| Код ТН ВЭД | 314794 |
Как аккредитованный завод BASF 3D Ultrafuse PEI 9085 Fused Fillament, мы соблюдаем строгие протоколы качества - каждая партия подвергается строгим испытаниям для обеспечения последовательных стандартов эффективности и безопасности.
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Pressurized cabin air distribution components are printed directly from BASF 3D Ultrafuse PEI 9085 fused filament when certification requires flame-smoke-toxicity performance without secondary coating. Wrap-around duct sections, butterfly valve flanges, and manifold adapters are built with a 0.40 mm hardened steel nozzle, 0.20 mm layer height, and chamber air temperature maintained at 90–110 °C. The four-zone hot end is profiled to hold a melt temperature spread of ±5 °C around 375 °C. Excursions above 390 °C produce polymer degradation and acid gas odor. Readings below 360 °C cause melt fracture and incomplete interlayer diffusion. Spools are dried at 120 °C for 4 h to below 0.02 % residual moisture before extrusion. Higher moisture content creates hydrolysis, nozzle spitting, and Z-axis delamination under cabin pressure cycling. For non-pressure-retaining acoustic shrouds, 45 % rectilinear infill with 4 perimeters balances mass against vibration damping. For duct connectors exposed to positive cabin pressure, infill is raised to 100 % solid with 6 perimeters and 0.15 mm layer height to reduce interlayer leakage paths. Vertical burn compliance is verified on printed coupons at 1.5 mm thickness using FAR 25.853(a) Appendix F Part I. Smoke optical density is measured with ASTM E662, and toxic gas release with BSS 7239. Terminal parts replace machined ULTEM 9085 stock in cabin recirculation plenums, avionics cooling shrouds, and seat-row air nozzles.
For epoxy prepreg systems cured at 121 °C and 0.62 MPa, composite fabrication cells convert the same filament into vacuum-forming fixtures, caul plates, and drill jigs. The tool body is printed with 100 % solid infill, 7 perimeter walls, and 0.15 mm layer height to eliminate vacuum leaks across the tool backface. Surface porosity is closed with a light solvent wipe and post-cured at 200 °C for 2 h. This step stabilizes the polymer against creep during repeated autoclave cycles. Dimensional change after 250 cycles is monitored against a master datum hole grid using ISO 1101 geometric tolerance references. Interlayer tensile specimens tested under ISO 527-2 show Z-direction properties below XY-direction values; load-bearing vacuum ports are therefore printed with split-line orientations rotated 45 ° between layers. The main failure mode observed on production shop floors is corner lift-off when the tool is loaded before chamber soak. The tool is ramped at 1 °C/min to 80 °C before full vacuum and autoclave pressure are applied. Drill jigs and trim fixtures printed from the same spool retain edge hardness at elevated temperature, allowing hand routers to follow printed contour templates without resin pickup.
Rail vehicle interior programs require fire performance across multiple EN 45545-2:2020 test sets simultaneously, not just a single wall thickness. Seat-back monitor housings, HVAC outlet grilles, and armrest end caps are printed with 100 % PEI 9085, without flame-retardant coating, because the base polymer already meets the limiting indices for Hazard Level 2 in non-layered products. The extrusion settings are adjusted for long flat parts. Nozzle temperature is held at 365 °C. Bed temperature is set to 160 °C. Chamber temperature is maintained at 110 °C. Print speed is limited to 35 mm/s. A brim of 8 mm width is applied to control corner warpage on parts longer than 300 mm. Compliance is documented with EN 45545-2:2020 R1 surface flame spread, R6 smoke emission, and R7 toxic fume release on printed specimens at 2 mm section thickness. The terminal components are installed without painting or sealing. Edge quality is maintained through 0.15 mm layer steps to avoid wicking paths that can change flame front direction. Published data for laser-sintered PEI alternatives in the same hazard level envelope is limited, so filament-based parts are qualified part-by-part using the same printed section thickness as production geometry.
