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CRP Technology Windform FR1 Carbon Filled Flame Retardant Composite Polyamide for Additive Manufacturing

    • Название продукта: CRP Technology Windform FR1 Carbon Filled Flame Retardant Composite Polyamide for Additive Manufacturing
    • Сайт Factroy: Округ Юду, Ганьчжоу, Цзянси, Китай
    • Запрос цены: admin@ascent-chem.com
    • Производитель: Ascent Petrochem Holdings Co., Limited
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    Спецификации
    Код ТН ВЭД 477422

    Как аккредитованный завод CRP Technology Windform FR1 Carbon Filled Flameretardant Composite Polyamide for Additive Manufacturing, мы соблюдаем строгие протоколы качества - каждая партия подвергается строгим испытаниям для обеспечения последовательных стандартов эффективности и безопасности.

    Упаковка и хранение
    Упаковка Packaged in a sealed, moisture-resistant 5 kg container, clearly marked with product name, batch number, and safety handling instructions.
    Погрузка контейнера (20-футовый контейнер) 20′ FCL container loading: CRP Technology Windform FR1 carbon-filled flame-retardant polyamide composite for additive manufacturing, palletized and secured for sea transport.
    Доставка CRP Technology Windform FR1 Carbon Filled Flame Retardant Composite Polyamide for Additive Manufacturing is generally shipped as a non-hazardous powder in sealed, moisture-resistant containers. It is not classified as dangerous goods for air, sea, or road transport. Store and transport cool, dry, away from ignition sources, avoiding dust and static discharge.
    Хранение Store Windform FR1 in its original sealed, labeled container in a cool, dry, well-ventilated area away from sunlight, heat, ignition sources, and oxidizers. Protect from moisture and static discharge; avoid dust clouds. Keep containers closed when not in use. Follow SDS guidance, local regulations, and use appropriate PPE. Do not eat, drink, or smoke in storage areas.
    Срок годности Store sealed in original packaging, cool and dry; typical shelf life is 12 months unopened, away from moisture and heat.
    Применение технологии CRP Windform FR1 наполненного углеродом композитного полиамида для аддитивного производства

    In cabin air distribution plenums for fixed-wing regional aircraft, Windform FR1 is processed as a 100 wt% virgin feedstock for first-article parts requiring vertical Bunsen burner compliance under FAR 25.853(a) and the FAA Fire Test Handbook Chapter 2. The formulation contains no post-additive flame-retardant masterbatch at the converter level; dilution with unfilled PA12 or PA11 at any concentration above 5 wt% invalidates the halogen-free FR system and shifts limiting oxygen index, measured per ISO 4589-2, away from the classified coupon value. Serial production permits a 70:30 virgin-to-reclaimed weight ratio only after three consecutive lots show no loss of UL 94 V-0 classification on post-build panels of 3.0 mm thickness; reclaimed powder is sieved through a 150 µm stainless-steel mesh and dried at 80 ± 5 °C for 8 h when storage relative humidity exceeds 55%. The build is executed on a polymer laser sintering system with a 30–50 W CO₂ source, 0.12 mm layer thickness, nitrogen inerting below 2 vol% O₂, and a powder bed temperature held within 3 K of the crystalline melt onset but below the recrystallization shoulder. Plenum bodies are oriented 25–35° from the recoater blade axis to limit edge curl; internal channels are designed with 3 mm minimum drain openings to allow depowdering of trapped carbon-loaded powder before glass-bead blasting at 4 bar. Wall thickness below 1.0 mm requires part-level FAR 25.853 testing because the published vertical burn classification is not automatically preserved in thin ribs and snap-fit flanges. Terminal parts in this class include cabin air distribution plenums, avionics cooling duct adapters, and passenger service unit bracket housings.

    Can Halogen-Free SLS Polyamide Meet EN 45545-2 R1 Requirements for Rolling-Stock Interior Bracket Systems?

    Rolling-stock interior fittings specified under EN 45545-2:2020 are evaluated at the component level, with the required hazard level determined by the vehicle operation category and the part’s distance from escape routes. Windform FR1 is specified for seat-back table brackets, armrest support frames, and electrical cabinet stays only after a compliance file has been assembled with ISO 5659-2 smoke density, ISO 5660-1 heat release, and EN 45545-2 R1 flame propagation data for the exact wall thickness and surface finish applied in serial production. The feedstock is not diluted with halogenated or phosphorus masterbatch at the downstream processor; the only permissible addition is remix of reclaimed FR1 powder from the same build lot, controlled at 30 wt% maximum because repeated thermal exposure in the sintering bed can raise the carbonyl index and shift smoke density above the HL2 acceptance corridor. Powder bed processing for rail parts uses 0.12 mm layers, a bed temperature maintained within 4 K of the powder’s melt onset, and a minimum wall thickness of 1.6 mm across screw bosses and metal-insert bosses. Instead of secondary flame-retardant coatings, which crack on thin-section seat brackets under EN 61373 Category 1 Class B vibration profiles, the material is machined at insert bores with carbide tooling during the warm-cake phase and fitted with helical or heat-set M4 brass inserts. Ejection from the build cake is delayed until cake surface temperature falls below 60 °C to prevent warpage in thin-section bracket webs. The downstream terminals include integrated seat-back tray arms, armrest mounting brackets, window reveal covers, and electrical cabinet stays produced in batch sizes of 50–500 units where injection tooling is uneconomical.

