Products

ALM FR 106 Nylon 11 SLS Prototyping Polymer

    • Product Name: ALM FR 106 Nylon 11 SLS Prototyping Polymer
    • Factroy Site: Yudu County, Ganzhou, Jiangxi, China
    • Price Inquiry: admin@ascent-chem.com
    • Manufacturer: Ascent Petrochem Holdings Co., Limited
    • CONTACT NOW
    Specifications
    HS Code 735899
    Material ALM FR 106 Nylon 11 SLS Prototyping Polymer
    Tensile Strength 45 MPa
    Tensile Modulus 1.6 GPa
    Elongation At Break 30%
    Flexural Modulus 1.4 GPa
    Impact Strength Notched Charpy 11 kJ/m²
    Density 1.03 g/cm³
    Heat Deflection Temperature Hdt 1 8mpa 70 °C
    Melting Temperature 198 °C
    Flame Rating Ul94 V-0
    Dielectric Strength 25 kV/mm
    Surface Resistivity 10^13 ohm/sq
    Water Absorption 24h 0.9%

    As an accredited ALM FR 106 Nylon 11 SLS Prototyping Polymer factory, we enforce strict quality protocols—every batch undergoes rigorous testing to ensure consistent efficacy and safety standards.

    Packing & Storage
    Packing Packaged in a sealed 10 kg container to protect against moisture, ensuring dry, free-flowing ALM FR 106 Nylon 11 SLS powder.
    Container Loading (20′ FCL) One 20′ FCL container of ALM FR 106 Nylon 11 SLS Prototyping Polymer, securely packed and ready for shipment.
    Shipping ALM FR 106 Nylon 11 SLS Prototyping Polymer ships as non-hazardous powder in sealed, moisture-proof containers. Avoid static ignition and store in cool, dry conditions. Standard ground or air freight is suitable. Ensure proper labeling and handling to prevent dust dispersion. Approximately 50 words.
    Storage Store ALM FR 106 Nylon 11 SLS Prototyping Polymer in its original, tightly sealed container in a cool, dry, well-ventilated area. Protect from moisture, direct sunlight, and excessive heat. Keep away from ignition sources and incompatible materials. Use desiccant if needed, and reseal promptly after use to maintain powder flowability and performance.
    Shelf Life Shelf life is 12 months from manufacture when stored unopened in a cool, dry place.
    Application of ALM FR 106 Nylon 11 SLS Prototyping Polymer

    Series production of cabin air return grilles for regional aircraft has been evaluated using ALM FR 106 Nylon 11 SLS prototyping polymer where the flame exposure requirement is derived from 14 CFR 25.853(a), the vertical Bunsen burner test using a 12-second ignition source and a 2.0 mm thick specimen. The build is carried out on an open-platform SLS machine equipped with a 100 W CO₂ laser and a layer thickness of 0.10 mm; the powder bed surface temperature is maintained within the sintering window typical for polyamide 11, and the beam speed is adjusted to achieve fully dense walls without secondary melt at the downskin. A virgin-to-recycled powder refresh ratio of 70:30 by weight is used for first-article prototypes, while lower virgin fractions down to 50:50 may be screened for dimensional fit checks only if the melt volume-flow rate measured to ISO 1133-1:2022 remains within the supplier-defined control band. After depowdering, the parts are bead-blasted at 3 bar using 100 μm glass beads, then conditioned at 23°C and 50% relative humidity for 40 hours according to ISO 291 before any flame testing, since moisture uptake alters afterflame time and drip behaviour. The terminal prototype components are air return grilles, avionics cooling plenum covers, and low-pressure cabin air duct segments. Because published data for this specific grade is limited, every new powder lot is also verified using ASTM D638-14 Type IV specimens built in the same build chamber and compared against the supplier baseline for tensile strength and elongation at break.

    What Limits the Sintering Window When Recycled FR Polyamide 11 Feeds Rail Interior Builds?

