| Код ТН ВЭД | 712828 |
Как аккредитованный завод Hexcel HexPEKK EM для печати SLS, мы соблюдаем строгие протоколы качества - каждая партия подвергается строгим испытаниям для обеспечения последовательных стандартов эффективности и безопасности.
| Упаковка | Hexcel HexPEKK EM for SLS Printing is supplied in 1 kg sealed foil bags with desiccant and clear safety labeling. |
| Погрузка контейнера (20-футовый контейнер) | Hexcel HexPEKK EM for SLS Printing loaded in a 20′ FCL container, palletized, secured, and shipped with proper chemical documentation. |
| Доставка | Hexcel HexPEKK EM for SLS Printing is typically shipped as a non-hazardous, non-regulated solid powder under DOT/IATA/IMDG. It is packaged in sealed, moisture-resistant containers. Store cool and dry; avoid dust and ignition sources. Domestic and international shipping options are available with appropriate documentation. |
| Хранение | Store Hexcel HexPEKK EM powder in a cool, dry, well-ventilated area at ambient temperature and low humidity. Keep original containers tightly closed, away from heat, sparks, open flames, direct sunlight, moisture, and incompatible materials. Avoid dust generation; use local exhaust and PPE. Protect from static discharge. Maintain good housekeeping and follow supplier SDS and shelf-life guidance. |
| Срок годности | Typically 24 months when stored unopened in original packaging in a cool, dry place, away from direct sunlight. |
Hexcel HexPEKK EM is processed in high-temperature selective laser sintering equipment with a nitrogen-purged build chamber, a heated feed bed, and a build platform held inside the PEKK recrystallization band. The bed set point is not copied from a generic polyaryletherketone processing chart; it is derived from differential scanning calorimetry on each powder lot according to ISO 11357-3 and confirmed by multi-point bed-temperature profiling. A temperature spread of only a few degrees across the build surface can produce visible warpage on flat parts, so high-temperature SLS platforms with closed-loop zoning are used instead of open-loop ceramic heaters. Chamber oxygen is monitored continuously at a limit defined in Hexcel's validated machine parameter file; the limit is lower than typical polyamide-12 SLS systems because aromatic ketone oxidation at bed temperature causes discoloration and loss of interlayer fusion. Powder handling includes drying, sieving, and a controlled virgin-to-refreshed ratio; powder lot acceptance includes particle size distribution and melt-viscosity characterization by high-pressure capillary rheometry to ISO 11443 rather than low-shear melt flow index. After the build, the powder cake is cooled under a controlled thermal schedule to manage recrystallization shrinkage. Glass-bead tumbling or ceramic deburring removes semi-sintered particles from internal galleries; this surface treatment changes roughness, can affect fatigue and chemical penetration, and must be included in any validation program. Because the laser scan strategy is platform-specific, Hexcel's certified parameter file for the intended machine is required. Tensile and flexural coupons printed in the Z direction generally exhibit lower elongation at break than X/Y coupons when tested to ASTM D638-14 and ASTM D790-17; the magnitude of that difference is application-specific and must be measured on each SLS platform.
Selective laser-sintered air distribution plenums, noise-attenuating duct sections, and flight-deck ventilation adapters are produced as single-piece hollow parts with internal flow paths that subtractive or injection-molding routes cannot reproduce. A printed duct can integrate variable wall thickness, mounting flanges, and acoustic chambers without draft-angle constraints; however, the certification file must prove that the layer-fused structure resists ignition in the vertical Bunsen burner test of 14 CFR 25.853(a) and remains below the heat-release and smoke-density ceilings of 14 CFR 25.853(d). The relevant instruments are an Ohio State University heat-release calorimeter operated to FAR 25.853 Appendix F Part IV and a smoke-density chamber operated to ASTM E662. Because SLS parts retain microvoids at layer interfaces, specimen preparation must include the actual printed surface condition and build orientation, not machined test coupons. Gas toxicity is addressed separately under OEM-specific methods such as Boeing BSS 7239 or Airbus ABD0031 and AITM 3.0005; these methods require the processor to document that post-build depowdering and drying do not leave residual monomers or processing aids. Hexcel's published HexPEKK EM aerospace qualification data should be requested for the specific SLS platform and layer thickness, because flammability results from one powder-bed system do not automatically transfer to another. The test program must also establish a minimum as-printed wall thickness below which thin-layer delamination during exposure to the 35 kW/m2 heat-release condition becomes the dominant failure mode.
