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GEHR Plastics Ultem AM1010F FILAMENT (PEI) Filament for 3D printing

    • Название продукта: GEHR Plastics Ultem AM1010F FILAMENT (PEI) Filament for 3D printing
    • 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 684129

    Будучи аккредитованным заводом GEHR Plastics Ultem AM1010F FILAMENT (PEI) для 3D-печати, мы соблюдаем строгие протоколы качества - каждая партия подвергается строгим испытаниям для обеспечения последовательных стандартов эффективности и безопасности.

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    Применение нити GEHR Plastics Ultem AM1010F FILAMENT (PEI) для 3D-печати

    Inside pressurized aircraft cabin air distribution, a printed PEI bushing and an adjustable gasper support bracket replace machined Ultem 1000 rod stock when short-run lead time or inventory pressure forces an alternate fabrication path. The GEHR Plastics Ultem AM1010F filament is predried at 150 °C for no less than 4 h in a desiccant dryer with a −40 °C dew point air supply to a moisture content below 0.02 % by weight. During printing at ambient relative humidity above 60 %, the filament is fed from a hopper dryer at 100 °C. Printing is performed on a heated chamber system with the build volume maintained at 130–145 °C, the platen at 140–160 °C, and a 0.4 mm hardened steel nozzle at 375–380 °C. Layer height is held at 0.15 mm, extrusion width at 0.45 mm, and shell count is set to 5, producing a solid outer envelope through which no sparse infill is accessible to flame fronts; the resulting bead width-to-layer height ratio is 3:1. The part is oriented so that no layer boundary aligns with the airflow direction; when a gasper pivot boss is printed, the boss axis is tilted 35° from the build plane to prevent interlaminar shear at the snap-fit retention groove. Compliance for the duct body and retainer is anchored to FAR 25.853(a) App F Part I 60 s vertical burn, FAR 25.853(d) App F Part IV peak heat release of 65 kW/m² and total heat release of 65 kW/m² over the first two minutes, and ASTM E662-21a smoke density using 75 kW/m² irradiance in the vertical orientation. Published data for AM1010F as printed at 0.15 mm layer height under these exact burn conditions is limited; therefore the part is not substituted in cargo liner or primary structure without component-level requalification. Terminal components are low-rate cabin gasper retainers, avionics tray spacers, and ECS duct adapters that operate below 170 °C continuous surface temperature, with short excursion tolerance to 200 °C during ground soakback.

    Downstream segmentReferenced standard / test methodMonitored parameterProcessing response
    Cabin air and avionics ductingFAR 25.853(a) App F Part I; FAR 25.853(d) App F Part IV; ASTM E662-21a60 s vertical burn; peak heat release 65 kW/m²; total heat release 65 kW/m²; smoke density at 75 kW/m²solid shell count 5; layer height 0.15 mm; boss axis tilt 35°
    Surgical tray prototypesISO 10993-1:2018; USP Class VI; ISO 17665-1:2006dimensional stack height after 30 autoclave cycles at 134 °C100 % fill; raster rotation 45°; steam dwell 6 min
    Wave solder palletUL 94 V-0 at 0.75 mm; IPC SM-840; ASTM D257-14flatness drift over 500 cycles at 260 °C0.12 mm layer; 35 % gyroid infill; annealing 190 °C 2 h
    NOx sensor connector housingSAE J1455; ISO 16750-4; UL 94 V-090 min thermal soak at 125–135 °C; chemical immersion 15 min at 80 °C0.25 mm layer; 3 perimeters; machining allowance 0.15 mm
    Autoclave cure toolISO 527-2; ISO 75-2; ISO 11359-2vacuum pressure loss over 30 min at 0.9 bar0.20 mm layer; 25 % gyroid interior; 100 % solid first 10 mm
    Downhole connector insulator ringASTM D149-20; ASTM D257-14; IEC 60243-1insulation resistance after 48 h aging at 85–90 °C0.15 mm layer; 100 % solid fill; post-machined 0.4 µm Ra

    How Does Autoclave Cycling Degrade Layer-to-Layer Adhesion in PEI Surgical Tray Prototypes?

