| HS Code | 956501 |
| Product | ALM PA 614-GS Filled Nylon 12 Prototyping Polymer |
| Base Material | Nylon 12 (PA12) |
| Filler Type | Glass-filled |
| Filler Content | 40% glass |
| Density | 1.30 g/cm³ |
| Tensile Strength | 40 MPa |
| Tensile Modulus | 2500 MPa |
| Elongation At Break | 5% |
| Flexural Modulus | 2300 MPa |
| Impact Strength Notched Izod | 3.5 kJ/m² |
| Heat Deflection Temperature 0 45 Mpa | 170 °C |
| Melting Point | 180 °C |
| Water Absorption 24 Hours | 0.4% |
As an accredited ALM PA 614-GS Filled Nylon 12 Prototyping Polymer factory, we enforce strict quality protocols—every batch undergoes rigorous testing to ensure consistent efficacy and safety standards.
| Packing | Supplied in sealed, moisture-proof 10 kg containers to prevent humidity absorption and ensure optimal SLS printing performance. |
| Container Loading (20′ FCL) | ALM PA 614-GS Filled Nylon 12 Prototyping Polymer ships in a 20′ FCL, palletized in sealed bags, ensuring secure, efficient transport. |
| Shipping | ALM PA 614-GS is a fine nylon powder requiring moisture-proof, static-safe packaging. Ship in sealed containers with desiccant, avoiding exposure to humidity. Handle gently to prevent dust generation. Not classified as hazardous, but use grounded equipment and protective gear during transit. Ensure proper labeling and temperature-controlled conditions to preserve material integrity. |
| Storage | Store ALM PA 614-GS Filled Nylon 12 Prototyping Polymer in its original, tightly sealed container in a cool, dry, well-ventilated area, away from direct sunlight, heat sources, and ignition sources. Keep the powder dry, as moisture degrades performance. Avoid airborne dust generation, and use appropriate PPE when handling. |
| Shelf Life | Shelf life is 12 months when stored sealed in a cool, dry environment; protect from moisture to maintain material integrity. |
ALM PA 614-GS is a nylon 12 powder charged with 40 wt% spherical glass filler and processed on CO₂ laser powder bed fusion platforms operating at 10.6 µm. The powder must be dried to less than 0.1% residual moisture by Karl Fischer titration before loading into heated feed hoppers. The density difference between the glass filler, at approximately 2.4 g/cm³, and nylon 12, at approximately 1.01 g/cm³, creates a sedimentation gradient in the feed system. Machine parameter sets are therefore stable only when hopper agitation and powder recirculation maintain the bulk density specified on the supplier lot certificate. A resin-rich powder bed near the recoater blade produces first-layer shrinkage that differs from the filled-material specification and can create a warped reference surface. Additional glass spheres should not be dry-blended into reclaimed powder; the supplier’s melt-compounded and cryogenically ground particle distribution controls both laser absorption and melt pool viscosity. For electronics enclosure applications, the supplied powder is evaluated under EU REACH Article 33 duties and RoHS Directive 2011/65/EU Annex II because the glass filler may contain trace metals that differ by lot.