| Application segment | Standard or method | Specimen condition | Boundary record |
|---|---|---|---|
| Aerospace cabin ducting | FAR 25.853(a) App F Part I | 1.5 mm printed coupon | 60 s vertical burn pass |
| Aerospace smoke | ASTM E662 | 25 kW/m² irradiance | pass/fail per airframe program |
| Rail interior | EN 45545-2:2020 R1/R6/R7 | 2 mm printed plaque | HL2 non-layered index |
| Automotive insulator | ASTM D149 | 2 mm printed plaque | dielectric breakdown pass/fail |
| Electronics carrier | IPC-J-STD-004 | flux contact as-printed | no microcracking after ROL0/ROL1 |
On high-voltage battery assembly lines, the same filament is used for busbar support brackets, module alignment trays, and underhood standoffs that require dimensional stability after hot-oil exposure. The processing window is narrowed to a nozzle temperature of 370–390 °C and a chamber temperature of 100–120 °C to maximize interlayer adhesion in thick sections. For busbar insulators, the print recipe uses 100 % solid fill, 0.10 mm layer height, and 0.35 mm extrusion width to reduce void content below the breakdown threshold. Dielectric strength is verified on printed plaques in accordance with ASTM D149. Insulation resistance is measured under IEC 62631-3-1. Parts function in regions where temperature excursions reach 150 °C for short cycles. Sustained exposure beyond 180 °C causes measurable creep under clamping load. For this reason, metal fasteners are used with shoulder washers to limit compressive stress on the printed boss faces. Batch-to-batch spool diameter variation below 0.05 mm is accepted. Larger ovality produces filament feed slip and under-extrusion at the 0.35 mm nozzle gap.
In industrial vacuum forming cells, epoxy-board nests are replaced with printed PEI 9085 female molds for short-run thermoplastic trim. The substitution is valid only where the sheet preheat does not exceed 220 °C at the tool surface for more than 10 min. The mold is printed with 0.30 mm layer height, 3 perimeter walls, and 20 % triangular infill to permit fast thermal cycling. The top 1.5 mm of the mold is printed as a sacrificial face with 0.10 mm layer height and 100 % solid fill. After machining or sanding, the face is sealed with a 200 °C thermal post-treatment. Molds for mineral-filled polypropylene sheet show no measurable face wear after 500 forming cycles. Published data for glass-reinforced sheet stock is limited. Pull-out studs and vacuum channels are printed integral to the mold body to avoid drilling stress concentrations. Dimensional checks on formed parts are recorded against the mold master using ISO 1101. Deviations above 0.25 mm require mold re-machining or face replacement.
Within electronics assembly lines, solid printed PEI 9085 carrier trays and selective solder pallets handle PCB transport through reflow ovens. The trays are printed at 100 % infill with 0.20 mm layer height using a 0.40 mm nozzle. Exposure to 260 °C peak reflow temperature for 90 s is within the polymer’s short-term thermal capability. Flux contact with types ROL0 and ROL1 according to IPC-J-STD-004 produces no surface microcracking after wiping with isopropyl alcohol. Aggressive chlorinated solvents cause surface microcracking and must not be used. The only recurring maintenance operation recorded is replacement of printed support pins after mechanical fatigue. Pin lifetime is improved when the pin base radius is designed above 1.0 mm to reduce stress concentration.
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BASF 3D Ultrafuse PEI 9085 Fused Fillament is an amorphous polyetherimide-based feedstock for fused filament fabrication in high-temperature material extrusion systems. The product is supplied in 1.75 mm and 2.85 mm nominal diameters on 750 g spools, with a reported solid density of 1.34 g/cm³ under ISO 1183-1. The material is not a metal-polymer system and does not require catalytic debinding or sintering; after extrusion and support removal it remains a thermoplastic polyetherimide part. This separates it from the BASF Ultrafuse 316L and 17-4 PH grades, which are green-body feedstocks for furnace sintering. The resin is also distinct from filled high-temperature filaments because it is unfilled, yet it requires an actively heated build chamber, an all-metal hot end, and a hardened steel or ruby nozzle. Published processing guidance indicates a nozzle setpoint between 350 °C and 380 °C, a build plate from 120 °C to 140 °C, and a chamber setpoint from 150 °C to 180 °C. Open-frame or passively heated machines are therefore outside the documented process envelope.
