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PlastiComp Complet LCF30-PA12 Nylon 12, 30% Long Carbon Fiber Content

    • Product Name: PlastiComp Complet LCF30-PA12 Nylon 12, 30% Long Carbon Fiber Content
    • 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 103137
    Density 1.23 g/cm³
    Tensile Strength 220 MPa
    Tensile Modulus 18 GPa
    Flexural Strength 300 MPa
    Flexural Modulus 16 GPa
    Elongation At Break 1.2%
    Notched Izod Impact 120 J/m
    Heat Deflection Temperature At 1 82 Mpa 170 °C
    Melting Point 178 °C
    Volume Resistivity 1000 ohm·cm
    Moisture Absorption 24h 0.30%

    As an accredited PlastiComp Complet LCF30-PA12 Nylon 12, 30% Long Carbon Fiber Content factory, we enforce strict quality protocols—every batch undergoes rigorous testing to ensure consistent efficacy and safety standards.

    Packing & Storage
    Packing Plastic composite pellets supplied in sealed moisture-proof bags, 25 kg per bag, preventing contamination and moisture absorption.
    Container Loading (20′ FCL) One 20-foot full container load of PlastiComp Complet LCF30-PA12 Nylon 12, containing 30% long carbon fiber, packed and shipped.
    Shipping Ship as an engineered thermoplastic composite in sealed, moisture-barrier bags with desiccant to prevent nylon degradation. Palletize and protect from physical damage, moisture, and static discharge. Ensure proper labeling for carbon-fiber content. Avoid open handling to minimize fiber dust. Transport in dry, ventilated containers, keeping away from ignition sources and incompatible chemicals.
    Storage Store PlastiComp Complet LCF30-PA12 in its original, sealed container in a cool, dry area away from direct sunlight, heat sources, and moisture. After opening, purge with dry air or nitrogen, reseal tightly, and use promptly. Avoid condensation and contamination. Keep containers off bare floors and away from incompatible chemicals to maintain low moisture content and optimal carbon fiber properties.
    Shelf Life Store in original sealed packaging, cool and dry. Shelf life is indefinite; dry before processing if moisture absorbed.
    Application of PlastiComp Complet LCF30-PA12 Nylon 12, 30% Long Carbon Fiber Content

    Where multirotor airframe arm-to-hub junction plates are specified, PlastiComp Complet LCF30-PA12 is introduced for mass reduction in secondary load-bearing structures that cannot accept metallic inserts. In primary load paths, only virgin material is injected; no regrind is permitted because retained fiber length distribution shifts below a critical threshold after one regrind cycle. Compliance for civil UAS structural prototypes is typically anchored to ASTM F3298-19 for airframe design verification, with material batch release requiring ASTM D638-14 tensile modulus and strength, ASTM D3763 high-speed puncture, and ASTM D648 heat distortion temperature. Restricted substance screening follows REACH SVHC and RoHS Directive 2011/65/EU Annex II. The 30% long carbon fiber content is maintained by weight-in-feed control on a low-shear reciprocating screw with 1.8:1 to 2.0:1 compression ratio; back pressure is held to 0.3–0.7 MPa to avoid fiber attrition. The compound is pre-dried at 80 °C for 4 h in a desiccant dryer with a dew point of ≤ −40 °C, and the melt temperature at the nozzle is held between 235 °C and 250 °C. Mold temperature is controlled at 65–80 °C through oil-heated channels. Hot runner systems, if used, require free-flow tips without dead zones because fiber accumulation at valve pin seats has been observed in production trials. Terminal parts include motor mount plates, landing gear saddle brackets, battery tray corner gussets, and antenna mast bases. Where carbon-filled thermoplastic is bolted directly to aluminum airframe members, a glass-reinforced PA12 or EPDM isolation layer is inserted to interrupt the galvanic couple because long carbon fibers are electrically conductive.

    What Limits Melt Front Convergence in Long-Fiber PA12 Charge-Air Duct Brackets?