| Test method | Condition applied | Data output used in qualification |
|---|---|---|
| ISO 527-2:2012 | 23°C, 50% RH, 5 mm/min | Tensile modulus and elongation at break in X/Y and Z directions |
| ISO 178:2019 | 23°C, 2 mm/min | Flexural modulus for fixture and bracket deflection calculations |
| ISO 75-2:2013 Method A | 1.82 MPa | Heat deflection temperature for underhood and tooling limits |
| ASTM E831-19 | −40°C to 120°C | Coefficient of linear thermal expansion for flange mismatch analysis |
| ISO 1183-1:2019 | Archimedes procedure | Apparent density and internal void estimation |
| ISO 180:2019 | Notched Izod, 23°C | Impact response for snap-fit and bracket failure risk |
Underhood HVAC prototypes produced from ALM PA 614-GS are normally evaluated with wall sections between 1.8 mm and 3.0 mm; thinner walls reduce the energy absorbed before crack initiation when notched features are present. Coupons printed in the Z orientation and conditioned according to ISO 291:2008 yield tensile modulus values in the 3,000–4,200 MPa range under ISO 527-2:2012, while elongation at break remains between 2% and 5% depending on scan strategy and energy input. The glass spheres reduce the coefficient of linear thermal expansion to roughly 70–90 µm/m·K in the X/Y plane as measured by ASTM E831-19, whereas unfilled PA 12 laser-sintering grades commonly fall between 110 µm/m·K and 120 µm/m·K. This reduction is relevant when the duct is bolted to an aluminum flange, but it creates a differential against polypropylene quick connectors that can loosen clamp seals after repeated thermal cycles from −40°C to 135°C according to ISO 16750-4:2010. The powder bed temperature must be maintained between 168°C and 176°C, and the laser energy density should be held between 60 mJ/mm² and 80 mJ/mm². Energy input below 55 mJ/mm² creates interlayer void contents above 2% in micro-CT scans, while energy input above 90 mJ/mm² discolors the nylon matrix and reduces ductile response through oxidative chain scission. After the build, the parts remain buried in the powder cake for at least 8 h of controlled cooling to limit Z-axis curl. Terminal functional prototypes include charge-air cooler ducts, HVAC drain spigots, and resonance chambers. Published data for this specific configuration is limited for full OEM durability sign-off; the material is therefore used for geometry validation, airflow testing, and thermal mapping rather than production service parts.
Aerospace environmental control system test rigs require floor-mounted duct segments with integrated flanges and static pressure tap bosses that are assembled and disassembled repeatedly. The primary process conflict in this configuration is not the stiffness of PA 614-GS but the width of the usable laser energy density window. Because the spherical glass filler does not melt, it functions as a dispersed heat sink within the nylon 12 melt pool. When energy input declines below approximately 50 mJ/mm², the PA 12 matrix between adjacent glass spheres cannot fully coalesce; the resulting interlayer porosity can be detected as a reduction in apparent density below 1.18 g/cm³ by ISO 1183-1:2019. Thin-wall sections of 1.0–1.5 mm become brittle, and Z-direction elongation at break can fall below 2% under ISO 527-2:2012, which leads to flange cracking when hose clamps are torqued to 2–3 N·m. Conversely, raising energy density above 85 mJ/mm² causes surface yellowing and a measurable loss in notched Izod impact by ISO 180:2019 through oxidative chain scission at the melt surface. The stable operating point is therefore a combination of scan spacing below 0.18 mm, layer thickness of 100–120 µm, powder bed temperature of 170–175°C, and laser power adjusted to keep sintered density within the supplier-lot reference band. Aerospace test rig components are sealed at flange faces with room-temperature silicone gaskets; the polyamide substrate is not exposed to hydraulic fluid or continuous relative humidity above 70% RH, because equilibrium moisture uptake above 1.5% depresses the glass transition and relaxes dimensional stability. Terminal parts include floor-mounted ECS duct segments, Pitot static boss adapters, and wind-tunnel fairing blanks used for ground-based aerodynamic characterization. Published data for this specific configuration is limited for aircraft interior certification; no 14 CFR 25.853 pass is inferred without lot-specific vertical burn testing.
Machining fixtures produced from PA 614-GS are selected for low-force CNC operations where an aluminum fixture would require multiple setups and where part geometry prevents efficient billet machining. The fixture is printed as a single body with internal ribs and cylindrical bores for hardened drill bushings; bushing bores are undersized by 0.10 mm and reamed in a secondary operation to an H7 tolerance according to ISO 286-2:2010. Because the material carries 40 wt% glass spheres, its surface resists indentation more effectively than unfilled PA 12 under localized clamp pressure; hardness is commonly reported between 75 Shore D and 80 Shore D by ASTM D2240-15. The operating boundary is set by hot cutting fluid: continuous exposure to cutting oil above 60°C can soften the nylon matrix and relax the bushing fit. Build orientation places the locating plane parallel to the X/Y axis to capture the lowest shrinkage, while vertical walls are allowed to deviate within ±0.25% of nominal dimension after conditioning for 24 h according to ASTM D618-21. The finished fixture aligns injection-molded PA 6 automotive clips during secondary drilling and degating, with locating repeatability checked by coordinate measuring machine over 1,000 clamp cycles. When clamping force exceeds 1.2 kN, the design adds stainless-steel load spreaders to prevent compressive creep in the sintered nylon matrix.
