| Код ТН ВЭД | 463208 |
Как аккредитованный завод по быстрому прототипированию полимеров iSQUARED Ultem 9085, мы соблюдаем строгие протоколы качества - каждая партия подвергается строгим испытаниям для обеспечения последовательных стандартов эффективности и безопасности.
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In airworthiness-certified cabin interior replacement programs, iSQUARED ULTEM 9085 rapid prototyping polymer is fed to high-temperature FDM/FFF equipment as a single-component, unfilled PEI blend; no supplemental flame-retardant masterbatch is added at the converter stage because the formulation is 100% 9085 resin. Moisture control preceding extrusion is mandatory: feedstock is dried at 150°C for 4 h in a desiccant dryer until residual moisture is below 0.04%, since hydrolysis at melt temperatures between 350–380°C causes interlayer voiding and a measurable drop in tensile strength. On a Stratasys Fortus 450mc-class platform with a heated chamber held at 90–120°C and a layer height of 0.254 mm, the resulting laminates are evaluated to 14 CFR 25.853(a) vertical burn requirements only when raster orientation, wall count, and part density are frozen in the toolpath file. The addition ratio is therefore a build-density specification rather than a resin dilution level: 100% solid infill for structural air duct brackets, 5 perimeter roads, and 0% regrind in the filament lot trace. Smoke density and heat release are anchored to ASTM E662-17 and the OSU 65/65 chamber method referenced in 14 CFR 25.853(d) Appendix F Part IV; batch-specific test certificates should be requested from the filament supplier because published data for every generic printed configuration is limited. Downstream production consists of controlled-chamber FDM deposition, dedicated support material removal, drilling and reaming of mating bores to H7 tolerance, and installation of helicoil or press-fit brass inserts. Finished part classes include cabin air diffuser vanes, tray table latch brackets, sidewall cable mounting blocks, avionic bay ventilation grilles, and PSU fan shroud standoffs.
Process stability at wall thicknesses below 1.6 mm is governed by heat accumulation in the melt pool during short toolpath reversals on a high-temperature FDM platform, not by print resolution. Under-hood coolant return ducts and charge-air sensor housings are produced at 100% solid density, with a 0.254 mm layer and a 0.305 mm nozzle orifice to preserve the UL 94 V-0 rating at 1.5 mm cited in the ULTEM 9085 resin datasheet. Compliance evaluation follows UL 94 vertical burn, ASTM D648-18 for deflection under 1.82 MPa, and ASTM D638-14 tensile tests on coupons sectioned from XY and ZX orientations; because FDM anisotropy reduces Z-tensile strength relative to XY, bosses and snap arms are oriented so principal load follows the XY raster plane. The addition ratio remains 100% unreinforced 9085; glass-filled PEI compounds are not substituted because they shift the shrinkage profile and invalidate the unfilled datasheet baseline. For threaded inserts, the bore is machined after printing and a brass insert is installed with ultrasonic insertion at 20 kHz and 0.2 s dwell, not printed into the part. Terminal finished components include vehicle battery vent duct prototypes, sensor mounting flanges, ECU enclosure spacers, and wire harness routing clips used under 120°C continuous service.
Because semiconductor tooling qualification cells prioritize dimensional stability, outgassing, and static dissipation, iSQUARED ULTEM 9085 is processed only where insulative rather than conductive properties are specified. Compliance for final machined parts references RoHS 2011/65/EU, the current REACH candidate list for SVHC disclosure, UL 94 V-0 flame grouping, and electrical testing under ASTM D257-14 and IEC 60243-1; outgassing acceptance is verified under ASTM E595-15, but published data for FDM-layered 9085 after specific cleaning protocols is limited, so coupon-level TML and CVCM values must be generated for production lots. The addition ratio is 100% unfilled 9085 with no carbon black, carbon fiber, or antistatic masterbatch; if a surface resistivity below 1×109 Ω/sq is required by the tool specification, a different static-dissipative grade is indicated. Downstream production involves FDM deposition, followed by three-axis CNC fly-cutting to maintain a mounting hole positional tolerance of ±0.05 mm and a datum flatness of 0.05 mm across 150 mm, then cleaning with deionized air. Terminal parts include wafer cassette guide rails, test socket bodies, packaging tray prototypes, and probe card stiffener mockups.
Operating a printed 9085 mandrel at 100% infill and top/bottom skin thickness not less than 3.0 mm addresses vacuum-bag consolidation at 0.85 bar negative pressure and autoclave cure profiles peaking at 180°C for 120 min; however, the coefficient of thermal expansion of the printed tool must be characterized per ISO 11359-2:2021 before first article, because repeated cycling shifts the mating face if the tool is not normalized after printing. Compliance for tooling acceptance typically references ASME Y14.5-2018 for surface profile tolerances and ASTM D648-18 for deflection verification, not FST fire standards. The addition ratio is 100% ULTEM 9085 with no porous infill; any reduction below solid density creates vacuum leak paths through the shell and permits resin bleed during cure. Process sequence: FDM deposition in a 90–120°C chamber, section bonding with a PEI-compatible epoxy film, post-bond CNC machining to ±0.08 mm surface profile, application of a high-temperature tool sealant, and, where residual stress is detected by dial indicator over 0.1 mm, a normalization cycle below the measured HDT applied only after fixture compensation; published data for optimum soak time on 9085 printed tools is limited. Terminal parts include composite lay-up mandrels, router trim fixtures, drill locator plates, and vacuum form tool inserts for short-run production.