    Underhood charge-air ducting and turbo intercooler bracket programs evaluate this compound when short glass PA66 parts show creep above 120 °C. The compounding ratio remains 30% long carbon fiber by weight in a PA12 matrix; if a flame-retardant package is requested, the fiber sizing and impact retention must be revalidated because acid-functional additives can reduce polyamide molecular weight during extended residence time above 250 °C. Compliance follows IATF 16949:2016 PPAP, with mechanical acceptance under ISO 527-2:2012, ISO 179-1/1eU:2010, and ASTM D648 heat deflection. Chemical exposure is screened under ASTM D543-21 using SAE 5W-30 oil, OAT coolant, and de-icing salt solution; long-term glycol contact above 105 °C remains an application boundary because PA12 hydrolysis accelerates under acidic degradation products. Drying uses a forced-air desiccant hopper set to 80 °C for 4 h, with moisture below 0.1% confirmed by ISO 15512 Method A. Melt temperature is held at 235–250 °C; mold temperature is held at 70–85 °C using oil-heated circuits. The critical process conflict is weld-line formation where melt fronts converge at an un-gated rib or metal insert hole. Production trials have shown that moving the gate from the boss edge to the flange edge alters weld-line tensile strength and shifts fiber orientation; moldflow simulation with a long-fiber orientation tensor and fiber breakage model is required before steel cutting. If flow front velocity exceeds the jetting threshold, surface defects and exposed fibers appear. Tooling is typically run on a hydraulic injection molding machine of 350–500 t clamp force when cavity count exceeds 2+2; the long carbon fiber reduces flow length, so wall sections below 2 mm are avoided. Terminal components include charge-air duct brackets, turbo inlet stays, intercooler end-cap carriers, and battery cooling plate frames. Regrind at 20 wt% is allowed in non-structural covers only; load-bearing engine bay components use 100% virgin material.

    Application zonePre-drying requirementMelt temperature at nozzleTool temperatureRegrind allowance
    UAS primary load path80 °C for 4 h, dew point ≤ −40 °C235–250 °C65–80 °C0%
    Underhood non-structural cover80 °C for 4 h, moisture ≤0.1%235–250 °C70–85 °C20 wt%
    Orthotic structural strut80 °C for 4 h, dew point ≤ −40 °C235–245 °C75–85 °C0%
    Subsea ROV non-pressure housing80 °C for 4 h, moisture ≤0.05%235–250 °C70–85 °C0%
    ESD end-of-arm tooling80 °C for 4 h, dew point ≤ −40 °C235–250 °C75–85 °C20 wt% non-critical
    Cycling pedal body80 °C for 4 h, moisture ≤0.1%235–245 °C70–80 °C0%

    Active ambulatory users generate cyclic bending loads on posterior struts, which has driven fabrication of ankle-foot orthosis components from LCF30-PA12 instead of titanium. The formulation is fixed at 30% long carbon fiber in PA12; no regrind is permitted because first-pass fiber length retention is necessary for fatigue resistance. Biocompatibility for external skin contact is documented under ISO 10993-5:2009 and ISO 10993-10:2010; structural validation follows ISO 10328:2016 for lower-limb prostheses and ISO 22523:2006 for orthotic components. If a colour masterbatch is added, the masterbatch carrier and pigments must also carry test documentation from the same ISO 10993 series. The pre-drying sequence is 80 °C for 4 h to a dew point of ≤ −40 °C; moisture content is verified by ISO 15512 Method A at ≤0.1%. Injection molding is performed with a 22:1 to 24:1 L/D low-shear screw, melt temperature 235–245 °C, mold temperature 75–85 °C, and back pressure 0.3–0.5 MPa. Ejection is configured for thick sections to avoid bending the hot part before the polymer has recrystallized. Post-molding annealing at 100 °C for 2 h in a circulating air oven is applied when residual stress reduction is required; published data for the effect of annealing on this exact carbon fiber PA12 configuration is limited. Terminal components include prosthetic socket frame struts, ankle-foot orthosis uprights, wheelchair camber axle inserts, and pediatric hip hinge bodies. Where continuous skin contact is expected, a second-shot medical TPU overmold or fabric liner is used because exposed long carbon fiber can cause skin irritation. Galvanic isolation from metal components is required when the orthotic strut attaches to titanium or stainless steel fasteners.