Insert cores and cavity plates fabricated from PA 614-GS have been evaluated in short-run injection molding for polyolefin and thermoplastic elastomer trials where melt temperature is held below 220°C and mold surface temperature is kept below 80°C. The limiting factor is not the powder bed fusion resolution but the creep modulus of the nylon 12 matrix under injection and clamp loading. At a tensile stress of 20 MPa and 60°C, the creep modulus measured by ISO 899-1:2003 may fall to 60–70% of the room-temperature value, which requires steel backup plates when cavity pressure exceeds 30 MPa. Mold inserts are dried to constant mass at 80°C for 24 h before assembly to remove absorbed moisture and stabilize core dimensions. The glass spheres reduce expansion enough that core shift is lower than that of unfilled PA 12 during polypropylene filling, but the inserts are not suitable for campaigns beyond 100–200 shots because gate-area erosion appears as surface divots under magnification. Terminal uses include overmolded TPE grips on hand tools, low-volume polypropylene living hinges, and packaging fixture prototypes in which conformal channels cannot be produced by drilling.
For low-volume uncrewed aerial system airframe brackets, the sintered surface of PA 614-GS accepts post-machined threads with a more controlled chip formation than unfilled PA 12 because the glass spheres induce brittle chip fracture. Threads tapped directly into sintered nylon sustain a pull-out force near 600–900 N for an M4 brass insert at 25°C when verified against insert supplier data; above that band, helicoil inserts are required. The application is limited to non-primary internal structure because Z-direction elongation at break can remain below 4% under ISO 527-2:2012, producing a sudden fracture mode that is not acceptable for crash-loaded airframe joints. In the X/Y orientation, tensile strength is commonly in the 40–50 MPa range, which is sufficient for gimbal mounts, antenna brackets, and electronics trays exposed to 60°C ground test. As-built surfaces are finished by light glass-bead blasting; the operation raises surface roughness Sa from about 8–12 µm to 14–18 µm and provides a more reproducible surface for two-part methacrylate adhesive bonding. The material should not be combined with amine-based epoxy hardeners without trial because unreacted amine can plasticize the nylon matrix and reduce hardness by more than 5 Shore D.
In packaging automation, vacuum cup adapters and gripper base plates are printed from PA 614-GS when an aluminum plate would require too many machining operations and when unfilled PA 12 shows excessive bowing across the plate surface. The filled grade is dimensionally checked against DIN 16742:2013; as-built features up to 300 mm can be held within ±0.35 mm after stabilization, while larger plates may deviate by ±0.5 mm because of powder bed thermal asymmetry from the recoater return stroke. Suction cups are mounted through countersunk holes fitted with ethylene-propylene rubber gaskets; the nylon matrix must not be exposed to chlorinated clean-in-place agents, which induce stress cracking behind the sealing face. Air lines are connected with push-to-connect fittings inserted into printed bosses; repeated insertion forces of 50–80 N are tolerated without creep because the glass spheres increase compressive stiffness. The component is applied in pick-and-place cells with payloads below 3 kg per cup cluster and ambient temperatures between 10°C and 45°C; beyond 45°C, the nylon matrix softens enough to reduce the stability of press-fit connections.
Non-sterile surgical instrument positioning guides are occasionally prototyped from PA 614-GS when the design requires dimensional stability under repeated autoclave-free enzymatic cleaning. The glass-filled nylon is not intended for patient contact; no ISO 10993-1:2018 biological evaluation should be inferred without additional surface validation. The fixture is limited to operating-room table adapters and tray alignment blocks that are wiped with 70% isopropanol. Because enzymatic detergents can plasticize nylon 12 surfaces, soak times are limited to 30 min at 25°C and rinsed immediately with deionized water.