    When a polyetherimide tray stack is printed for reusable surgical instrument sorting, the acceptance criterion is dimensional stability after 100 autoclave cycles. The AM1010F filament is dried to a moisture content below 0.02 % by weight and processed at 380 °C extruder, 150 °C platen, 140 °C chamber, 0.15 mm layer height, 0.45 mm bead width, and 100 % part fill with a linear raster pattern rotated 45° between layers. No sparse infill is allowed in the tray base because fluid retention in unfilled triangular voids accelerates detergent carryover and biofilm adhesion. The stacking posts are modeled with a 1.0 mm boss-to-bore radial clearance and a 0.2 mm face seal chamfer to prevent moisture ingress into the layer interfaces. After each spool change, a 20 mm cube is printed at the production settings and measured across the Z axis; batch acceptance is rejected if the cube deviates more than 0.03 mm. Compliance is governed by ISO 10993-1:2018 biological evaluation planning for limited-contact surgical accessories, USP Class VI reactivity for materials that receive autoclave exposure, and ISO 17665-1:2006 moist heat sterilization. The validation sequence employs 134 °C for 5 min in a pre-vacuum autoclave for 30 cycles with a 0.5 bar/min pressure ramp, followed by dimensional check of the tray stack height across four corner bosses. A print orientation with the tray base flat on the platen yields the lowest warpage but places the steam-facing surfaces perpendicular to the Z layers; this configuration is therefore paired with a 6 min steam dwell and a 20 min dry cycle at 105 °C to reduce residual moisture expansion. Data for sterile barrier performance of FFF PEI without post-process coating is limited, so terminal use is limited to prototypes, sizing trays, and instrument trials, not to implantable or skin-contacting high-risk devices. Terminal components are autoclave-resistant sterilization trays, surgical instrument sorting cassettes, and trainer models for instrument decontamination workflows.

    Soldering Pallet Flatness Drift at 260 °C Reflow

    A wave solder pallet printed from AM1010F is checked for flatness before and after 500 cycles at 260 °C contact preheat. The material is laid down at 0.12 mm layer height with a 0.40 mm hardened steel nozzle, chamber at 130 °C, platen at 150 °C, extruder at 375 °C, and a 0.36 mm bead width, giving a width-to-height ratio of 3:1. Top and bottom solid layers are set to 7, and the edge carriages are built with 6 shells. In the central pallet deck the infill is gyroid at 35 % density, but any area within 5 mm of a through-hole for PCB locator pins is modeled with 100 % solid infill to avoid solder wave pressure deflection. The pallet is annealed at 190 °C for 2 h in a nitrogen oven after printing, with a heating ramp of 0.5 °C/min and a cooling ramp of 0.3 °C/min to relieve residual stresses that otherwise produce 0.4–0.8 mm bow across a 300 mm span after the first solder cycle. Compliance references UL 94 V-0 at 0.75 mm, IPC SM-840 for solder mask compatibility, and ASTM D257-14 for surface resistivity measured at 500 V. The printed surface is treated with a light vapor blast of 120 mesh aluminum oxide at 0.2 MPa to reduce resin smear before use; no solvent wipe is applied because acetone, MEK, and methylene chloride induce stress crazing in PEI. Published data for contact angle change on vapor-blasted PEI after 2000 cycles is limited; therefore the pallet is qualified by pilot lot inspection at 50, 150, and 500 cycles. Terminal components are wave solder pallets, reflow fixtures, PCB support plates, and stencil printer tooling plates that replace glass-filled silicone or polyimide laminate supports.