    Subsea ROV Manipulator Housings and Cathodic Disbondment Resistance

    Deepwater ROV tooling structural shells use LCF30-PA12 when the assembly must be non-magnetic and resistant to galvanic corrosion in seawater immersion. The material is limited to non-pressure-containing structural shells; any pressure-retaining use must be revalidated under API 17H:2019 or the applicable end-user pressure vessel code. The compound ratio is 30% long carbon fiber in PA12; no regrind is used for components exposed to seawater pressure cycling. Screening for sour hydrocarbon exposure is performed under NORSOK M-710, but published data for this specific configuration is limited, so qualification is component-specific. Seawater absorption is measured under ISO 62:2008; the carbon fiber network reduces volumetric swelling compared with unreinforced PA12, but differential swelling at machined edges can open microcracks if cutting coolant is not removed. Cathodic disbondment testing applies only where an outer coating is used; in such cases the coating system is evaluated under ISO 15711:2003 because the underlying carbon-filled PA12 is electrically conductive. Drying before molding is 80 °C for 4 h to a moisture target of ≤0.05%, verified by ISO 15512 Method A. Processing uses a low-compression screw of 1.9:1 to 2.1:1, nozzle melt temperature 235–250 °C, mold temperature 70–85 °C, and injection pressure limited to avoid fiber breakage at thin hinge features. Terminal components include ROV manipulator link shells, hydraulic valve covers, sonar mounting frames, and syntactic foam clamp inserts. Electrically conductive carbon fiber must be isolated from aluminum and magnesium mounts with glass-reinforced PA12 or EPDM bushings; otherwise the galvanic couple accelerates aluminum corrosion in oxygenated seawater. Machining of molded blanks requires carbide tooling with through-tool coolant; residual carbon dust must be removed from surfaces before assembly because conductive debris can bridge insulated connectors.

    When Electrostatic Dissipation and Dimensional Stability Govern End-of-Arm Tooling

    The 30% long carbon fiber network yields enough through-plane conductivity to remove static charge from vacuum grippers in automated packaging lines. Surface resistivity is measured on molded plaques per IEC 61340-2-3:2016; because resistivity varies with mold temperature, injection speed, and skin layer thickness, ESD qualification is performed at both 12% and 50% relative humidity, not only at 23 °C/50% RH. Compliance for ESD-protected areas follows IEC 61340-5-1:2016; mechanical acceptance uses ISO 527-1:2019/ISO 527-2:2012 and ISO 179-1/1eU:2010. Restricted substance documentation follows REACH and RoHS Directive 2011/65/EU Annex II. The compound is pre-dried at 80 °C for 4 h; the hopper must have a dew point of ≤ −40 °C. Melt temperature at the nozzle is 235–250 °C; mold temperature is 75–85 °C. Tooling plates and gripper bodies with wall thickness from 4 mm to 10 mm exhibit warpage if an unbalanced cooling layout is used; cooling circuits are therefore run with turbulent flow above a Reynolds number of 4000 and separate flowmeters per circuit. Regrind at 20 wt% is allowed only for non-critical covers and sensor brackets; virgin material is retained for load-bearing arm structures. Terminal components include palletizing end-effector frames, vision camera brackets, vacuum cup adapters, and robot tool changer housing shells.

    Cycling Pedal Bodies Require Impact Testing Before Cleat Retention Sign-Off

    Clipless pedal bodies and ski touring binding release levers are injection molded only after pre-drying at 80 °C for 4 h. The 30% long carbon fiber content raises cleat retention torque compared with unreinforced PA12, but component-level validation is required under ISO 4210-2:2015 pedal impact and fatigue clauses. A mold temperature of 70–80 °C is used to minimize surface fiber read-through. No regrind is used in impact-loaded pedal bodies; regrind at 20% is reserved for non-structural covers. Melt temperature is held at 235–245 °C. Terminal parts include pedal bodies, heel levers, and trekking pole lock housings.

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    Certification & Compliance
    More Introduction

    Specifying PlastiComp Complēt LCF30-PA12 requires recognition that the compound is a pultruded long-carbon-fibre-reinforced polyamide 12 containing a nominal fibre loading of 30% by weight. The reinforcement is not dispersed as short monofilaments; continuous carbon fibre tows are impregnated with the PA12 matrix, drawn, and pelletized to a fixed length, typically 11–13 mm. The fibre bundles remain oriented along the pellet axis and are liberated only during plasticating. Consequently, the final moulded part retains a fibre-length distribution whose number-average length is frequently reported in the 1–3 mm range when low-shear moulding conditions are used, whereas short-carbon-fibre compounds may drop below 0.5 mm. The matrix selection of PA12 rather than PA6 or PA66 is deliberate: the longer aliphatic chain reduces equilibrium moisture uptake, improves dimensional stability in humid environments, and provides resistance to aliphatic hydrocarbons, greases, and many automotive fluids. The trade-off is a lower melting range and lower continuous-use thermal ceiling than semi-aromatic or PA66-based compounds. Application contexts include structural brackets, robotic end-effectors, housings, dry-running gears, sporting goods, and orthotic or prosthetic components.

