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Processing Guidelines for CETEX Thermo-Lite PPS - TenCate

Processing Guidelines for CETEX Thermo-Lite PPS - TenCate

Processing Guidelines for CETEX Thermo-Lite PPS - TenCate

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<strong>Processing</strong> <strong>Guidelines</strong> <strong>for</strong> <strong>CETEX</strong><br />

<strong>Thermo</strong>-<strong>Lite</strong> ® <strong>PPS</strong> (Polyphenylene Sulfide)<br />

Uni-Tape <strong>Thermo</strong>plastic Composite Materials<br />

Introduction: <strong>CETEX</strong> <strong>Thermo</strong>-<strong>Lite</strong> ® <strong>PPS</strong> thermoplastic uni-tape composite materials from<br />

<strong>TenCate</strong> are processed by heating the material above the <strong>PPS</strong> melting point and molding it and<br />

cooling it under pressure to the desired shape. Because no chemical change occurs to the <strong>PPS</strong><br />

matrix, processing is very rapid. The fast processing of <strong>CETEX</strong> <strong>Thermo</strong>-<strong>Lite</strong> materials is also<br />

made possible because of the rapid crystallization rate of the <strong>PPS</strong> matrix. The key thermal<br />

processing parameters are:<br />

Melt Temperature 560�F (293�C)<br />

Typical <strong>Processing</strong> Temperature 625�F (330�C)<br />

Typical prepreg material <strong>for</strong>ms that are supplied by <strong>TenCate</strong> are shown in the Table 1. These<br />

materials are shown as examples and fiber type, resin type, fiber areal weight, and fiber/resin<br />

contents can be varied depending on specific customer requirements.<br />

TABLE 1: <strong>CETEX</strong> <strong>Thermo</strong>-<strong>Lite</strong> ® Prepreg Products<br />

Product Description<br />

<strong>PPS</strong>/Carbon Prepreg - AS-4C, 60% Fiber Weight, 150 FAW, 12" Wide<br />

<strong>PPS</strong>/Carbon Prepreg - AS-4, 67% Fiber Weight, 145 FAW, 12" Wide<br />

<strong>PPS</strong>/Carbon Prepreg - IM-2A, 66% Fiber Weight, 100 FAW, 12" Wide<br />

<strong>CETEX</strong> <strong>Thermo</strong>-<strong>Lite</strong> prepregs have been fabricated into laminates and parts using a number of<br />

different methods, including heated platen press molding, autoclave molding, matched die<br />

compressions molding, thermo<strong>for</strong>ming, roll <strong>for</strong>ming, pultrusion, tape lay-up, and filament<br />

winding. The most common methods of fabricating and finishing laminates and parts using<br />

thermoplastic materials are described in this report. The parameters and methodologies outlined<br />

in these processes should be used as guidelines in obtaining high quality structures. Careful<br />

process experimentation will generally improve the results obtained <strong>for</strong> a specific application.<br />

While the temperatures and pressures described in the following processes have been tailored to<br />

<strong>PPS</strong> based <strong>CETEX</strong> <strong>Thermo</strong>-<strong>Lite</strong> materials, the general processes are applicable to a number of<br />

other resin systems, such as Polyetherimide (PEI), Polyetheretherketone (PEEK), Polyamide<br />

(PA), et al.<br />

TENCATE ADVANCED COMPOSITES USA, INC. ISO 9001<br />

18410 Butterfield Blvd. 2450 Cordelia Road AS 9100<br />

Morgan Hill, CA 95037 Fairfield, CA 94534 USA Registered<br />

Tel 408 776 0700 Tel 707 359 3400 www.tencate.com<br />

Fax 408 776 0107 Fax 707 359 3459 E-mail: tcac-usa@tencate.com


Press Lamination: A laminate can be press molded from any <strong>CETEX</strong> <strong>Thermo</strong>-<strong>Lite</strong> prepreg by<br />

stacking two or more plies in the desired orientation into a picture frame mold, transferring the<br />

assembly to a heated platen press where it is brought to approximately 625-675�F (330-360�C) at<br />

contact pressure until the material reaches temperature. The pressure should then be increased to<br />

250 psi (1.7 MPa) and held <strong>for</strong> approximately 30 minutes. The assembly should then be quickly<br />

transferred to a chilled platen press and cooled to room temperature while pressure is maintained.<br />

Autoclave Lamination: Autoclave consolidation is used <strong>for</strong> fabricating laminates from any<br />

<strong>Thermo</strong>-<strong>Lite</strong> prepreg tape. Individual layers are stacked in the desired orientation and vacuum<br />

bagged (vacuum should be maintained throughout the entire process). A high temperature<br />

bagging material, such as Kapton polyimide should be used. The assembly should then be placed<br />

in the autoclave and brought to approximately 600-625�F (315-330�C), at which time the<br />

pressure is increased from ambient to 100 psi (6.9 bar) and maintained <strong>for</strong> around 30 minutes.<br />

The part should then be cooled to less than 200�F (93�C), at which time the pressure can be<br />

dropped to ambient, the vacuum released, and the part brought to room temperature.<br />

<strong>Thermo</strong><strong>for</strong>ming Laminates into Shapes: <strong>Thermo</strong><strong>for</strong>ming is used to convert a flat consolidated<br />

continuous fiber rein<strong>for</strong>ced laminate into a complex shape with no change in starting laminate<br />

thickness. The laminate should be heated to around 625-650�F (330-345�C) in an infrared or<br />

similar oven and then quickly transferred to a matched core/cavity mold where it can be <strong>for</strong>med<br />

at 150-600 psi (10-40 bar). For optimum properties and <strong>for</strong>mability, heating of the composite<br />

laminate should take no longer than 8 minutes. Overall part production cycle times are between<br />