    Inside engine bay validation, a printed PEI housing for a NOx sensor connector body is exposed to 125 °C air on the exhaust side and 135 °C on the sensor boss while the vehicle runs a 90 min thermal soak. The AM1010F filament is printed with a 0.25 mm layer height, 0.5 mm extrusion width, 0.4 mm hardened steel nozzle, 380 °C extruder, 145 °C bed, 140 °C chamber, and 3 perimeters around the clip features; the resulting bead width-to-layer height ratio is 2:1. The connector body is oriented with the mating face upward and a 0.15 mm sacrificial cap over the O-ring groove; after printing, the cap is machined off on a 3-axis mill with a 2 mm carbide endmill at 12,000 rpm and 0.05 mm depth of cut to achieve the 0.10 mm groove profile tolerance. The part is annealed at 185 °C for 2 h with a ramp of 0.5 °C/min and then tested for creep under an M6 bolt preload of 3 N·m. Compliance is drawn from SAE J1455 for underhood environmental exposure, ISO 16750-4 for temperature/humidity cycling, and UL 94 V-0 at 0.75 mm for ignition resistance; chemical resistance is verified by 15 min immersion in ASTM reference fuel C, 15W-40 engine oil, and ethylene glycol/water 50/50 at 80 °C. The printed housing is not used with brake fluid, power steering fluid, or aromatic hydrocarbon cleaners because PEI stress cracks under those agents. Data for long-term vibration at engine-mounted resonance frequencies for this specific printed geometry is limited, so the housing is paired with an elastomeric isolation grommet and validated by modal testing on an electrodynamic shaker at 5 g RMS, 20–2000 Hz. Terminal components are sensor connector bodies, cam cover wire guides, and hot-side air intake sensor bosses.

    When Tool Face Vacuum Integrity Dictates Layer Height and Sealant Post-Processing

    For a low-rate autoclave cure tool operated at 180 °C and 0.6 MPa, the printed PEI tool face is treated as a porous laminate that requires sealing. AM1010F is printed at 0.20 mm layer height, 0.60 mm extrusion width, 0.60 mm hardened steel nozzle, 370 °C extruder, 150 °C platen, 140 °C chamber, and 5 perimeters to obtain a 3.0 mm dense outer shell. The interior is filled at 25 % gyroid density, but the first 10 mm from the tool face is modeled as 100 % solid with a layer-to-bead overlap of 30 % to interrupt vacuum leak paths. After printing, the tool face is machined with a 6 mm ball-nose cutter at 8000 rpm, 0.20 mm stepover, and 0.10 mm final pass depth, then sealed with a two-part epoxy tooling sealer to fill residual interlayer voids. Vacuum integrity is verified by a 0.9 bar differential pressure drop test over 30 min; if the pressure loss exceeds 0.05 bar, the part is returned for an additional seal coat and cure at 80 °C for 2 h. Compliance references ISO 527-2 for tensile properties, ISO 75-2 for deflection temperature under flexural load, and a CTE measurement using ISO 11359-2 from 23 °C to 180 °C, which controls the thermal expansion mismatch to carbon fiber/epoxy laminates. The printed tool is not exposed to release agents containing aromatic hydrocarbons; a water-based release film is used. Published data for autoclave cycle fatigue of FFF PEI tooling at 0.6 MPa beyond 50 cycles is limited, so the process is qualified per individual master by dimensional audit of the molded composite part after cycles 1, 10, and 50. Terminal components are autoclave cure tooling, vacuum forming dies, and drill fixtures for carbon fiber trim operations.

    High-Pressure Connector Insulator Performance Without PEEK

    A PEI insulator ring for a 10,000 psi rated downhole connector is printed from AM1010F with a 0.15 mm layer height, 0.45 mm bead width, 0.40 mm hardened steel nozzle, 380 °C extruder, 150 °C platen, 140 °C chamber, and 100 % solid fill to eliminate microvoids that reduce dielectric strength; the bead width-to-layer height ratio is 3:1. The ring is post-machined on both faces with a diamond tool to a surface finish of 0.4 µm Ra and then annealed at 195 °C for 1.5 h under dry nitrogen. The material is selected for its glass transition temperature of 217 °C and its retention of dielectric strength above 150 °C; compliance references ASTM D149-20 for short-time dielectric breakdown, ASTM D257-14 for volume and surface resistivity at 500 V, and IEC 60243-1 for electric strength of solid insulating materials. The ring is qualified for 48 h aging in deionized water at 85 °C and 5 % NaCl at 90 °C, followed by a 500 V insulation resistance check; any value below 10 GΩ triggers rejection. The service boundary is set at 150 °C continuous operating temperature and exposure to methane, hydrogen sulfide, and mineral oil; exposure to ketones, chlorinated solvents, and strong alkaline drilling muds is excluded because those agents cause stress cracking or surface hydrolysis in PEI. Data for printed PEI at 0.15 mm layer height under high-pressure methane permeation is limited; therefore the part is not used as a pressure barrier or primary seal, only as an electrical insulator inside a metal-housed connector. Terminal components are downhole connector insulator rings, sensor coil bobbins, and logging tool stand-off blocks.