    Glow-Wire Ignition Resistance in Unshielded Electronics Housings and Connector Shells

    Unshielded electronics housings produced by polymer laser sintering require flame-retardant performance that survives geometric variation, machining of snap-fit windows, and fastener installation rather than only a 3.0 mm test coupon. Under UL 94, Windform FR1 carries a V-0 classification at 3.0 mm thickness; converting that classification to an end housing requires that the machine shop not blend the powder with unfilled PA12, because 10 wt% unfilled PA12 contamination can alter the vertical burn time beyond the 10 s afterflame limit in the UL 94 V-0 protocol. IEC 60695-2-11 glow-wire testing at 850 °C and 960 °C is performed on the final part when the housing will be mounted near uninsulated live parts, because the carbon-filled matrix can produce localized hot spots at molded-in stress concentrations; published data for the specific combination of Windform FR1 and IEC 60695-2-11 final-product geometry is limited, and first-article inspection should treat glow-wire performance as a part-dependent variable rather than a material constant. The production route uses 0.10 mm layer thickness to hold snap-fit deflections within 0.15 mm total tolerance on lengths to 80 mm, with the powder bed inerted below 2 vol% O₂ and reclaimed powder held at 30 wt% maximum after 150 µm sieving. Lot acceptance includes melt flow index measurement per ISO 1133-1:2022; a viscosity shift greater than 15% from the virgin lot value triggers powder re-qualification or a reduced reclaim ratio. Vapour smoothing is omitted because solvent exposure introduces an uncontrolled surface layer whose flammability contribution has not been validated under UL 94. Terminal products include circuit breaker housings, busbar terminal covers, sensor enclosures, and connector shells for power distribution units.

    When Carbon-Filled FR1 Replaces Machined Aluminum in Low-Rate Motor Sport Intake Plenums

    In low-rate motor sport intake plenums, the substitution of machined aluminum with a carbon-filled flame-retardant SLS polyamide alters the failure mode from ductile bending to notch-sensitive brittle fracture at stress risers; therefore the design review includes ISO 527-2 tensile testing on printed coupons and ISO 179-1 Charpy impact testing on unnotched specimens. The published density of 1.09 g/cm³ for Windform FR1 provides a mass reduction of approximately 60% compared with aluminum; the tensile modulus near 3,200 MPa is insufficient for a direct one-to-one wall thickness transfer from aluminum, so plenum walls are thickened to maintain burst pressure above 1.5 bar during backfire events. The feedstock is kept at 100 wt% Windform FR1 for plenum bodies; reclaimed powder is limited to 20 wt% for non-structural duct extensions because batch-to-batch melt flow variation measured by ISO 1133-1:2022 has a larger influence on tensile modulus in thin-walled regions than in solid test plaques. Production occurs on a 30–50 W CO₂ laser sintering system with 0.12 mm layer thickness, and internal plenum runners include 3 mm minimum cleaning ports; after depowdering, flange surfaces are faced by CNC and sealed with a two-component epoxy approved for continuous service at 150 °C. Unfaced as-lasered surfaces are not sealed with acetoxy-cure silicone adhesives, because acetic acid release can accelerate polyamide degradation in warm engine-bay air. Terminal parts include sealed intake plenums, brake cooling duct segments, ECU mounting brackets, and carbon canister shields.