    Why Does Fibre Length Control the Onset of Fibre Fracture Versus Pull-Out?

    The reinforcing efficiency of carbon fibre in a PA12 matrix is governed by the critical fibre length. For a carbon-fibre/PA12 interface with an interfacial shear strength estimated at 20–35 MPa and a fibre tensile strength near 3.5–4.0 GPa, the critical transfer length is on the order of 0.3–0.6 mm. Fibres shorter than this threshold fail to reach their tensile strength before interfacial debonding; they are extracted from the matrix, and stiffness transfer is incomplete. In a short-carbon-fibre PA12 compound, final fibre lengths after injection moulding commonly fall below 0.5 mm, so the bond surface area is small and the fibre aspect ratio may approach the critical limit. Long-carbon-fibre pellets, by contrast, produce residual fibre lengths of 1–3 mm under moderate shear, exceeding the critical length by a factor of 2–6×. This shifts the dominant failure mechanism from interfacial pull-out to fibre tensile rupture, which raises tensile and flexural strength, increases stiffness retention at elevated temperature, and improves crack-propagation resistance. Impact tests show the effect most strongly in unnotched or low-triaxiality geometries, where the continuous-fibre network can distribute energy over a larger damage zone.

    Mechanical, Thermal, and Density Benchmarks Published for LCF30-PA12

    Representative lot-to-lot ranges for a dry-as-moulded state, as compiled from supplier data and independent LFT-PA12 reports, are shown in Table 1. Because fibre orientation, weld-line placement, and moulded fibre length alter results, the values should be treated as directional rather than minimum specifications. Tensile and flexural properties are sensitive to gate placement; the highest numbers are obtained in flow-aligned specimens, while cross-flow and weld-line specimens can exhibit retention losses above 30–50%. Density increases relative to unfilled PA12, and the carbon fibre substantially lowers linear thermal expansion along the fibre axis. The notched Charpy and Izod values should be interpreted in the context of fibre-induced anisotropy: the crack path in a notched specimen may run along the fibre-matrix interface, so notch sensitivity is higher than in unfilled PA12 even though unnotched energy absorption is improved.

    PropertyTypical rangeTest method
    Density1.13–1.16 g/cm³ISO 1183-1
    Tensile strength185–215 MPaISO 527-1/-2
    Tensile modulus18–22 GPaISO 527-1/-2
    Flexural strength280–330 MPaISO 178
    Flexural modulus16–20 GPaISO 178
    Notched Izod impact10–16 kJ/m²ISO 180/A
    Deflection temperature at 1.8 MPa160–175 °CISO 75-2/A
    Mould shrinkage, flow direction0.05–0.20%ISO 294-4

    Drying of Complēt LCF30-PA12 before processing is mandatory whenever the product has been exposed to ambient air for more than 1 h at relative humidity above 60%. A desiccant dryer with a dew point at or below −40 °C should be used, with an inlet air temperature of 80–90 °C for 4–6 h or until residual moisture is below 0.10% by Karl Fischer titration. Moisture above this threshold hydrolyzes the amide bonds during melt processing, which can reduce molecular weight and produce surface splay, gas marks, and a measurable loss of tensile elongation. The recommended melt-temperature window for long-carbon-fibre PA12 is 260–285 °C; residence time should not exceed 8–10 min to avoid thermal degradation of the matrix and carbon-fibre sizing. Mold temperatures between 80 °C and 100 °C are typically required to obtain good surface replication and to avoid prematurely freezing the flow front, which would entrap exposed fibres and create a rough surface finish. Use of a general-purpose high-compression screw with a short feed section can break fibres before the melt reaches the nozzle. A low-compression screw of 20:1–24:1 L/D with a compression ratio near 2:1–2.5:1, low back pressure of 0.3–0.7 MPa, and a free-flow nozzle orifice of at least 2.5 mm is preferable. Gate thickness and land length should be at least 60–70% of the nominal wall section; pin or tunnel gates introduce high shear and reduce final fibre length. Weld lines are a particular boundary condition: because long fibres tend to orient parallel to the weld line rather than across it, weld-line tensile strength can drop below 50–60% of the base flow-aligned value. If the part cannot be gated to avoid weld lines, the strength at the weld line must be considered the design-limiting property, not the datasheet strength.

