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3D Systems Figure 4™ TOUGH-GRY 10 Plastic

    • Название продукта: 3D Systems Figure 4™ TOUGH-GRY 10 Plastic
    • 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 244161

    Как аккредитованный завод 3D Systems Figure 4™ TOUGH-GRY 10 Plastic, мы соблюдаем строгие протоколы качества - каждая партия подвергается строгим испытаниям для обеспечения последовательных стандартов эффективности и безопасности.

    Упаковка и хранение
    Упаковка
    Доставка
    Хранение
    Применение 3D-систем Figure 4™ TOUGH-GRY 10 Plastic

    Snap-fit enclosure prototyping for portable industrial controllers with wall sections between 1.2 mm and 2.0 mm is typically executed on a Figure 4 Modular system with a 124 mm × 70 mm × 196 mm vat and 405 nm DLP imaging at 30 µm layer thickness. Build orientation is rotated 12° to 18° from the long axis to minimize stair-step stress at latch roots; supports are removed from green parts prior to post-cure, and the parts are washed in a two-stage Figure 4 EZ Rinse-C bath with each stage limited to 90 seconds to avoid solvent uptake. Residual solvent is removed with 1.5 bar dry compressed air, and ribs narrower than 0.8 mm are cleared with a 0.5 mm carbide bur before UV curing. Latch deflection is measured on an Instron 5960 with a 500 N load cell at a crosshead speed of 2 mm/min in accordance with ISO 527-1; ASTM D638 Type V coupons printed in XY and Z orientations are compared, with Z-oriented tensile strength typically 12% to 25% lower due to the interlayer boundary. If the enclosure must survive 500 insertion cycles at 25°C and 50% RH, the boss ID is reamed with a 0.05 mm undersized pin gauge before press-fit inserts are installed to remove as-built waviness. Published data for prolonged thermal aging above 45°C in this snap-fit configuration is limited, so validation at the upper service temperature should include 168 h deflection recovery at 45°C.

    Automotive Mounting Clip Evaluation Under Thermal Cycling

    For passenger cabin wiring harness clips and trim mounting brackets, snap-arm recovery after repeated installation and ambient thermal swing from -20°C to 60°C is the governing requirement. The clip hinge is oriented at 30° to the build platform to avoid shear-plane delamination when the arm is deflected 1.5 mm during installation onto a 2.0 mm steel bracket. After UV post-cure, retention force is measured with a Mecmesin force gauge at 200 mm/min; the installed clip is then cycled in a thermal chamber using ISO 16750-4:2010 clause 5.3.1 temperature cycling between -20°C and 65°C, 30 cycles, with 1 h dwells. Post-cycle retention loss beyond 15% is treated as a design failure because the material’s creep modulus near the upper service temperature is less than its room-temperature value. Clips with wall thickness below 1.0 mm at the hinge root are rejected for production tooling due to breakage during lateral insertion. Direct underhood exposure above 70°C is outside the operational boundary for this resin, and amine-containing anti-squeak coatings applied before full cure can leave a tacky surface due to incomplete surface conversion; only PTFE dry-film lubricants are used on clip contact faces.

    What Limits CMM Fixture Nest Repeatability When Printed in TOUGH-GRY 10?

    In CMM holding nests and gauge datum pads, the resin is printed at 10 mm thickness with 1.5 mm sacrificial machining allowance, then finish-milled with a 1.0 mm single-flute carbide end mill at 12,000 rpm. As-printed surfaces may show flatness deviation of ±0.15 mm over a 50 mm span due to staircase and polymerization shrinkage; after machining, flatness of ±0.05 mm is practical if the part is re-inspected after conditioning. A Zeiss Contura CMM with a 0.5 mm ruby stylus and probe force of 0.2 N produces no measurable deflection when pad thickness exceeds 8 mm. Dimensional repeatability is degraded by moisture at RH > 60%; ISO 291 conditioning at 60% RH for 72 h can produce visible growth in long datum spans. Therefore, fixture nests are stored in desiccated cabinets below 30% RH and are not loaded into the CMM directly from print trays. Probe contact on unpainted faces is kept below 100 cycles per point because repeated stylus contact can burnish fine stair-step peaks and shift local best-fit alignment. If the fixture must hold an aluminum gearbox cover during scanning, locating pins are not printed; ground 3.0 mm steel dowels are press-fit into reamed holes after post-cure. Published data for long-term fixture stability beyond 6 months under shop lighting is limited, so annual CMM correlation is retained.