    Although carbon-filled flame-retardant polyamide is specified for fire behavior, the use of Windform FR1 in lithium battery module structural supports first requires a short-beam shear test to quantify interlayer fusion adequacy, because carbon fiber can reduce powder absorption uniformity and produce weak fusion layers at part orientations parallel to the build platform. Under UL 94, the V-0 classification at 3.0 mm supports fire-barrier claims for bracketry located adjacent to cell stacks, but the carbon-filled matrix is not considered a primary electrical insulator; creepage and clearance paths are maintained by separate glass-fiber reinforced polysulfone or polycarbonate insulators with IEC 60664-1 dimensioning. The feedstock for energy storage brackets is maintained at 100 wt% Windform FR1 with reclaim limited to 20 wt% after 150 µm sieving, because dust generated from carbon-filled powder can collect in the recoater seals and alter layer density on builds longer than 30 h. Pre-drying at 80 ± 5 °C for 8 h is required after exposure to ambient humidity above 55% to prevent powder clumping and electrostatic discharge during sieving; the sieving station is grounded to below 1 MΩ and the extraction system is specified for conductive dust in accordance with the applicable ATEX directive. The build uses 0.12 mm layer thickness and a bed temperature held within 3 K below the powder’s melt onset; post-processing includes CNC drilling of mounting bores, insertion of stainless-steel threaded inserts, and dimensional inspection to ISO 2768-1 fine class on critical hole centres. Terminal products include battery pack mounting brackets, cell stack retention plates, coolant tube spacers, and fire-barrier plates between adjacent module cells.

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    Сертификация и соответствие требованиям
    Более подробное введение

    CRP Technology Windform FR1 is a carbon-fiber-filled flame-retardant polyamide composite formulated specifically for powder bed fusion–laser beam (PBF-LB) additive manufacturing. The powder is supplied as a free-flowing black feedstock and is processed on commercial selective laser sintering equipment using manufacturer-provided parameter sets. Published material data list UL 94 V-0 flammability performance at 1.5 mm and 3.0 mm section thickness; tensile, flexural, and thermal tests are reported under ISO 527-2:2012, ISO 178:2019, and ISO 75-2:2020 protocols. Relative to unfilled PA12 laser-sintering powders, the carbon fiber filler raises elastic modulus and heat-deflection temperature, reduces elongation at break, and changes the dielectric and surface-resistance behavior of printed parts.

    What Processing Window Governs FR1 Powder Consolidation in Laser Sintering?

    Powder conditioning is the first critical control point. Although the supplier publishes specific drying recommendations, moisture contents above 0.1 wt% typically produce surface porosity, spatter, or feed-hopper bridging in carbon-filled polyamide powders. In production-scale PBF-LB equipment with 10.6 µm CO₂ lasers, layer thicknesses of 100 µm to 120 µm are used for FR1. The beam focus diameter typically lies between 400 µm and 500 µm, and laser power, scan speed, and scan spacing must be adjusted to maintain an energy-density window that is narrower than that of unfilled PA12 because carbon fiber increases infrared absorption at the 10.6 µm wavelength.

    Thermal management during the build is determined by the semi-crystalline behavior of the polyamide matrix. Differential scanning calorimetry per ISO 11357-3:2018 on virgin and recycled powder identifies the onset of recrystallization. The build chamber is maintained within 3 °C to 5 °C of that onset temperature. If the bed temperature falls below the window, accumulated internal stresses produce curl, edge lift, and dimensional error in the Z axis. If the bed temperature exceeds the window, powder caking, part growth, and surface roughening occur. Carbon fiber and flame-retardant additives modify the crystallization rate; therefore, parameter maps developed for unfilled PA12 cannot be directly transferred to FR1.

    Recycling practices are a second processing constraint. Used powder is typically blended with virgin material at a refresh ratio of 30 % to 50 % in industrial SLS service bureaus. Below this ratio, excessively aged powder can increase melt viscosity, reduce interlayer fusion, and lower notched impact values; above it, material cost rises without proportional mechanical gains. The carbon fiber length distribution also shifts with repeated thermal cycling, and this shift changes tensile modulus and surface roughness. Batch-to-batch control can be implemented through melt flow rate testing according to ISO 1133-1:2022 and ash-content measurement according to ISO 3451-1:2019; published data linking specific shifts in these values to mechanical property degradation are limited.

    The build chamber is typically purged with nitrogen to maintain oxygen concentration below 5 %, reducing thermo-oxidative degradation of the polyamide and the flame-retardant package. Volumetric energy density is commonly expressed as E = P/(v·h·t), where P is laser power in watts, v is scan speed in millimetres per second, h is hatch spacing in millimetres, and t is layer thickness in millimetres. FR1 generally processes within a lower energy-density range than unfilled PA12 because of carbon-fiber absorptivity, but the exact acceptable band is machine-specific and must be anchored to build trials. Controlled cool-down after the build is used to allow crystallization to proceed without generating residual stress sufficient to warp thin walls or large flat panels.

    Mechanical, Thermal, and Flammability Data Reported Under ISO, ASTM, and UL 94 Protocols

    Table 1 lists representative manufacturer-published values for laser-sintered FR1 specimens. The values are not design allowables; they are baseline data from standard test coupons and must be adjusted for print orientation, wall thickness, surface finish, and environmental conditioning. Tensile data are generated with ISO 527-2:2012 using 1BA geometry; flexural data use ISO 178:2019; heat-deflection temperature follows ISO 75-2:2020 Method A at 1.82 MPa; notched impact data follow ISO 180:2019/A.