A patient-contact device produced from HexPEKK EM is not automatically cleared for long-term implantation simply because bulk PEKK has hydrolytic stability. The ISO 10993-1 biological evaluation plan must be applied to the exact printed surface, including any residual powder, cleaning agent, and post-processing media. Cytotoxicity per ISO 10993-5, sensitization per ISO 10993-10, and chemical characterization per ISO 10993-18 are the minimum screening studies for a material that will contact bone or soft tissue; for permanent bone contact, ISO 10993-6 implantation testing is usually added. For osseointegration cages, lattice geometry is design-dependent; strut diameter, pore size, and connectivity must be validated by micro-computed tomography rather than generic specification sheets. Published data for this specific configuration of HexPEKK EM is limited, so the manufacturer must generate implant-specific mechanical and biological data under ISO 13485 design controls. Cleaning validation under ISO 17665 steam sterilization or an alternative terminal sterilization method must demonstrate that blocky powder particles are not retained in the lattice; residual powder shedding can create particulate contamination in the surgical field. Additives used to stabilize or color the powder may become leachables after repeated sterilization, so chemical characterization must include process aids and any post-processing media. This application segment is therefore treated as a qualification program rather than a standard material substitution.
In semiconductor wafer handling, a printed contact surface must satisfy competing requirements: it must resist thermal distortion during acid vapor or plasma cleaning, it must not release condensable volatiles onto wafers, and it must not generate a surface charge that damages gate oxides. For outgassing, standard screening uses ASTM E595; a common acceptance ceiling is 1.00% total mass loss and 0.10% collected volatile condensable material when tested at 125°C under vacuum. HexPEKK EM parts must be tested after a thermal bake or vacuum conditioning step, because loose powder and absorbed moisture can inflate total mass loss values. Electrostatic discharge is assessed by surface resistivity to ASTM D257; the required range depends on the wafer handling zone, and Hexcel should state whether the EM grade is static-dissipative or unfilled. If the EM grade is unfilled, an ionizing air stream or conductive coating may be required in personnel-dispatched wafer transfer. Dimensional restraint is affected by recrystallization stresses stored during the SLS build; stress-relief annealing above the end-use temperature is necessary before precision machining of wafer nests and end effectors. Without stress relief, parts can drift after first exposure to process temperature, especially when wall thickness changes abruptly at wafer pockets. Post-machining flatness is verified with a granite surface plate and dial indicator, and the measured flatness tolerance is typically tighter than the printed part can hold directly from the powder bed.