    In rail vehicle interior prototyping, flame-retardant polyamide 11 parts such as seat back shells, armrest carriers, and side wall close-out panels are built under EN 45545-2 hazard level conditions. The sintering window narrows as the recycled powder fraction increases because the flame-retardant additive package, which may be phosphorus-based or melamine-based depending on the supplier formulation, can shift the onset of melt crystallization and reduce the temperature interval between bed melting and part growth on a 100 W CO₂ laser machine. The fresh powder fraction is therefore controlled by measuring the melt volume-flow rate to ISO 1133-1:2022 at 235°C with a 2.16 kg load; when the MVR exceeds the virgin powder reference by more than the supplier-controlled percentage, the recycled powder fraction is capped at 30 wt% or the build is re-charged with 100% virgin powder for the next job. A part bed surface temperature gradient of more than ±2°C from the centre to the edge of an EOS P396 or equivalent open-platform SLS machine has been observed to produce orange peel and undesirable growth on thin vertical walls. Smoke density and toxic gas emission are evaluated to ISO 5659-2 and NF X 70-100 when rail component certification is planned; published data for this specific grade is limited, so the prototype is not considered a compliance demonstration without separate coupon testing. The terminal components are installed only as functional mock-ups, and production mould release is withheld until the complete fire performance matrix has been repeated on injection-moulded plaques.

    Test standardConditionTerminal prototype componentReason for inclusion
    14 CFR 25.853(a)Vertical Bunsen burner, 12 s ignition, 2.0 mmCabin air return grilleAircraft interior fire performance screening
    EN 45545-2Heat release, smoke density, gas toxicitySeat back shellRail interior fire safety compliance
    IEC 60695-11-10Vertical flame, 3.0 mm plaqueElectrical enclosure coverUL 94 V-0 pre-compliance screening
    ISO 1133-1:2022235°C, 2.16 kgPowder lot controlMelt volume-flow rate and recyclate acceptance
    ASTM D638-14Type IV, 5 mm/minMechanical validation specimensTensile strength and elongation baseline
    ISO 75-2:20131.8 MPa, 120°C/hUnder-hood duct prototypeHeat deflection temperature screening

    Fuel Quick-Connector Prototype Chemistry and Dimensional Stability

    The substitution of SLS prototype thermoplastics in fuel vapour management components requires chemical exposure data before any injection mould tooling release. ALM FR 106 Nylon 11 SLS prototyping polymer is used for SAE J2044-style quick connectors, evaporative canister mounting brackets, and fuel rail retainers because the long-chain polyamide backbone provides low moisture absorption relative to PA6 and PA66, measured to ISO 62 after 24 hours of water immersion. Dimensional stability is not assumed; green parts are built at a layer thickness of 0.10 mm on a 3D Systems ProX SLS 6100 or similar machine, then annealed in a convection oven at 150°C for 2 hours to reduce residual stress before measuring key dimensions against the CAD model. Powder refresh ratio is set at 60:40 virgin-to-recycled for general mechanical parts, but 100% virgin powder is specified for quick-connector bodies where any microvoids from degraded recyclate reduce pressure retention. Chemical resistance is screened using ASTM D543 by immersion in ASTM Reference Fuel C at 60°C for 70 hours; the mass change and tensile retention are recorded, but published data for this exact grade is limited. Terminal prototypes are clipped into production nylon 12 fuel lines and subjected to 5 bar pneumatic leak checks using a mass spectrometer leak detector calibrated to helium leak rates below 1×10⁻⁶ mbar·L/s. Stainless steel quick-connector locking tabs are not substituted with SLS polymer because creep at the retention barb may occur under sustained fuel line pressure at under-hood temperatures.

    For electrical enclosure prototypes evaluated against UL 94 V-0 at a final wall thickness of 3.0 mm, the SLS build density and wall section uniformity determine the flame performance before any injection mould tooling is cut. ALM FR 106 Nylon 11 SLS prototyping polymer is processed with a 0.10 mm layer thickness and a 100 W CO₂ laser, and the build chamber is held at the lower end of the PA11 sintering window to prevent secondary melt on thin ribs and snap-fit features. The vertical burn test is performed according to IEC 60695-11-10 on specimens cut from flat plaques built in both X-Y and Z orientations; specimens are conditioned for 48 hours at 23°C and 50% relative humidity per ISO 291. A powder refresh ratio of 70:30 virgin-to-recycled by weight is used for early electrical enclosure iterations, and the used powder is sieved through a 200 μm mesh to remove agglomerates before reuse. Terminal components include low-voltage junction box covers, battery management system mounting brackets, and industrial sensor housings. Because flame-retardant additives may migrate to the surface during prolonged exposure to elevated humidity, parts intended for IEC 60529 ingress protection are sealed with a non-amine-based conformal coating; amine-based coatings are avoided due to potential premature crosslinking at the surface. Material compliance documentation for EU RoHS 2011/65/EU and the REACH SVHC candidate list should be obtained from the supplier before production, as the flame-retardant additive package may contain regulated substances that require declaration in finished electrical equipment.