    During low-pressure coolant circuit prototyping for glycol-water service at 2 bar internal pressure, sealing faces are oriented upward to avoid support witness marks across O-ring grooves. The housing is printed at 20 µm layer thickness and UV post-cured, then coolant ports are tapped with an M6 × 1.0 H7 cut tap followed by a chase pass to remove micro-burrs at thread crests. Hydrostatic testing is conducted at 2.5 bar for 30 min with a pressure decay allowance of 0.05 bar; failures are most often observed at thread roots where untapped as-printed layers create a brittle shear plane. Before assembly, the housing is dried at 40°C for 4 h under 30% RH to remove surface moisture that can inhibit thread sealant adhesion. A 30-day immersion study in ethylene glycol/water at 40°C under ISO 175 is used to assess material softening; published chemical resistance data for this specific coolant mixture is limited, so organizations replicate the exact coolant formulation and sealant. Service above 45°C or continuous exposure to ester-based hydraulic fluids is outside the verified boundary and can induce microcracking around compressed O-ring grooves. Sealing faces are not lapped; instead, a 0.5 mm silicone-coated paper gasket is used to compensate for as-printed waviness.

    When TOUGH-GRY 10 Replaces Machined Acetal in Robotic End-of-Arm Tooling

    After TOUGH-GRY 10 is selected as a replacement for machined acetal in robotic end-of-arm locator pads, processing and post-machining are adjusted for edge stability under cyclic clamping impact and palletizing shock loads. Printed pads are embedded into aluminum end-effector nests with a 0.2 mm press fit; the contact surface is finish-milled to a flatness of 0.03 mm and the top face is left uncoated where friction against steel is needed. The flexural modulus is evaluated under ASTM D790-17 using 3.2 mm bars, and dry sliding against ground steel shows higher friction than machined acetal; therefore a PTFE dry-film topcoat is applied to release faces to prevent part hang-up during pallet release. Clamp pad life is bounded by edge chipping at the 0.5 mm raster lip when the robot closes at velocity above 250 mm/s without end-of-arm springs; a 0.8 mm edge chamfer machined at 45° reduces chipping. If the end-of-arm tool picks up parts from a 60°C injection mould, the pad contact temperature should be measured at the surface because creep under sustained clamp force accelerates above 50°C. Published data for impact fatigue in this specific printed pad configuration is limited, so replacement intervals are set by weekly visual inspection under 10× magnification rather than by fixed cycle count. The printed pads are not ultrasonically welded to the aluminum carrier; compressive preload via M3 stainless fasteners is used to avoid fracture at the pad wall.

    Electrical Connector Prototype Housings and Pin Retention Geometry

    With two-millimetre-pitch connector housings, rectangular pin pockets are the critical feature requiring slot width tolerance of ±0.03 mm and wall thickness at 0.8 mm. The housing is printed with the pocket openings facing upward to avoid support material filling the narrow cavities; after UV post-cure, each pocket is sized with a 0.6 mm broach and checked with a non-contact optical gauge. Pin insertion force is measured with a 50 N load cell at 25 mm/min, with acceptance between 5 N and 15 N per pin; axial pin retention is tested at 10 mm/min in a tensile wedge fixture that isolates the crimp. Heat-staking bosses are formed at 150°C with a 2 mm rounded tip and a dwell of 2 seconds; longer dwell causes surface collapse and delamination beneath the boss because the heat-affected zone extends beyond the boss diameter. Housings are evaluated for flammability under UL 94 HB at 1.5 mm thickness; if an end market requires V-0, this material is not specified. REACH Regulation (EC) No 1907/2006 and RoHS Directive 2011/65/EU Annex II declarations are obtained from the supplier SDS lot trace, but conformance is not assumed without batch-level documentation. The housing wall adjacent to the pocket must maintain 0.8 mm or thicker after broaching; thinning below 0.6 mm produces cracking during pin insertion. If the connector is exposed to chlorinated cleaning agents, cracking can occur in stressed pin pockets; mild aqueous detergent with pH 6 to 8 is used for cleaning, and solvent wiping with ketones is avoided.

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    Более подробное введение

    Within the Figure 4 projection-based photopolymerization platform, 3D Systems supplies Figure 4™ TOUGH-GRY 10 Plastic as a gray production-grade photopolymer intended for functional prototypes, manufacturing aids, and low-volume end-use parts. The material is formulated to deliver a measured balance of tensile strength, flexural stiffness, and notched Izod impact resistance; its datasheet anchors these properties to ASTM D638, ASTM D790, ASTM D256, and ASTM D648. The resin is processed on Figure 4 Standalone, Modular, and Production configurations using 405 nm UV projection, with build parameters and support structures controlled through 3D Sprint or equivalent machine software. The number 10 in the grade designation identifies the lower toughness tier within the tough-gray family, not a filler weight percentage or viscosity value. Parts printed in TOUGH-GRY 10 are supplied in a gray tone that can be machined, sanded, or painted after post-cure. Operational boundaries should be derived from heat deflection temperature under 0.455 MPa and 1.82 MPa rather than from short-term visual appearance after printing.