| Application segment | Standards and methods | Measured boundary condition | Failure mode to be ruled out |
|---|---|---|---|
| Cabin air distribution plenum | 14 CFR 25.853(a), 14 CFR 25.853(d), ASTM E662 | burn length, afterflame time, peak heat release rate, smoke density | layer-plane delamination during burn or smoke obscuration |
| Implantable lattice | ISO 10993-5, ISO 10993-10, ISO 10993-18 | cytotoxicity, sensitization, leachable profile | residual powder or cleaning-agent toxicity |
| Wafer contact fixture | ASTM E595, ASTM D257 | TML ≤ 1.00%; CVCM ≤ 0.10%; surface resistivity target | volatile deposition on wafers or static discharge to gate structures |
| Downhole back-up ring | NORSOK M-710, ISO 15156, ISO 899-2 | RGD cycles, sour exposure, creep strain limit | explosive decompression fracture along Z-layer boundaries |
| Composite cure tool | helium leak test, thermal cycle survey, laser tracker | leak rate, dimensional drift after thermal soak | vacuum loss through machined toolface microporosity |
Downhole connector bodies, anti-extrusion back-up rings, and seal assembly components printed from HexPEKK EM are exposed to methane, carbon dioxide, wet hydrogen sulfide, and amine corrosion inhibitors at pressures that can exceed 69 MPa and temperatures above 150°C. A seal back-up ring is not a pressure vessel; its critical failure mode is fracture under rapid gas decompression when absorbed gas expands between layer planes. For this reason, material qualification should include explosive decompression testing to NORSOK M-710 or project-specific RGD cycles, along with sour-service compatibility under ISO 15156 and NACE MR0175 where hydrogen sulfide is present. The test specimen must be printed in the same orientation and wall thickness as the production part; machined plaques do not reproduce the layer-boundary gas absorption profile. Creep is evaluated by compressive creep or tensile creep at temperature using techniques such as ISO 899-2, but creep data alone do not indicate whether a low-permeability skin remains intact through layer interfaces. The part designer must also account for SLS anisotropy in bearing strength, because back-up rings loaded across the Z direction can split at layer boundaries at lower load than in-plane coupons. Powder removal from blind retaining grooves is another processing constraint; internal channels require vacuum extraction and repeated tumbling with ceramic or glass bead media, which can alter surface roughness and dimensional tolerance. Published data for HexPEKK EM under a complete downhole qualification matrix is limited, especially for repeated RGD cycles after thermal ageing, so service-specific testing is mandatory. Elastomer compatibility must also be checked because plasticizers and amine scavengers in seal compounds can migrate into the polymer surface and change stress-crack resistance under sustained gland load.
For composite cure tooling printed from HexPEKK EM, the largest economic risk is not material softening at autoclave temperature but helium leakage through the machined toolface after repeated thermal cycling. The tool is usually printed as a hollow egg-crate or lattice-backed shell with a solid toolface; the toolface is machined and sealed, while the backing structure reduces thermal mass and improves heat-up uniformity. The failure mode observed on production tools is progressive vacuum leakage through layer-plane porosity, especially when the tool surface is machined thin to reduce mass. A helium leak test to a project-specific acceptance level is applied before first use, and tools are re-tested after several thermal cycles. Dimensional stability is verified by laser tracker or photogrammetry after a thermal soak; a shift of even 0.25 mm across a 1 m tool can cause trim and assembly mismatch. Because PEKK has a lower coefficient of thermal expansion than tooling board or epoxy tooling, the printed tool can reduce spring-in compensation factors in high-temperature laminate processing, but the exact compensation must be derived from a flat laminate study rather than assumed. The build envelope and powder-bed temperature uniformity of the SLS platform determine the maximum unsupported tool span; oversized tools are split and bonded, and the bond line must be located away from highly loaded vacuum edges. Moisture absorbed by the printed backup structure during storage must be baked out before bagging because water outgassing at cure temperature increases bag-side pressure and can create leaks at sealant joints.
Chemical processing manifolds, solvent distribution blocks, and acid-resistant valve bodies are printed from HexPEKK EM when the service environment combines aggressive fluids with temperatures that attack acetal, polyamide, or polypropylene. The printed manifold is designed with smooth internal bores, gradual radius bends, and integral ports to minimize dead volume and pressure drop. Leak tightness is not an inherent property of the SLS process; it must be demonstrated by helium mass spectrometry or pressure-decay testing to the end-user's maximum allowable leak rate. Chemical resistance is evaluated by immersion in the actual process fluid at the maximum service temperature using a method based on ISO 175 or ASTM D543, with tensile or flexural strength retention measured before and after exposure. The most severe site is not the bulk wall but the layer interface; an aggressive solvent can penetrate along residual interlayer boundaries and cause delamination under internal pressure. Holes for threaded inserts or flanges introduce additional stress concentrations; post-build heat treatment and machining with sharp tools reduce microcracking at cut edges. Users should not employ amine-based sealants or cleaning solvents without compatibility data; strong amines can stress-crack aromatic ketone polymers under sustained load. The exact pressure rating of a printed manifold depends on wall thickness, build orientation, thread design, and temperature; a single published tensile value cannot be converted into a safe working pressure without a pressure-cycling test. Because HexPEKK EM's datasheet does not typically supply long-term creep rupture data in each chemical environment, hydrostatic testing at 1.5× design pressure is a necessary factory acceptance step for pressure-bearing printed manifolds.