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    Более подробное введение

    GEHR Plastics ULTEM AM1010F FILAMENT (PEI) is a polyetherimide monofilament supplied for fused filament fabrication of amorphous high-temperature thermoplastics. The product designation AM1010F identifies a polyetherimide resin optimized for extrusion, available in 1.75 mm and 2.85 mm diameters with a nominal diameter tolerance of ±0.05 mm. Published density is 1.27 g/cm³ when measured under ISO 1183-1:2019, and differential scanning calorimetry shows no crystalline melt peak; the glass transition temperature is 217 °C under ISO 11357-2:2020. Because the material is amorphous, solidification is controlled by vitrification rather than crystallite growth, which reduces the sharp volumetric contraction associated with semicrystalline filament but does not eliminate build-chamber residual stress.

    Representative application areas include aircraft cabin interior components requiring FAR 25.853(a) vertical burn evaluation, electrical connector bodies and housings rated V-0 under UL 94, and tooling exposed to autoclave cycles. End-use performance must be tested on specimens of the final build orientation; injection-molded resin values do not transfer directly to fused deposition bodies. For load-bearing printed parts, property comparisons are made under ISO 527-2:2012 and ISO 178:2019 rather than molded plaque data.

    What moisture ceiling must be observed before extrusion?

    Moisture uptake in ULTEM AM1010F is lower than in nylon but sufficient to cause hydrolytic chain scission when residual water is present above 0.02 wt% at extrusion temperatures above 300 °C. Spool-level drying in a desiccant dryer with a dew point of ≤ −40 °C at 150 °C for 4 h is the minimum pre-processing threshold. During printing, the spool should be held at 80 °C to 90 °C under a positive purge of dried air or nitrogen. In production-scale ovens, spools stacked more than one layer deep exhibit center-of-stack thermal lag and may not reach the 150 °C setpoint within 4 h; such batches produce splay at the nozzle exit and reduced interlayer fusion. Hydrolytic chain scission also lowers notched Izod impact, making drying a process-control parameter rather than a storage recommendation.

    Enclosure temperature, bed adhesion, and layer fusion thresholds

    The extrusion barrel is typically set to 370 °C to 390 °C, with all-metal hot ends and hardened tool-steel nozzles; below 350 °C, melt viscosity retards layer fusion, while above 400 °C residence-time degradation increases. The build platform is maintained at 140 °C to 160 °C, and a closed chamber is required. Chamber air temperature at the part surface should be held at 120 °C to 180 °C for parts with wall thickness above 8 mm or length above 150 mm. The coefficient of linear thermal expansion is approximately 5.6 × 10⁻⁵ °C⁻¹ per ASTM E831-19, implying a free linear contraction from 217 °C to 23 °C of roughly 1.1%. Without chamber heating, this contraction is restrained by the build plate and previously deposited layers, producing edge lift and interlayer fracture. On open-platform FFF systems limited to 90 °C, published data for this specific configuration is limited, but production-floor reports describe delamination and z-direction tensile loss in thick-section parts.