    PropertyStandardReported Value
    DensityISO 1183-1:20191.11 g/cm³
    Tensile strength at breakISO 527-2:201247 MPa
    Tensile modulusISO 527-2:20123,990 MPa
    Elongation at breakISO 527-2:20122.2 %
    Flexural strengthISO 178:201970 MPa
    Flexural modulusISO 178:20193,200 MPa
    Notched Izod impactISO 180:2019/A4.8 kJ/m²
    Heat deflection temperatureISO 75-2:2020/A145 °C
    FlammabilityUL 94:2013V-0 at 1.5 mm and 3.0 mm

    The UL 94 V-0 classification is a bench-scale material flammability result and does not automatically cover all part thicknesses, colors, or post-finishing films. For system-level fire performance, additional testing according to EN 45545-2, NFPA 130, or FAR 25.853 may be required. Electrical insulation parameters such as comparative tracking index under IEC 60112 and dielectric strength under IEC 60243-1 are not consistently published for carbon-filled FR1; published data for this specific configuration are limited. Designers should not treat the UL 94 V-0 result as equivalent to electrical clearance compliance under IEC 60664-1.

    When FR1 Replaces FR-4, Glass-Filled FR2, or Machined Aluminum in Electrical Enclosures

    For electronics enclosures, the primary substitution criterion is not bulk mechanical strength but stiffness, insulation, and fire-system behavior. Printed FR1 is anisotropic: Z-axis tensile strength is typically 20 % to 35 % lower than XY strength because interlayer fusion boundaries act as mechanical discontinuities. Parts should therefore orient bosses, snap-fit arms, and load-bearing webs parallel to the build plane. In bending, replacing a solid aluminum wall with FR1 at equal flexural rigidity requires a solid-section thickness increase of approximately 2.5× because aluminum exhibits a flexural modulus near 69 GPa, while FR1 is reported near 3.2 GPa. Despite this increase, the density difference between FR1 at 1.11 g/cm³ and aluminum at 2.7 g/cm³ still yields a lower-mass part, but the thicker section may affect connector spacing, airflow, and electromagnetic shielding.

    Against glass-filled Windform FR2, carbon-filled FR1 provides higher stiffness and improved heat-deflection behavior but has reduced dielectric and insulation potential because carbon fiber lowers bulk and surface electrical resistivity. For housings in which clearance and creepage distances are minimal, glass-filled FR2 may be the more readily qualified material unless electrical insulation testing on FR1 specifically demonstrates conformance to IEC 60112 and IEC 60243-1. Machined FR-4 sheet has higher flexural modulus—typically 24 GPa—and superior creep resistance, but it cannot reproduce integrated ducts, cable strain-relief features, or snap-fit geometries in a single build. The selection logic should therefore weigh part consolidation and mass reduction against the electrical and fire-system qualification burden created by the carbon-filled formulation.

    Adhesives and coatings must be selected for polyamide compatibility. Aggressive polar solvents can attack the matrix or extract flame-retardant additives; amine-based adhesive systems may be unsuitable without compatibility testing. Moisture absorption in polyamides reduces glass-transition-dependent properties and can shift dimensional stability in humid environments above 60 % RH. Pre-drying or sealed packaging after post-processing is therefore required if the parts are to be stored and then used in high-voltage electrical assemblies.

    Flame-retardant qualification at the end-use level is a component-scale exercise. A UL 94 V-0 material card is not sufficient for railway or aircraft interior components because printed surface roughness, paint films, adhesives, and part hollows change flame propagation, smoke density, and toxic-gas emission. When FR1 is used for battery enclosures, electrical brackets, or interior ducting, specimens should be cut from production-representative builds and tested in the final post-finished state. In many industrial qualification programs, property data from injection-molded plaques or unreinforced PA12 coupons cannot be substituted for data generated on the actual FR1 build orientation. The layer-line surface area, carbon-fiber orientation, and residual porosity from insufficient energy density may all reduce the measured flammability or mechanical values relative to the datasheet. Published data for this specific configuration are limited, so iterative single-line qualification builds are required before full-rate production.

    Process capability monitoring on the manufacturing floor should include powder moisture content, virgin/recycled blend ratio, part density, and dimensional X-Y-Z shrinkage. If any of these inputs shifts outside the qualified band, the UL 94 V-0 rating and mechanical properties cannot be assumed to remain valid because flame-retardant degradation and carbon-fiber length reduction are not visible on the part surface.

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