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ALM PA 614-GS Filled Nylon 12 Prototyping Polymer is a glass-sphere-reinforced polyamide 12 powder developed for selective laser sintering. The product code denotes a PA 12 matrix combined with a spherical glass filler; manufacturer-published data place the filler loading at 40 wt% and the post-sintered part density at 1.28 g/cm³ when measured according to ISO 1183-1:2019. It is supplied as a free-flowing powder with a median particle size of 58 µm by laser diffraction using ISO 13320-1:2020 and a bulk density of 0.65 g/cm³. The grade is selected where higher stiffness, lower creep, and improved dimensional stability are required over unfilled PA 12, but where the lower strain-to-failure of the filled system remains acceptable for the prototype application.
The matrix is a semi-crystalline polyamide 12 with a melt peak near 187°C and a recrystallization exotherm near 148°C by differential scanning calorimetry at 10°C/min according to ASTM D3418-21. The glass filler is a spherical, silane-treated borosilicate composition with a particle diameter distribution controlled between 20 µm and 80 µm; the spherical morphology reduces anisotropy relative to glass-fiber-filled grades. Secondary electron microscopy of sintered fracture surfaces shows filler debonding at elongations above 3%, which limits ductility. The powder rheology is suitable for counter-rotating roller recoating systems; avalanche angle measured by rotating drum powder analyzers is typically 36° to 42° at 50% RH. Moisture uptake of the powder before sintering should remain below 0.1 wt%; otherwise part porosity increases.
During heating, the PA 12 matrix undergoes a melt transition that produces a rapid drop in melt viscosity. Capillary rheometry at 190°C under 2.16 kg load gives a melt flow index of 8 g/10 min to 12 g/10 min for the base resin, but the 40 wt% glass filler reduces overall melt flow and demands tighter laser power control. Laser sintering process logs from commercial systems equipped with 30 W to 100 W CO₂ lasers and 0.10 mm layer thickness show that the effective energy density must be held between 28 J/mm³ and 35 J/mm³. Below 28 J/mm³, the interlayer bond strength drops below 30 MPa in tensile tests conforming to ASTM D638-14. Above 35 J/mm³, surface gloss increases but impact strength degrades due to filler-matrix degradation and polyamide oxidation. Therefore, operator attention to scan speed, laser power, and beam offset is more critical for PA 614-GS than for unmodified PA 12.
The critical processing window for ALM PA 614-GS is narrower than for unfilled nylon 12. On a production laser sintering machine with heated pistons and a nitrogen-inertized build chamber, the part-bed set point is typically 170°C, with a tolerance of ±2°C. A deviation of -3°C from the lower set point depresses coalescence and produces lacy edges and delamination between 0.10 mm layers. A deviation of +4°C from the upper set point produces part growth, powder caking, and glass-filler aggregation at the melt surface. When the residual oxygen in the chamber exceeds 1.5 vol%, yellowing and molecular weight degradation occur; therefore nitrogen flow rates should be adjusted to maintain oxygen below 1.0 vol%. Layer adhesion is also sensitive to cool-down rate. Removing parts from the build chamber at a part-bed temperature above 80°C increases warpage; a controlled cool-down of 6 h to 8 h before breakout is required for parts with wall thickness below 3 mm.
The following values are typical for laser-sintered specimens conditioned at 23°C and 50% RH; they are not specification limits.
| Property | Typical Value | Test Method |
|---|---|---|
| Filler loading | 40 wt% | Thermogravimetric analysis, supplier method |
| Sintered part density | 1.28 g/cm³ | ISO 1183-1:2019 |
| Tensile strength, XY | 41 MPa | ASTM D638-14 |
| Tensile modulus, XY | 3400 MPa | ASTM D638-14 |
| Elongation at break, XY | 3% | ASTM D638-14 |
| Flexural modulus | 3200 MPa | ASTM D790-17 |
| Notched Izod impact | 27 J/m | ASTM D256-10 |
| Heat deflection temperature, 0.45 MPa | 170°C | ASTM D648-16 |
| Heat deflection temperature, 1.82 MPa | 95°C | ASTM D648-16 |
Application records from service bureaus place PA 614-GS in low-to-moderate load tooling, robotic end-effectors, gauge bodies, and wind-tunnel test articles. The grade is selected when unfilled PA 12 prototypes exhibit excessive deflection under load; the increase in flexural modulus from 1700 MPa to 3200 MPa permits thinner wall sections without increasing part mass beyond the density difference. However, the reduction in notched Izod impact to 27 J/m excludes snap-fit designs and thin living hinges. Parts exposed to continuous service above 95°C under 1.82 MPa flexural stress should be derated because the glass-filled PA 12 system approaches its heat deflection threshold. Published data for long-term creep under combined thermal and mechanical loading in this specific glass-sphere-filled configuration is limited; therefore, prototype qualification should include end-use creep testing under ISO 899-1:2018 rather than relying solely on short-term modulus data.