    Mechanical property data generated under ASTM D638, D790, and D256 conditions

    Manufacturer-reported typical values are generated after conditioning specimens at 23 ± 2 °C and 50 ± 5 % RH for 24 h. The tensile strength at break is reported near 42 MPa, tensile modulus near 1.8 GPa, and elongation at break near 9%. Flexural strength is approximately 59 MPa with flexural modulus near 1.75 GPa. The notched Izod impact result is approximately 28 J/m. Heat deflection temperature is approximately 54 °C at 0.455 MPa and approximately 49 °C at 1.82 MPa. Shore D hardness is approximately 80D. These values place the product in the semi-rigid engineering photopolymer class.

    Typical manufacturer-reported mechanical and thermal values for Figure 4™ TOUGH-GRY 10 Plastic
    PropertyTest methodTypical value
    Tensile strength at breakASTM D63842 MPa
    Tensile modulusASTM D6381.8 GPa
    Elongation at breakASTM D6389%
    Flexural strengthASTM D79059 MPa
    Flexural modulusASTM D7901.75 GPa
    Notched Izod impactASTM D25628 J/m
    Heat deflection temperature at 0.455 MPaASTM D64854 °C
    Heat deflection temperature at 1.82 MPaASTM D64849 °C
    Shore D hardnessASTM D224080D

    Build orientation introduces anisotropic mechanical response in these photocured parts. Tensile coupons built in the xy-plane typically show higher strength and modulus than those built with the tensile axis parallel to the z-axis. The difference is caused by interlayer conversion gradients and incomplete boundary crosslinking. Production lots should therefore include internal test coupons built in the same orientation and at the same layer thickness as the final parts. The notched Izod value of 28 J/m should not be compared directly with injection-molded ABS or polycarbonate without noting that ASTM D256 values are specimen-size dependent. For impact-loaded designs, edge radii and generous fillets are required because the material retains the brittle fracture behavior of acrylate-based photopolymers. The heat deflection values indicate that continuous exposure above 49–54 °C under load leads to creep and dimensional change; intermittent dry heat from machining or paint bake cycles must be kept below these thresholds.

    Processing on Figure 4 systems begins with resin cartridges conditioned to 20–25 °C. Resin below this range exhibits higher viscosity that can reduce recoating uniformity and increase the frequency of first-layer adhesion defects. The liquid photopolymer is imaged at 405 nm using machine-specific layer thickness and exposure parameters supplied by 3D Systems. After printing, uncured resin is removed with an approved solvent such as isopropyl alcohol in a two-stage wash; the first bath removes the bulk liquid, and the second bath removes residual monomer from blind holes and high-surface-area support tips. Parts are then post-cured in a UV chamber using the manufacturer-specified irradiance and duration. Insufficient post-cure leaves residual acrylate groups that lower surface hardness and increase outgassing, while excessive post-cure can embrittle thin walls and support-near surfaces. Production lines should inspect blind holes and undercuts with a borescope or ultraviolet flashlight to detect uncured pools, because trapped liquid monomer continues to crosslink during storage and generates local stress concentrations. Open vat life is shorter than sealed cartridge life; resin removed from the vat should not be returned to virgin cartridges unless the facility has validated filtration and contamination control.

    Resin storage follows photopolymer industry practice: sealed cartridges are kept at 5–30 °C, and partially used cartridges are blanketed with dry nitrogen if the facility has the capability. Low-temperature storage can increase viscosity and reduce first-layer uniformity; the cartridge should be acclimated to 20–25 °C for at least 4 h before printing. Shaking is avoided because entrained air produces voids in cured layers; slow rolling or gentle inversion is used instead. When resin is transferred from a vat, the operator should record the lot number and cumulative open time to track batch-to-batch variation in printed part color and mechanical properties.

    Where does TOUGH-GRY 10 sit within the Figure 4 gray photopolymer portfolio?