Конкурентоспособные цены Hexcel HexPEKK EM для печати SLS, которые соответствуют вашему бюджету - гибкие условия и индивидуальные котировки для каждого заказа.
Для получения образцов, цен или более подробной информации свяжитесь с нами по адресу +8618136850665 или отправить по почте admin@ascent-chem.com.
Мы ответим вам как можно скорее.
Телефон: +8618136850665
Электронная почта: admin@ascent-chem.com
Гибкие условия оплаты, конкурентоспособные цены, первоклассное обслуживание — обращайтесь прямо сейчас!
Hexcel HexPEKK EM is a polyetherketoneketone (PEKK) powder feedstock formulated for selective laser sintering (SLS) on high-temperature CO₂ laser powder-bed fusion platforms. The grade designation EM identifies a conductive filler system that moves the consolidated part from the electrically insulating behavior of unfilled PEKK into the static-dissipative and shielding-capable regime. The product is supplied as a free-flowing powder for use in the HexAM additive-manufacturing workflow, with part properties measured after SLS coalescence rather than on injection-molded test plaques. PEKK belongs to the polyaryletherketone family; the 2:1 ketone-to-ether ratio yields a semicrystalline morphology with a glass transition in the 160–170 °C range and a peak melt temperature near 300–315 °C as measured by differential scanning calorimetry according to ISO 11357-3:2018. In SLS, the material is processed on machines with heated build chambers capable of maintaining part-bed temperatures close to the crystallization onset, using 10.6 µm CO₂ laser energy to selectively melt powder layers. The principal differentiator from unfilled HexPEKK 100 is the controlled bulk electrical response, which is intended for avionics housings, electronics assemblies, and aircraft interior components requiring electrostatic discharge control or electromagnetic interference attenuation. The EM filler is dispersed at a size scale below the nominal SLS layer thickness, allowing the powder to flow through recoating blades and preserving a finer as-built surface than typical discontinuous carbon-fiber-filled polyaryletherketone powders.
The powder is not supplied as a one-parameter material. It requires combination with machine-specific laser power, scan speed, hatch spacing, and part-bed temperature settings. These settings are normally delivered as a validated parameter library for a specific high-temperature SLS platform rather than as a universal data sheet because the thermal history at the powder-bed surface controls crystallinity and interlayer diffusion. Hexcel supplies the material under the HexPEKK EM grade designation, with particle-size distribution and bulk density controlled to SLS requirements. Laser diffraction according to ISO 13320-1:2020 is the applicable method for powder particle-size verification; PEKK SLS feedstocks typically show a D50 near 50–60 µm and a bulk density near 0.40–0.50 g/cm³. Powder with excessive fines below 10 µm reduces flow and can form agglomerates in the recoating system, while oversize particles above 150 µm create layer defects and local porosity.
Powder conditioning precedes any machine parameter adjustment. At relative humidity above 60%, absorbed moisture on the powder surface reduces flowability and can generate porosity during laser consolidation; PEKK powders are therefore dried before use, with residual moisture held below 0.1 wt% and hopper purge gas maintained at a dew point below −40 °C. The SLS build chamber is purged with nitrogen to hold oxygen below 1.0 vol% to limit thermo-oxidative degradation. High-temperature SLS platforms must preserve part-bed temperature uniformity within ±3 °C across the build envelope because local deviations alter crystallinity and produce Z-direction curl. Layer thickness is selected in the 0.10–0.15 mm range; beam diameter, scan spacing, laser power, and scan speed are adjusted on a machine-OEM parameter library so that the applied energy density produces complete layer-to-layer coalescence without excessive melt-pool spread. Cooling after build is conducted under nitrogen at controlled rates that balance dimensional stability against excessive crystallinity; rates in the 0.5–2.0 °C/min interval are typical for PEKK SLS and must be validated for the EM filler system. Observed production-scale failure modes include powder caking in feed hoppers after moisture intrusion and part-bed edge-temperature drops of more than 5 °C that raise scrap rate. A machine with insufficient part-bed temperature capacity cannot process PEKK at the required thermal setpoint; attempts to compensate by raising laser energy density usually produce surface oxidation, porosity, and part growth rather than cohesive interlayer strength.
