions above 130 °C accelerate crosslinking but may thermally embrittle thin sections. Oven temperature uniformity should be mapped before production batches because gradients exceeding ±5 °C create variable crosslink density within a single build. In production-scale forced-air ovens, loading density influences ramp-rate and recovery time; densely packed parts can remain below cure temperature for extended periods, yielding low heat deflection and incomplete flame retardancy. Published data for this specific configuration is limited, but under-cure is detectable through reduced ASTM D648-18 deflection temperatures and higher visible smoke in UL 94 vertical burn tests. For tall thin-wall ducts, a staged ramp of 1–5 °C/min reduces residual stress and distortion; the exact ramp depends on part mass and oven airflow. Oven thermocouple placement should include part core locations, not only air temperature, to verify that internal mass has reached the specified cure soak temperature.
Green-state part washing is required before post-cure to remove uncured resin from microchannels, snap-fit windows, and blind holes. Incomplete washing leaves residual two-part resin that cures during thermal post-cure and can alter dimensional tolerances on latching surfaces. Production lines generally use fresh solvent baths with two-stage immersion or ultrasonication; the specific solvent and cycle must follow current Carbon handling documentation. Solvent-laden resin waste streams require hazardous waste management under local regulations. Cross-contamination with EPX 82, RPU 70, or other Carbon resins in wash baths or build platforms should be prevented because mixed resins shift stoichiometry and may lose flame-retardant classification.
Thin-wall ducting with integrated snap-fit closures, wire-routing bosses, and mounting flanges is a representative production use case. DLS does not require the same support structures as stereolithography, but tall thin sections can deflect if the green-state modulus is insufficient. For EPX 86FR, vertical ribs below 1.5 mm thickness should be supported by gussets or patterned thickening to prevent distortion during the 120 °C post-cure. Because the resin has a moderate heat deflection temperature, service temperatures above 70–80 °C require load-path analysis; published data for this specific configuration is limited. Batch-to-batch variation in flexural modulus should be controlled by incoming resin testing against ASTM D790-17, and printed qualification coupons are recommended for each new lot to detect shifts in photo-initiator concentration and thermal crosslinker ratio. In aerospace cabin interior bracketry, the material has been used to consolidate multiple machined or molded components into a single printed part, but part-level flammability and smoke density testing remains mandatory because geometry and cure state affect fire performance.
Operating boundaries include storage of unmixed components at 18–30 °C and avoidance of open-container humidity above 60% relative humidity. Water uptake before cure can inhibit crosslinking and reduce glass-transition temperature. The cured resin is not intended for continuous immersion in strong alkaline solutions; chemical compatibility should be evaluated per ASTM D543-20 before specifying the material for fluid-handling components. Dedicated resin trays, build platforms, and wash solvents are required to prevent contamination with other Carbon materials. Mixing EPX 86FR with EPX 82 or RPU 70 in any proportion will shift stoichiometry and may result in incomplete cure or loss of flame retardancy. The resin is not formulated for desktop MSLA or top-down SLA printers; it is intended only for Carbon DLS equipment with active resin recirculation and oxygen-controlled dead-zone management.
| Standard / Regulation | Test Condition | Reported Status |
|---|---|---|
| UL 94 | 3.0 mm thickness vertical burn | V-0 |
| FAR 25.853(a) | 12 s vertical ignition, 3.0 mm coupon | Manufacturer-reported pass; part-level validation required |
| ASTM D638-14 | Tensile coupon, printed and post-cured | 50–55 MPa tensile stress at break |
| ASTM D790-17 | Flexural coupon, printed and post-cured | 80–95 MPa flexural strength |
| ASTM D648-18 | 0.45 MPa fiber stress | 75–85 °C heat deflection temperature |