Prototype housings for diagnostic instruments and preoperative anatomical models printed from iSQUARED ULTEM 9085 are evaluated under ISO 10993-1:2018 only as limited-contact, non-implantable parts; the material is not supplied under an implantable-grade designation, and resin certificates are not a substitute for finished-device biocompatibility testing. The addition ratio is 100% virgin 9085 for laboratory prototypes; regrind or recycled filament is excluded because chain-of-custody documentation for patient-contact evaluations cannot be maintained with mixed lots. For intact skin contact, a manufacturer typically commissions cytotoxicity and sensitization assays per ISO 10993-5 and ISO 10993-10 on FDM coupons averaged from five build orientations. Downstream processing includes FDM deposition, wet sanding with 1200-grit paper to lower surface roughness below 0.8 µm Ra where sealing is required, and cleaning with a non-chlorinated solvent; sterilization compatibility must be validated per ISO 17664-1, because published data for repeated steam autoclaving of 9085 FDM parts is limited. Terminal finished items are surgical tool mock-ups, diagnostic instrument chassis prototypes, CT calibration phantom housings, and non-sterile preoperative anatomical planning models.
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iSQUARED Ultem 9085 Rapid Prototyping Polymer is a fused-filament-grade polyetherimide/polycarbonate (PEI/PC) blend based on SABIC ULTEM 9085 resin. The product is supplied as filament with nominal diameters of 1.75 mm and 2.85 mm and a dimensional tolerance of ±0.05 mm. The amorphous material is intended for heated-chamber fused filament fabrication (FFF) platforms with all-metal hot ends rated to 400°C. Representative density for the base resin is 1.34 g/cm³ per ASTM D792. Because the material is a PEI/PC blend, it occupies a processing position between unfilled polyetherimide and flame-retardant PC/ABS: lower melt viscosity than standard PEI, higher heat deflection than PC/ABS, and a documented vertical burn rating under UL 94. Published multi-factor interaction data specific to iSQUARED-processed Ultem 9085 filament remain limited; the following figures are base resin values from SABIC technical documentation and should be verified on production lots before design release.
| Property | Typical Value | Test Method |
|---|---|---|
| Specific gravity | 1.34 | ASTM D792 |
| Melt flow rate at 337°C/6.6 kg | 17 g/10 min | ASTM D1238 |
| Tensile stress at yield | 47 MPa | ASTM D638 |
| Tensile modulus | 2150 MPa | ASTM D638 |
| Flexural modulus | 2140 MPa | ASTM D790 |
| Notched Izod impact | 106 J/m | ASTM D256 |
| Heat deflection temperature at 1.82 MPa | 153°C | ASTM D648 |
| Flammability at 1.5 mm | V-0 | UL 94 |
Relative to unfilled polyetherimide grades such as ULTEM 1010, Ultem 9085 shows a lower heat deflection temperature of 153°C at 1.82 MPa compared with approximately 216°C for ULTEM 1010 under the same stress. Its tensile yield strength is also lower. The offset is a higher melt flow index and reduced extruder torque on high-temperature FFF lines. The polycarbonate-modified blend permits stable processing on equipment rated to 160°C, whereas unfilled PEI often requires chamber setpoints above 180°C for larger cross-sections. This does not make Ultem 9085 a direct substitute for ULTEM 1010 in all applications; the selection depends on the thermal boundary condition of the part, not on the printer availability alone.
Against flame-retardant PC/ABS, Ultem 9085 raises the heat deflection temperature from the typical 85–95°C range to 153°C and provides a UL 94 V-0 rating at 1.5 mm. The PEI/PC structure also shows more consistent dimensional stability in heated-air environments and lower thermogravimetric mass loss at temperatures above 120°C when compared with butadiene-containing PC/ABS blends. The trade-off is that Ultem 9085 requires a heated build chamber and continuous drying, whereas PC/ABS can be printed on open-frame machines with less setup overhead.
Compared with semi-crystalline polyketones such as PEEK and PEKK, Ultem 9085 has lower tensile modulus, lower continuous-use temperature, and lower resistance to strong acids and chlorinated solvents. However, it avoids the crystallite-induced warpage and high chamber requirements of polyketones. For rapid prototyping programs that require flame-smoke-toxicity documentation, low moisture sensitivity relative to polyamide, and lower cost than PEEK, the material is frequently the first specification tested.