    Filling behaviour differs from both unfilled PA12 and short-carbon-fibre grades. The presence of 30% long carbon fibre increases melt viscosity at low shear; minimum wall thickness below 1.5–2.0 mm can cause freeze-off before complete filling, especially at mold temperatures under 80 °C. Flow-length-to-wall-thickness ratios should be roughly 60–100:1 for short shots under typical pressures, compared with 150–250:1 for unfilled PA12. This is a rheological constraint, not a linear reduction. Hot-runner systems with small gates, sharp turns, or long residence time can damage fibres and are generally avoided; if hot runners are unavoidable, full-round or oval channels with diameters not less than 6 mm and gate diameters of 1.2–2.0 mm are used. Fibre breakage in the screw, runner, and gate consumes mechanical property margin. Moulds should be vented aggressively because carbon-filled PA12 can entrain gas from sizing decomposition and moisture; vent depth is typically 0.015–0.025 mm with land lengths of 0.5 mm.

    When Moisture, Chemical Resistance, and Electrical Conductivity Shift the Part Requirements

    Because the matrix is PA12, the compound has lower equilibrium moisture absorption than PA6 or PA66 grades. Saturation water uptake of unreinforced PA12 is approximately 1.5% under ISO 62 conditions; the 30% carbon fibre phase dilutes the hygroscopic polymer and reduces the macroscopic uptake to roughly 0.5–1.0% depending on laminate orientation and fibre-end wicking. This means dimensions and glass-transition-sensitive stiffness are more stable in humid air than with other aliphatic nylons; however, the compound is not a moisture barrier and should not be used as a sealing surface in continuous water contact without testing. The carbon reinforcement introduces appreciable electrical conductivity. Surface resistivity of long-carbon-fibre PA12 is typically in the semiconductive to conductive range, and the material cannot be regarded as an electrical insulator. This property may be beneficial for electrostatic dissipation or for components requiring a conductive path, but it also creates the risk of galvanic coupling when the plastic is mounted to a more noble metal in the presence of an electrolyte. Insulating bushings or isolation washers are required if the carbon-filled part is in contact with magnesium or uncoated aluminium in wet environments.

    The chemical resistance profile is dominated by the PA12 matrix, which is resistant to aliphatic hydrocarbons, diesel fuel, greases, hydraulic fluids, and zinc chloride solutions. Strong acids, strong oxidizing agents, phenols, and some chlorinated solvents are known to attack polyamide 12 and should be avoided. In fuel-contact applications, PA12 is used in tubing and connectors, but the long-fibre grade should not be assumed to meet permeability or extraction requirements without test data to SAE J2260 or equivalent. Immersion can also reduce fibre-matrix adhesion because water and polar solvents migrate along the interface; tensile strength in 50% relative humidity is therefore similar to dry values, but after prolonged hot-water ageing the fibre-matrix debonding can reduce transverse tensile properties by 20–40% relative to dry-as-moulded.

    Compared with unfilled PA12, Complēt LCF30-PA12 shifts the modulus from roughly 1.4–1.6 GPa to 18–22 GPa, an increase of more than an order of magnitude, while tensile elongation at break falls from typical ductile values above 50–200% to about 1.5–2.5%. The material therefore replaces ductile snap-fit geometries poorly but is appropriate for stiffness-dominated brackets, frames, and load-bearing housings that would otherwise require metal. Against a short-carbon-fibre PA12 compound, the long-fibre architecture typically preserves higher notched and unnotched impact energy at equal fibre weight fraction, reduces the drop in fatigue resistance under cyclic loading, and improves creep resistance. The difference is most visible at low temperatures, where short-fibre compounds lose matrix ductility and long-fibre networks still resist crack extension. Against long-glass-fibre PA12, the carbon-fibre grade has higher tensile and flexural modulus at similar fibre volume fraction, lower density, and lower linear thermal expansion; however, it is also electrically conductive, more costly, and more abrasive to screws, barrels, and moulds. The grade should not be specified as a direct drop-in replacement for a long-glass-fibre part without reviewing tooling wear, gate sizing, and electrical isolation. In rotating or sliding parts, carbon fibre provides self-lubricating and wear-reducing behaviour relative to glass-filled PA12, but the wear surface will generate conductive dust that may interfere with adjacent electronics. These contrasts define the selection boundary: Complēt LCF30-PA12 is most useful where specific stiffness, fatigue resistance, dimensional stability, and chemical exposure coexist, and least suitable where weld-line strength, electrical insulation, low abrasive tool wear, or high ductility govern the design.

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