    Feed consistency is influenced by ovality and winding tension. Laser-micrometer inspection of filament diameter should maintain total indicator runout within ±0.05 mm; ovality beyond ±0.07 mm creates extrusion-rate variation above 3% and feedgear slip in Bowden systems. Direct-drive extruders with hardened-steel drive gears and idler force of 20 N to 30 N are preferred over PTFE-lined hot ends because the processing temperature exceeds the PTFE service limit. Incoming melt flow rate is logged under ISO 1133-1:2022 at 337 °C and 6.6 kg; the high-flow base-resin architecture permits layer times below 90 s in moderately sized parts, but the coolant effect of the build chamber still requires direct-drive extrusion.

    When print speed exceeds 30 mm/s with a 0.4 mm nozzle, does AM1010F remain process-stable?

    Extrusion flow characteristics of AM1010F are shear-thinning. With a 0.4 mm hardened steel nozzle and a layer height of 0.25 mm, stable volumetric output is generally limited to 15 mm/s to 30 mm/s; higher speeds require 0.6 mm or larger nozzles and increase back pressure on the drive gear. The recommended nozzle-to-bed first-layer gap is 0.1 mm below nominal for PEI sheet adhesion, measured with a feeler gauge rather than automated offset. At print speeds above 35 mm/s, interlayer diffusion time falls below the relaxation threshold for this polyetherimide grade, and x-y tensile values remain acceptable while z-direction tensile strength drops rapidly. Mechanical anisotropy is therefore governed by chamber heat and volumetric throughput. Tensile specimens printed flat and tested under ASTM D638-14 Type V or ISO 527-2:2012 5A/50 show orthotropic behavior; z-axis tensile strength for PEI additive parts is commonly 40% to 60% of xy-axis values under marginal chamber conditions. Published data for this specific product in a controlled 180 °C chamber is limited, so qualification programs should include representative z-direction tensile specimens.

    Thermal, mechanical, and flammability data for GEHR Plastics ULTEM AM1010F

    PropertyTypical ValueTest Method
    Density1.27 g/cm³ISO 1183-1:2019
    Glass transition temperature217 °CISO 11357-2:2020
    Tensile strength at break82 MPaISO 527-2:2012
    Tensile modulus3,200 MPaISO 527-2:2012
    Flexural strength130 MPaISO 178:2019
    Flexural modulus3,300 MPaISO 178:2019
    Notched Izod impact at 23 °C5.0 kJ/m²ISO 180:2019
    Heat deflection temperature at 1.80 MPa213 °CISO 75-2:2013
    Flammability classV-0 at 1.5 mmUL 94

    ULTEM AM1010F is distinguishable from ULTEM 9085 principally in glass transition, stiffness, and impact response. ULTEM 9085 is an impact-modified PEI grade with published resin values of glass transition temperature 186 °C by ISO 11357-2:2020, heat deflection temperature 153 °C at 1.80 MPa by ISO 75-2:2013, tensile strength 68 MPa by ISO 527-2:2012, and notched Izod impact 12 kJ/m² by ISO 180:2019. AM1010F therefore extends the thermal envelope upward while sacrificing some ductility, which shifts suitability toward static aerospace interior brackets and thermal tooling rather than snap-fit, high-impact components. Relative to unfilled PEEK, AM1010F processes at lower nozzle and chamber temperatures, but PEEK offers higher continuous-use temperature and stronger organic-solvent resistance. PEEK also requires nozzle temperatures above 400 °C and chamber temperatures above 180 °C, making AM1010F a more practical high-temperature polyetherimide where the operating environment does not exceed the PEI thermal range.

    Chemical incompatibility boundaries for AM1010F include chlorinated solvents, N-methyl-2-pyrrolidone, and strong alkaline solutions; environmental stress cracking may occur when printed parts are exposed to these solvents under load. Steam autoclave exposure requires printed-part porosity testing because layer interfaces can permit fluid ingress. End-use qualification for aerospace parts must evaluate print orientation, shell wall count, fill density, and any annealing step because UL 94 and FAR 25.853(a) are configuration-dependent tests. The V-0 rating at 1.5 mm reported for the resin grade does not automatically transfer to a printed air duct or connector housing without validation on representative fused deposition specimens.

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