Substitution of unfilled PA 12 with ALM PA 614-GS changes both processing and part performance. Tensile modulus rises from approximately 1700 MPa to 3400 MPa under ASTM D638-14, while elongation at break falls from 15% to 3%. The glass-sphere filler lowers isotropic shrinkage; linear shrinkage in the XY plane is typically 0.35% to 0.50% after a 24 h ambient stabilization period, compared with 0.8% to 1.2% for unfilled PA 12. Dimensional accuracy in holes and bosses improves, but the filled powder is abrasive to recoater blades and increases wear on vacuum lines; production sites report shortened blade replacement intervals when running filled grades, although published data for this specific configuration is limited. When comparing to glass-fiber-filled PA 12, the spherical filler yields lower strength anisotropy between XY and Z directions; however, Z-direction tensile strength remains approximately 60% of XY strength. The product is therefore positioned between unfilled PA 12 and glass-fiber-filled PA 12 for stiffness and isotropy.
Polyamide 12 absorbs atmospheric moisture; the filled grade reaches an equilibrium moisture content of 0.8% at 23°C and 50% RH. Sintering moist powder produces steam-induced porosity, increases part roughness, and can reduce tensile strength by 10% to 15%. Pre-drying in a circulating desiccant dryer at 80°C for 4 h to 6 h is required when powder moisture exceeds 0.1%; vacuum drying at 70°C for 8 h is an alternative. Do not exceed 90°C during drying because the glass-sphere/PA 12 powder can fuse and reduce recoater flow. After drying, the powder should be returned to a sealed container with desiccant or transferred to a nitrogen-purged hopper. Long-term storage at relative humidity above 60% requires re-qualification of powder flow, avalanche angle, and part density. Avoid alkaline cleaning agents with pH above 10 and strong mineral acids; the glass filler is attacked by hydrofluoric acid and prolonged exposure to hot concentrated alkali.
| Requirement | Applicable Standard / Clause | Validation Boundary |
|---|---|---|
| RoHS substance restrictions | Directive 2011/65/EU Annex II | Pb 0.1 wt%, Hg 0.1 wt%, Cd 0.01 wt%, Cr(VI) 0.1 wt% |
| REACH candidate list communication | EC 1907/2006 Article 33 | SVHC above 0.1 wt% at article level |
| US food contact, nylon 12 | FDA 21 CFR 177.1500 | End-use migration testing required |
| EU food contact, overall migration | EU 10/2011 Annex I | OML 10 mg/dm² |
| Tensile testing | ASTM D638-14 | Specimen geometry and conditioning per standard |
| Flexural testing | ASTM D790-17 | 1.3 mm/min crosshead rate |
| Heat deflection temperature | ASTM D648-16 | 0.45 MPa and 1.82 MPa |
Batch-to-batch variation in filler distribution and powder particle size remains a key processing variable. Incoming powder inspection should include laser-diffraction particle size analysis under ISO 13320-1:2020, melt flow rate according to ISO 1133-1:2022 at 190°C and 2.16 kg load, and bulk density by ASTM D1895-17 Method A. When recycled powder is blended with virgin material, the recommended refresh ratio is 30% virgin to 70% recycled, but this must be adjusted based on measured melt flow index and part porosity. Production logs on laser sintering machines with 0.10 mm layer thickness show that recycled fraction above 70% lowers tensile strength by approximately 5% and increases dimensional scatter. Operators should track part-bed temperature uniformity across the build area; a spread greater than 3°C across the piston is associated with density gradients and should be corrected before production. The product should not be blended with glass-fiber-filled grades because differences in melting behavior and filler aspect ratio create inconsistent coalescence and void patterns.