    Within the Figure 4 material set, the tough-gray grades form a progression in elongation at break and impact absorption. Figure 4™ TOUGH-GRY 10 is positioned as the lower-numbered tier in this grouping. Designers requiring greater snap-fit deflection or higher notched Izod values are directed to higher-numbered tough-gray grades under the same ASTM D638 and ASTM D256 methods. Compared with Figure 4 PRO-BLK 10, a rigid production-grade photopolymer, TOUGH-GRY 10 trades tensile modulus for increased elongation at break and is therefore used when clip towers, pressed inserts, or housing snap features are present. Compared with Figure 4 FLEX-BLK 20, TOUGH-GRY 10 retains greater tensile strength and lower elongation, which limits its use in fully flexible living hinges but improves dimensional stability in structural covers and brackets. On production workstations, the gray tone provides visual contrast against black rigid components during assembly; that is an operational benefit rather than a mechanical distinction. The material is not a direct substitute for injection-molded polypropylene or ABS; its lower notched Izod and heat deflection values require redesign of sharp corners and load-bearing bosses.

    When functional assemblies demand repeated snap-fit or threaded-insert performance

    For connectors, sensor housings, and access covers that require repeated assembly, the resin is drilled, tapped, or fitted with threaded inserts after post-cure rather than printed with internal threads alone. Cutting threads with high-speed steel tooling at spindle speeds below 1,500 rpm avoids localized softening above the 54 °C heat deflection threshold. Press-fit inserts are acceptable when the boss wall thickness is at least 2.5 mm and the hole diameter follows the insert manufacturer’s recommendation for semi-rigid polymers. Insert pull-out values should be derated from molded-plastic tables because the layered build produces lower toughness in the boss hoop direction. In functional snap-fit designs, the 9% elongation at break allows limited undercut deflection but does not permit the reversible yield of polyamide. Repeated snap-fit cycles beyond a few hundred can initiate microcracks at the undercut root; prototypes should be evaluated under ASTM D638 conditioned samples and under actual assembly speed. When metal threaded inserts are used, the resin is compatible with post-installation torque testing to ISO 898 or equivalent internal company specifications, provided the test is stopped before the boss wall cracks.

    Post-processing starts with support removal before final UV post-cure when dimensional accuracy is critical. Cured flash on support tips is removed with side cutters and sanded; wet sanding with 400–600 grit paper reduces heat and dust. The material accepts acrylic, enamel, and two-component polyurethane coatings after surface degreasing with isopropyl alcohol. Adhesion of coatings is evaluated with ASTM D3359 cross-cut tape testing; painted parts should be stored at room temperature for 24–48 h before tape pull. Dimensional stability under humid storage is governed by water absorption; unpainted parts exposed to cycling humidity can show small dimensional drift, so gauge dimensional checks should occur after a 24 h conditioning period. Machining operations—milling, drilling, reaming—are feasible with sharp carbide tooling and light depths of cut to prevent heat-induced softening near the HDT. Thread forming rather than thread cutting is not recommended in thin walls because the lower ductility compared with POM or polyamide can lead to microcracking at the thread flanks. If parts require ultrasonic welding, the process window is narrow because the photopolymer does not flow like a semicrystalline thermoplastic; published data for this specific configuration is limited.

    Long-term thermal aging at 60 °C in air can shift tensile strength and color because residual photoinitiator and acrylate groups continue to react. Parts subjected to automotive interior temperatures above the heat deflection threshold should be tested under ISO 6722 thermal aging or company-specific thermal cycling. The material does not exhibit a melting point, so flow under load is the primary failure mode. Creep testing is not part of the default datasheet; if load-bearing parts are used for more than 48 h at elevated temperature, long-term creep coupons should be generated.

    The resin is not recommended for continuous immersion in strong solvents, ketones, or chlorinated hydrocarbons. Short-term contact with alcohols and aliphatic hydrocarbons is generally tolerated but must be validated under final service chemicals using ASTM D543 or equivalent comparative immersion testing. Medical device prototypes should not be placed into production without a separate ISO 10993 evaluation, and the standard gray grade is not automatically food-contact certified under FDA 21 CFR. For jigs used in metalworking shops, Figure 4™ TOUGH-GRY 10 fixtures are machined to accept hardened steel bushings; bushing retention is maintained when the hole tolerance is machined after UV post-cure rather than printed to size. In electronics assembly, the resin is used for solder pallet housings and test sockets where short-cycle contact temperatures do not exceed the heat deflection threshold; long-term exposure to heated reflow fixtures is outside the material’s operational boundary. Printed components in this grade are also used for low-volume production of gripper fingers and robotic end-of-arm tooling; the gray color aids visual identification of wear particles, while the moderate notched Izod value requires blunt impact geometries.

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