    Heat distortion temperature alone does not predict under-hood prototype performance

    Heat deflection temperature measured to ISO 75-2:2013 at 1.8 MPa and 120°C/h gives an initial screening value, but under-hood air intake duct prototypes built from ALM FR 106 Nylon 11 SLS prototyping polymer are also aged in hot air at 120°C for 500 hours to reveal oxidative embrittlement. The test specimens are exposed in a forced-air convection oven with an air change rate of 10 per hour, and tensile properties are measured to ASTM D638-14 before and after aging. A 100 W CO₂ laser system with a layer thickness of 0.10 mm is used; the parts are built with 30% virgin powder and 70% recycled powder for initial fit checks, but after aging results show tensile strength retention below the supplier-defined limit relative to unaged material, the powder refresh ratio is raised to 50:50 or the part is rebuilt using 100% virgin powder. The terminal components are intercooler end cap prototypes, crankcase ventilation tubes, and charge-air duct segments for turbocharged engine compartments. Dimensional change after oil mist exposure is checked to ISO 175 by immersion in IRM 903 oil at 100°C for 70 hours. Published data for this specific grade is limited, so no injection mould tooling is released from the SLS prototype alone, and the prototype is restricted to engine bay packaging studies and short-duration thermal cycling trials.

    When a Functional Seal Must Withstand Prolonged Oil Immersion at 110°C

    Oil-immersion trials for polyamide 11 SLS parts are typically conducted in synthetic ester-based hydraulic fluids at 110°C for 1000 hours when the terminal component is a static seal carrier or connector protector for downhole tools. ALM FR 106 Nylon 11 SLS prototyping polymer is built in a high-yield orientation with a layer thickness of 0.10 mm using a 100 W CO₂ laser, and the powder refresh ratio is initially set at 100% virgin for any part that will contact high-temperature oil, because recycled powder introduces carbonyl groups that lower hydrolytic resistance. Dimensional change is measured to ISO 175 after immersion in IRM 902 oil at 110°C; the acceptance criterion is not based on the prototype alone, and published data for this specific grade is limited. The terminal parts are custom connector protectors, thread protection caps, and static seal carriers used in oil and gas downhole tool prototypes. Chlorinated solvents and strong acids are excluded from cleaning programmes because the flame-retardant additive package may be attacked, and parts are dried at 80°C for 24 hours before oil immersion to remove moisture that could increase hydrolysis. A pre-drying step is also applied when the ambient relative humidity exceeds 60% at powder loading, and the powder is never processed from a cold hopper into a heated build chamber because condensation on the particle surface causes inconsistent energy absorption at the laser spot.

    Free Quote

    Competitive ALM FR 106 Nylon 11 SLS Prototyping Polymer prices that fit your budget—flexible terms and customized quotes for every order.

    For samples, pricing, or more information, please contact us at +8618136850665 or mail to admin@ascent-chem.com.

    We will respond to you as soon as possible.

    Tel: +8618136850665

    Email: admin@ascent-chem.com

    Inquiry

    Get Free Quote of Ascent Petrochem Holdings Co., Limited

    Flexible payment, competitive price, premium service - Inquire now!

    Certification & Compliance
    More Introduction

    ALM FR 106 Nylon 11 SLS Prototyping Polymer is a halogen-free flame-retardant polyamide 11 powder developed for polymer laser sintering platforms operating at 10.6 µm CO₂ wavelengths. The material is based on an 11-aminoundecanoic acid monomer backbone and incorporates a phosphorus–nitrogen flame-retardant package. It is not dependent on brominated or chlorinated additives for its flammability rating. Typical output geometries include cabin air duct sections, electrical connector housings, seating support frames, and wiring retention clips with wall thicknesses between 1.5 mm and 3.0 mm.