The consolidated HexPEKK EM part exhibits a semi-crystalline PEKK property profile modified by the conductive filler. Representative values reported for conductive PEKK SLS grades fall in the following ranges: density 1.29–1.33 g/cm³ by ASTM D792-20, XY tensile strength 80–95 MPa by ASTM D638-14, XY tensile modulus 3.8–4.5 GPa, XY elongation at break 2.5–4.0%, flexural strength 120–145 MPa by ASTM D790-17, flexural modulus 3.5–4.5 GPa, and heat deflection temperature at 0.45 MPa of 160–175 °C by ISO 75-2:2013. Z-direction properties are generally 15–30% lower than XY properties because of interlayer adhesion limits; this anisotropy is not a defect but a design input that must be carried through finite-element analysis. Surface resistivity is commonly measured on printed plaques after surface machining or cleaning with isopropanol, because powder residue or release agents can create a non-conductive skin. Values for the EM grade are specified in the static-dissipative range, typically 10⁵–10⁹ Ω/square under ASTM D257-14; electromagnetic shielding effectiveness is frequency-dependent and is measured using ASTM D4935-18 coupons or coaxial flanges. Published data for HexPEKK EM-specific shielding curves is limited, so application-specific verification must use the exact wall thickness, joint geometry, and post-processing sequence intended for production. The filler system also changes the Poisson’s ratio and fracture response relative to unfilled PEKK; Mode I fracture toughness and critical strain energy release rate should be evaluated under ASTM D5045-14 if the part contains snap-fits or press-fit inserts.
HexPEKK EM is positioned for components in which an unfilled PEKK would require secondary conductive coatings or metal shielding enclosures. In avionics chassis covers, connector housings, and antenna ground planes, the additive process can consolidate mounting bosses, cable strain reliefs, and shielding surfaces in a single build. The conductive filler system provides volume conductivity that reduces static charge accumulation; surface resistivity is evaluated according to ASTM D257-14, and charge-decay performance is assessed with instrumented charged-plate monitors or IEC 61340-2-3:2016 for the assembled part. Shielding effectiveness requirements are derived from the system-level electromagnetic compatibility specification; a 20–40 dB attenuation range is often requested over 1–10 GHz, but the part geometry and the presence of gaps or joints control the final result. Hexcel HexPEKK EM-specific shielding data should be generated on fused coupons with the production wall thickness and seam design rather than extrapolated from flat plaques. The conductive network can be disrupted by aggressive post-machining or by sanding, which can tear filler-rich surfaces and increase surface resistivity; therefore, machined surfaces should be checked on each build lot with a surface-resistance meter. The material is not a replacement for a metal shield when high shielding effectiveness above 60 dB is required across a broadband range. For ESD-safe interior panels, the critical performance parameter is usually the resistance-to-ground from the printed panel to the aircraft ground network; joints, fasteners, and gaskets must be considered separately because the printed part alone does not guarantee system-level continuity. In connector housings, dimensional change after chemical exposure must be below the clearance allowed for insert retention; a 14-day fluid immersion per ASTM D543-21 is therefore applied to representative hex-shaped housings before mating force measurements.