The amorphous character of the polymer means that no melt crystallization exotherm is present, but layer-to-layer adhesion and residual stress remain strongly governed by chamber temperature, extrusion temperature, and prior moisture content. On production-scale direct-drive systems with active chamber heating and a liquid-cooled cold zone, the material processes with a narrow window: below 350 °C the melt exhibits insufficient diffusion for consistent interlayer strength, while above 380 °C prolonged melt residence can produce carbonized nozzle deposits and pressure drift. Bowden arrangements are generally unsuitable because the filament is high-modulus and the spring-back on retraction increases the risk of buckling at the extruder drive. A nozzle diameter of 0.4 mm or larger is typical for extrusion stability, and extrusion multipliers are commonly held between 0.95 and 1.00 after line-thickness calibration on the specific machine.
At the molecular level, polyetherimide absorbs atmospheric moisture. The resin is reported to exhibit water absorption of 0.25% after 24 h under ASTM D570. Absorbed water at 350 °C to 380 °C flashes into steam during extrusion, generating microvoids, nozzle spitting, and intermittent extrusion-line roughness. In addition, moisture at high melt temperature may contribute to chain scission in condensation polymer systems, causing localized viscosity loss and reduced melt strength. The manufacturer therefore specifies pre-drying at 120 °C for 4 h in a forced-air drying oven. Spools left in an uncontrolled ambient environment above 60% relative humidity for extended periods require re-drying. Visual dryness is not an adequate control because bulk moisture can remain even when the surface appears dry.
Moisture-related extrusion defects are frequently misdiagnosed as incorrect nozzle temperature or insufficient purge. In practice, a frothy or speckled extrusion line during the first few metres of purging is a stronger indicator of water in the filament than of thermal degradation. Closed-loop hot-end temperature control alone cannot compensate for this condition. High-temperature material extrusion machines equipped with idle-temperature reduction and automatic purge routines are preferable, because static residence in the melt zone at 380 °C accelerates thermal degradation. The safe procedure is to dry the spool thoroughly, verify the hot-end setpoint with a calibrated pyrometer, purge after any dwell longer than 10 min, and begin printing only after a solid bead with uniform diameter is produced.
Because printed properties are toolpath-dependent, the values in Table 1 are reported from supplier-published data and resin reference data. They are not automatically valid for every part orientation, infill geometry, or machine configuration. For structural applications, part-specific testing is required.
| Property | Test method | Reported value | Condition |
|---|---|---|---|
| Density | ISO 1183-1 | 1.34 g/cm³ | Solid resin/filament |
| Tensile strength | ISO 527-2 / ASTM D638 | 68 MPa | XY printed coupon |
| Tensile modulus | ISO 527-2 | 2150 MPa | XY printed coupon |
| Elongation at break | ISO 527-2 | 5.9% | XY printed coupon |
| Heat deflection temperature | ISO 75-2/B at 0.45 MPa | 153 °C | Annealed/resin reference |
| Heat deflection temperature | ISO 75-2/A at 1.82 MPa | 143 °C | Annealed/resin reference |
| Notched Izod impact | ASTM D256 | 106 J/m | Resin reference |
| Water absorption | ASTM D570 | 0.25% | 24 h |
| Flammability | UL 94 | V-0 at 1.5 mm | Resin reference |
Material extrusion anisotropy is not captured by resin values. The Z-direction tensile strength of printed PEI 9085 is typically lower than the XY tensile strength because the layer interface is the weak plane. Published Z-direction data for this specific filament is limited, and design allowables should be established by printing test bars with the intended build orientation, layer height, infill density, and chamber setpoint. The notched Izod value is also sensitive to raster direction, shell thickness, and welding temperature. A resin-reference impact value does not substitute for a notched Izod test on a printed specimen with the actual toolpath. For aerospace interior applications, the resin flammability rating is a starting point only; component-level vertical burn testing under FAR 25.853 is required because part thickness, honeycomb or foam interfaces, and post-processing affect burn behaviour.