    Because laser-sintered components are inherently anisotropic, mechanical response differs between XY and Z orientations. The XY plane generally exhibits higher tensile strength and elongation than the Z direction, where incomplete interlayer coalescence limits load transfer. On production-scale systems with 30 W CO₂ lasers and 0.10 mm layer thickness, incident energy densities between 30 J/mm³ and 45 J/mm³ are typically used. Scan spacing is often reduced from 0.20 mm to 0.15 mm when Z-direction strength is a design requirement. The dispersed flame-retardant filler raises melt viscosity relative to unfilled nylon 11, so part-bed setpoints are commonly maintained between 170 °C and 178 °C, with the feed bed held 20–30 °C lower to preserve powder flow. When powder refresh drops below 30% virgin addition, surface finish and elongation at break degrade measurably on repeated builds.

    What Limits the Laser Sintering Window of This Flame-Retardant Polyamide 11?

    The sintering window is governed by the separation between the melting endotherm and the non-isothermal crystallization exotherm. Differential scanning calorimetry at 10 °C/min for unfilled nylon 11 generally places the melting peak near 186–190 °C and crystallization onset near 152–156 °C. The flame-retardant additive in FR 106 can act as a heterogeneous nucleation agent and raise crystallization onset by several degrees, tightening the available isothermal hold range. If the part-bed temperature is too high, the powder charge oxidizes, darkens, and can lose flowability; if it is too low, initial layers curl and parts detach from the build plate. Operators frequently offset this behavior by raising the part-bed temperature 5–8 °C above the unfilled nylon 11 baseline. Published data for this specific configuration is limited; machine-specific thermal validation remains mandatory for flight or transit production.

    Thermogravimetric analysis under nitrogen at 10 °C/min typically records initial decomposition near 320 °C for the compounded material, with residual char fraction above 20% at 700 °C. The base polyamide 11 portion decomposes almost completely between 450 °C and 500 °C under the same conditions. The retained carbonaceous char is significant in flame exposure because it slows fuel release from the polymer melt. This char-formation mechanism distinguishes halogen-free phosphorus-based systems from brominated systems that act primarily through gas-phase radical quenching.

    Ignition Response and Smoke Emission Compliance in Regulated Interior Applications

    Flame resistance is not a single property; it is evaluated across ignition, afterflame time, burn length, and smoke density. Thin plaques produced from FR 106 are commonly tested under 14 CFR 25.853(a)(1)(i) with a 12 s vertical flame and a 60 s post-exposure observation window. Acceptance criteria require an average afterflame time not exceeding 15 s, an average drip extinguishing time not exceeding 5 s, and an average burn length not exceeding 203 mm. The halogen-free formulation reduces acid gas generation relative to brominated flame-retardant PA12 grades, but smoke density under ASTM E662 remains a separate test that depends on part thickness, surface finish, and applied sealant layers. Published data for this specific configuration is limited; OEM-level validation should use production-representative wall thickness and build orientation.

    The representative values below are drawn from laser sintering datasheets for flame-retardant nylon 11 grades and should be treated as nominal, not design allowables. Specimens are laser-sintered in XY orientation and conditioned at 23 °C and 50% RH before testing.

    PropertyMethodNominal Value
    Tensile strengthASTM D638-1446 MPa
    Tensile modulusASTM D638-141600 MPa
    Elongation at breakASTM D638-148%
    Flexural strengthASTM D790-1758 MPa
    Flexural modulusASTM D790-171300 MPa
    Notched Izod impactASTM D256-10e132 J/m
    Heat deflection temperature at 0.45 MPaASTM D648-18160 °C
    DensityASTM D792-201.05 g/cm³

    For thin-wall sections below 1.0 mm, flammability rating and tensile properties can shift because of incomplete interlayer healing. The flame-retardant rating is thickness-dependent; V-0 is typically reported at 3.0 mm, while lower thicknesses require part-specific verification. Sharp internal radii below 0.5 mm should be avoided in load-bearing bosses and snap features because the dispersed flame-retardant filler raises notch sensitivity.

    Relative to unfilled nylon 11, ALM FR 106 trades ductility for flame resistance. In Z orientation, tensile strength is typically 60–80% of the XY value, and notched impact may be 20–40% lower than unfilled nylon 11 because the flame-retardant particles act as stress concentrators at layer interfaces. Compared with PA12-based flame-retardant SLS powders, the nylon 11 backbone shows lower water uptake. A 24 h immersion test under ISO 62 places PA11 formulations below 0.4%, whereas PA12 grades can exceed 1.0%. This difference is relevant in humid cabins, lavatory modules, and under-floor service environments where dimensional expansion must remain limited. Relative to polycarbonate and PBT, the PA11 structure retains better low-temperature impact response, but the flame-retardant content slightly reduces that advantage.