Unfilled HexPEKK 100 and similar unfilled PEKK SLS powders provide the highest elongation and are electrically insulating; they require conductive coatings for ESD-safe applications. Discontinuous carbon-fiber-filled PEKK grades raise tensile and flexural modulus but introduce greater anisotropy, rougher as-built surfaces, and lower elongation because of fiber alignment in the recoating direction. HexPEKK EM uses a conductive filler system formulated at a size scale below the nominal SLS layer thickness to preserve a finer surface and lower melt-viscosity penalty than fiber-filled grades while adding static-dissipative response. Table 1 summarizes the positioning of the three powder classes using publicly available PEKK SLS property envelopes and test methods. The ranges are not substitutions for the supplier certificate of analysis.
| Attribute | Unfilled PEKK | Carbon-fiber-filled PEKK | HexPEKK EM class |
|---|---|---|---|
| Surface resistivity by ASTM D257-14 | >1013 Ω/square | variable; often >106 Ω/square | 105–109 Ω/square |
| Density by ASTM D792-20 | 1.27–1.31 g/cm³ | 1.33–1.40 g/cm³ | 1.29–1.33 g/cm³ |
| XY tensile modulus by ASTM D638-14 | 3.2–3.8 GPa | 4.5–7.0 GPa | 3.8–4.5 GPa |
| XY elongation at break by ASTM D638-14 | 4–10% | 1.5–3.0% | 2.5–4.0% |
| As-built surface roughness, Ra | 8–15 µm | 12–25 µm | 8–18 µm |
Chemical compatibility screening for HexPEKK EM follows aerospace fluids exposure rather than generic immersion only. PEKK resins are generally resistant to phosphate-ester hydraulic fluids and hydrocarbon fuels; however, the conductive filler may alter surface wetting and should be tested using ASTM D543-21 immersion coupons under 14-day exposure at 60 °C. Collected volatile condensable material data for unfilled PEKK have been reported below 0.1% CVCM under ASTM E595-15, but HexPEKK EM-specific outgassing data is limited and must be requested from the supplier for space applications. The flame, smoke, and toxicity profile of the material is evaluated on finished printed parts because surface porosity and residual powder affect performance; candidate test methods include ASTM E662-21a or FAR 25.853 for smoke density and vertical burn. The EM filler system may reduce the limiting oxygen index relative to unfilled PEKK; therefore, thickness-specific qualification is required. The product is not cleared for direct food-contact use unless a separate FDA 21 CFR 177.2415 or equivalent migration study establishes compliance for the filled formulation. In addition, the use of aggressive solvents such as methylene chloride for vapor polishing should be avoided because solvent penetration can swell the conductive network and alter surface resistivity; if surface smoothing is required, mechanical abrasion followed by controlled reconditioning is preferred.
SLS does not require sacrificial support structures in the same sense as vat photopolymerization; the powder bed supports overhangs, but non-fused powder must be removed from internal channels, blind holes, and honeycomb-type features using compressed air, low-frequency vibration, or water-jet cleaning if permitted by the qualification. Post-machining of HexPEKK EM produces a discontinuous conductive network at machined surfaces; reaming or tapping holes can remove conductive filler-rich surface layers and alter resistivity. Batch-to-batch variation in filler dispersion can produce local surface-resistivity differences of up to one decade; therefore, quality control should include conductivity coupons from each build. Recycling of used powder must follow the machine OEM’s refresh rate; excessive recycle ratios reduce elongation and shift melt flow because of repeated thermal exposure. The powder bed temperature that yields optimum surface finish may differ from the temperature that maximizes XY tensile strength, so the process window is a compromise that should be locked by design of experiments rather than by single-variable changes. Parts requiring dimensional stability after humid aging should be conditioned at 23 °C and 50% RH for 48 h before final inspection; machinists should expect edge breakout when drilling thin walls below 0.8 mm and should use sharp polycrystalline diamond tooling. Internal threads in printed holes often require threaded inserts or helicoils because tapped PEKK does not provide metal-like thread durability; insert installation should be preceded by surface-resistance checks to ensure the conductive path remains intact. X-ray computed tomography according to ASTM E1570-21 can be used for internal porosity inspection; porosity below 2% is typical after optimized SLS, but local pores at recoating edges may be higher and must be considered for pressure-containing parts.