Moisture uptake in PEI/PC blends shifts melt viscosity and produces microvoiding in the extrudate. The material is dried at 150°C for 4 h to a target moisture level below 0.02 wt% before extrusion. A desiccating dryer with a dew point of -40°C and forced-air regeneration is preferred. Passive spool heaters at 70°C do not remove bound water quickly enough for high-flow PEI/PC, and extrusion from inadequately dried spools typically produces audible steam pop at the nozzle and surface blistering on vertical walls. After drying, filament is transferred to a sealed spool holder or an actively purged chamber with a dew point below -30°C.
Extrusion barrel setpoints of 380°C to 400°C are typical for 0.4 mm and 0.6 mm nozzle orifices. Hardened steel nozzles are specified because long runs at these temperatures can accelerate brass wear. The bed setpoint is 160°C, with polyimide tape or high-temperature adhesive film used as the build surface. Print speeds above 45 mm/s can reduce interlayer bond strength because the deposited bead residence time in the fusion zone becomes shorter. Retraction distance is limited to 0.5–1.0 mm to avoid pulling molten polymer into the cold barrel zone and freezing the filament above the heat break.
Filament batch records from high-temperature FFF service indicate that ovality exceeding 0.07 mm leads to feed gear slip and intermittent under-extrusion in direct-drive extruders with hardened feed wheels. Diameter variation below ±0.03 mm is therefore specified for production runs. Batch-to-batch melt flow index variation greater than ±2 g/10 min at 337°C/6.6 kg requires a barrel temperature offset of 5–10°C to maintain equivalent extrusion pressure and bead width.
Below 135°C chamber air temperature, Z-direction tensile strength in FFF specimens falls because the deposited bead cannot fuse to the previous layer before the surface quench. On a high-temperature system with a 300 mm × 300 mm × 400 mm build volume, operators observe corner chamfer lifting and microcrack formation during part cooling. The failure mode is process-induced, not a change in the base polymer; it is controlled by holding chamber air temperature at 150°C and setting part cooling fan speed to 0% for the first layers. At chamber temperatures above 165°C, thin vertical walls may sag, and breakaway support interfaces can remain too tacky for clean removal.
The processing window is narrow enough that thermocouple placement matters. A chamber thermistor located near the door hinge may read 150°C while the far corner of a large build plate is 10–15°C lower. Production-scale prints therefore use two-point or three-point chamber temperature monitoring, and the door is kept sealed for the full build. Parts with large planar footprint and thin top sections are most sensitive to this edge-to-center thermal gradient.
Flame-smoke-toxicity performance is a primary reason for specifying this material in aerospace and rail prototyping. Published SABIC ULTEM 9085 base resin documentation reports a UL 94 V-0 rating at 1.5 mm. For aircraft cabin interior prototype parts, the material is typically referenced to FAR 25.853(a) vertical burn and FAR 25.853(d) OSU heat release. Printed coupons require verification because void content, layer boundaries, and contamination can alter fire and smoke response independently of base resin data.
| Standard | Test condition | Documented result |
|---|---|---|
| UL 94 | 1.5 mm thickness | V-0 |
| FAR 25.853(a) Appendix F Part I | 60-second vertical burn | Pass per base resin documentation |
| FAR 25.853(d) OSU heat release | 65 kW/m² radiant heat flux | Total 65 kW·min/m², peak 65 kW/m² reported pass |
| BSS 7239 toxicity | Specific gas emission | Pass per supplier documentation on printed coupons |
Chemical resistance of Ultem 9085 to aliphatic hydrocarbon media, hydraulic fluid, and many aerospace cleaning agents is generally better than PC/ABS but below semi-crystalline PEEK. Chlorinated solvents, strong acids, and some ketones can attack the polyetherimide phase. Parts intended for contact with phosphate ester hydraulic fluids or aggressive paint strippers are evaluated under ASTM D543 because fluid absorption can reduce tensile strength and dimensional stability. The material is also checked for stress cracking after exposure to methyl ethyl ketone vapor during paint preparation.
Support structures are printed in a high-temperature breakaway material. Soluble support systems are generally avoided because prolonged bath immersion can introduce solvent uptake at the interface. After build completion, annealing at 150°C for 2 h is used to relieve internal stress, particularly in parts with uneven wall thickness. Annealing does not substantially increase crystallinity because the polymer is amorphous; its function is stress relaxation and dimensional stabilization before inspection and fitment.
Typical application environments include aircraft cabin interior duct housings, instrument panel prototypes, rail interior bracketry, and short-run tooling fixtures that must survive heated paint cycles. In these applications, final-part validation is required because printed-part anisotropy cannot be ignored. Isotropic resin data do not substitute for specimen testing on the production FFF cell using ASTM D638, ASTM D648, and the applicable flame test method. Supplier documentation states that the base resin is compliant with RoHS 2011/65/EU and REACH SVHC restrictions at the time of supply; end-use printed parts require separate verification because processing aids, support residues, and colorants may change the compliance boundary.