    When Low-Temperature Ductility Governs Material Selection over PBT and Polycarbonate

    Environmental control ducting and wire management channels operating at -40 °C impose impact and flexural requirements that polycarbonate and PBT often meet only with glass fiber or rubber modification. Nylon 11 retains segmental mobility at low temperatures because its long aliphatic chain delays the beta-relaxation peak. In FR 106, the phosphorus–nitrogen filler partially masks this behavior; notch sensitivity increases and designers should radius bosses, lugs, and clip roots. Low-temperature impact screening under ASTM D256 and dynamic mechanical analysis under ASTM D7028 are typical for cabin air duct replacements. Parts tested in Z orientation may show larger scatter than XY parts because layer interfaces act as low-energy crack paths.

    Moisture is a defined processing boundary. Although polyamide 11 absorbs less water than polyamide 12, the flame-retardant component is hygroscopic. If powder is exposed to relative humidity above 60%, pre-drying at 80 °C for 4–6 h in a desiccant dryer is required. Laser spatter, part-bed non-uniformity, and surface specking are observed when free moisture content exceeds approximately 0.3 wt%. Processors should avoid direct contact with strong oxidizers, strong acids, and strong bases at elevated temperature. The phosphorus-containing flame-retardant package may interact with amine-based post-cure systems; no published compatibility matrix exists for all solvent-based sealants.

    Increasing laser energy density improves Z-direction strength but can degrade the flame-retardant additive. The phosphorus-containing species may undergo thermal decomposition if the melt pool exceeds 350 °C for extended periods, reducing the effectiveness of the intumescent char. This creates a process conflict: the optimum energy density for mechanical interlayer fusion in thick sections may not coincide with the optimum for flame-retardant retention. On production lines the practical compromise is frequently an energy density between 30 J/mm³ and 38 J/mm³ for 0.10 mm layers, coupled with controlled scan counts. Thin walls may require reduced power to avoid thermal overshoot.

    Batch-to-batch variance of flame-retardant dispersion can affect both color and flame test results. Incoming powder should be checked for melt flow rate under ISO 1133-1:2022 and for residual moisture by Karl Fischer titration. When the melt flow rate of a used powder blend falls below 0.8 of virgin or exceeds 1.2 of virgin, the resulting parts show altered surface roughness and variable burn length. Granulometry should be verified by laser diffraction; a median particle size outside 45–65 µm may require recoating parameter adjustment.

    Post-Processing Constraints for Dyeing, Machining, and Environmental Sealing

    Dye uptake is lower than that of unfilled PA12 because the dispersed flame-retardant phase limits dye penetration in the outer 100–200 µm surface layer. Acid dye baths at 80–90 °C require extended immersion and produce muted colors; chromatic variance across a build can be influenced by powder refresh and part density. Drilling and tapping are possible with sharp carbide tooling, but spindle speeds above 3000 rpm can soften the matrix and produce melted chips around tapped holes. Dry bead blasting at pressures below 4 bar is used before solvent or paint application to prevent marbled surfaces. Epoxy and polyurethane topcoats are commonly applied for aesthetic or sealing purposes; their effect on flame performance must be retested because the coating can change drip behavior and burn length.

    The term halogen-free is not equivalent to smoke-free. Brominated flame retardants often operate in the gas phase, disrupting radical chains but producing hydrogen halide gas under combustion. The phosphorus–nitrogen system in FR 106 is intumescent and forms a solid carbonaceous char with lower acid gas release, but smoke density can remain significant. This distinction is relevant in confined cabins where visibility and acid-induced corrosion are considered. Brominated systems may achieve V-0 at lower loading and with better mechanical retention; however, environmental and occupational restrictions on brominated styrenes and antimony trioxide have driven adoption of halogen-free systems.

    Test FrameworkCondition or TitleTarget Component Class
    14 CFR 25.853(a)12 s vertical, 60 s observation, 203 mm burn lengthCabin interior panels, air ducting
    UL 94V-0 at 3.0 mmElectrical enclosures, connector housings
    ASTM E662Smoke density, non-flaming and flamingTransit interiors, aircraft seating
    ASTM D648-18Heat deflection temperature at 0.45 MPaUpper service-temperature screening
    ISO 1133-1:2022Melt flow rate ratio, powder aging controlIn-process powder certification
    Top