To differentiate PEI 9085 from ULTEM 1010, PEEK, and flame-retardant PC/ABS, the service environment must be fixed first. PEI 9085 has a lower heat deflection temperature than unfilled ULTEM 1010: 143 °C versus approximately 213 °C at 1.82 MPa under ISO 75-2/A. That difference restricts PEI 9085 when a tool or fixture must survive continuous exposure above 140 °C under flexural or tensile load. In return, PEI 9085 is typically processed at lower chamber and nozzle temperatures than ULTEM 1010 and is less notch-sensitive in many impact-loaded geometries. Compared with unfilled semicrystalline PEEK, which has a published heat deflection temperature near 152 °C at 1.82 MPa under ISO 75-2/A and continuous-use capability near 250 °C, PEI 9085 offers a lower processing temperature and eliminates the crystallization-dependent dimensional control that PEEK requires. The tradeoff is lower chemical resistance, lower maximum service temperature, and reduced resistance to hot aqueous acid or alkaline hydrolysis.
Against flame-retardant PC/ABS blends, PEI 9085 generally provides higher heat deflection and the ability to achieve UL 94 V-0 at thinner sections, but it imposes a much higher chamber temperature and nozzle setpoint. Many flame-retardant PC/ABS systems process at nozzle temperatures from 260 °C to 280 °C and can be printed on lower-temperature enclosed machines, whereas PEI 9085 requires sustained chamber operation near 160 °C to 180 °C. The difference in machine capability is a more significant barrier than the difference in raw material price. For chemically corrosive service, PEI 9085 should not be used with continuous immersion in chlorinated solvents, ketones, aromatic hydrocarbons, or high-pH alkaline solutions. Cleaning agents should be screened by immersion testing under ASTM D543, because stress cracking may appear only after the part is installed under load. Steam autoclaving above 134 °C and repeated hot-water exposure can also exceed the practical envelope for amorphous polyetherimide unless part-specific validation demonstrates acceptable retention of tensile strength and impact.
In fire-resistant housings, ducting, brackets, and functional prototypes, PEI 9085 is used where flame, smoke, and low-toxicity requirements exclude standard polycarbonate or PC/ABS grades. The material is also applied in tooling and semiconductor-adjacent fixtures where dimensional stability at elevated temperature is required but full PEEK chemical resistance is unnecessary. Unlike BASF metal-polymer filaments, PEI 9085 does not produce a metallic final part and does not require solvent debinding or sintering shrinkage compensation. Process control is therefore simpler than for catalytically debound metal systems, but polymer creep-fatigue data for printed PEI 9085 remains limited. For dynamic structural parts, test coupons should follow ASTM D638 or ISO 527-2, and long-term creep testing should be performed according to ISO 899-2 or an equivalent design-code protocol.
Post-processing by drilling, tapping, sanding, and light machining is possible with carbide or diamond tooling, but heat generation during machining can soften the surface and should be controlled by low feed pressure and sharp tools. Adhesive bonding is generally more consistent than solvent welding, and adhesive selection should include lap-shear testing under ASTM D3163 at the intended service temperature. The supplier documentation should be reviewed for REACH and RoHS declarations; a neat resin classification does not automatically certify a post-processed assembly for a specific regulatory environment. For printed aerospace parts, flame and smoke certification must be performed on the final fabricated component because part geometry, coating, and bonding layers affect the test outcome.