2-10 minutes, depending on material thickness and part geometry. Production tooling consists of<br />

machined aluminum halves, one that has a compliant layer of cast silicone, and an associated<br />

laminate tensioning system to prevent wrinkling within the part being thermo<strong>for</strong>med.<br />

Cutting and Machining: <strong>Thermo</strong>plastic composite laminates and thermo<strong>for</strong>med parts can be<br />

machined with feed rates and tip speeds similar to those used when machining brass.<br />

The following are some general guidelines:<br />

Circular Saw: Diamond-grit-edge blade of 220 grit. Blade speed: 6000 fpm<br />

(1830 mpm) with water or soap solution as coolant. Feed rates<br />

depend on thickness.<br />

Turning Operations: Cutting Speed: 350-400 fpm (105-120 mpm) <strong>for</strong> high speed tools,<br />

1500-2500 fpm (180-455 mpm) <strong>for</strong> Stellite or carbide tools, and<br />

2000-4000 fpm (600-1200 mpm) <strong>for</strong> diamond tools<br />

Milling Operations: Tip speed: 250-450 fpm (75-135 mpm) <strong>for</strong> carbide and diamond tools<br />

Plunge feed rate: 0.5-1 fpm (0.15-0.30 mpm)<br />

Drilling Operations: Feed Rate: 0.008-0.016 in/rev (0.2-0.4 mm/rev)<br />

Drill speed: 150-300 fpm (45-90 mpm)<br />

Drill point angles: 60� <strong>for</strong> thin parts, 90� <strong>for</strong> thick parts<br />

Clearance angle: 15�<br />

Tapping: Tool rake of 0� to 5� negative<br />

Shearing: Thicknesses up to 0.125 inch (3.2 mm)<br />

TENCATE ADVANCED COMPOSITES USA, INC. ISO 9001<br />

18410 Butterfield Blvd. 2450 Cordelia Road AS 9100<br />

Morgan Hill, CA 95037 Fairfield, CA 94534 USA Registered<br />

Tel 408 776 0700 Tel 707 359 3400 www.tencate.com<br />

Fax 408 776 0107 Fax 707 359 3459 E-mail: tcac-usa@tencate.com


Joining: <strong>Thermo</strong>plastic composites can be joined via mechanical fasteners, adhesive bonding, or<br />

fusion welding.<br />

Strong adhesive bonds are possible with epoxy adhesives when <strong>PPS</strong> surfaces are cleaned with a<br />

suitable degreasing solvent (i.e. MEK), grit blasted with #100 or #200 Aluminum Oxide,<br />

re-cleaned and flame or corona treated. Grit blasting may be omitted if surface cleaning<br />

effectively removes residual release agents, oils, or other impurities. Epoxy films or pastes with<br />

cure temperatures up to 350�F (177�C), polyurethanes, acrylics, and cyanoacrylates are effective<br />

adhesives depending on specific requirements. The following adhesives represent a starting point<br />

in the search <strong>for</strong> an appropriate adhesive. Once specific application in<strong>for</strong>mation is known,<br />

however, an appropriate adhesive manufacturer should be contacted.<br />

TABLE 2: Adhesive Examples<br />

1. Cytec<br />

� FM300 (350�F Epoxy Film), 300�F Service<br />

� FM300-2 (250�F Epoxy Film), 300�F Service<br />

� FM87-1 (250�F Epoxy Film), 250�F Service<br />

� FM73 (250�F Epoxy Film), 180�F Service<br />

2. Henkel<br />

� Hysol EA9394 (RT Cure, 2-Part Epoxy Paste), 250�F Service<br />

� Hysol EA9346 (250�F Cure, 1-Part Epoxy Paste), 250�F Service<br />

� Hysol EA9330 (RT Cure, 2-Part Epoxy Paste), 100�F Service<br />

3. Vantico<br />

� Epibond 1545 (150�F Cure, 2-Part Epoxy Paste), 150�F Service<br />

� XMH 8680 (RT Cure, 2-Part Polyurethane Paste), 120�F Service<br />

Painting: <strong>CETEX</strong> <strong>Thermo</strong>-<strong>Lite</strong> ® <strong>PPS</strong> composite surfaces can be painted with a variety of<br />

products. It is recommended that a paintable (non-silicone) mold release be used, if possible,<br />

during the molding of all surfaces to be painted. If a silicone or Teflon mold release is used<br />

during molding, laminate and part surfaces may require abrasion prior to painting. In all cases,<br />

surfaces must be wiped with a suitable solvent (e.g. MEK, DuPont 3919S) to remove oils,<br />

release agents, or other impurities.<br />

Health & Safety: Health and safety in<strong>for</strong>mation on handling and processing <strong>TenCate</strong> <strong>Thermo</strong>-<br />

<strong>Lite</strong> composite materials is described in a Material Safety Data Sheet available from <strong>TenCate</strong><br />

Advanced Composites USA, Inc. To obtain this or any other in<strong>for</strong>mation about <strong>TenCate</strong> <strong>PPS</strong><br />

thermoplastic composite materials, contact: <strong>TenCate</strong> Advanced Composites USA, Inc. and<br />

Phoenixx TPC, Inc. at the addresses and telephone numbers below.<br />

TENCATE ADVANCED COMPOSITES USA, INC. ISO 9001<br />

18410 Butterfield Blvd. 2450 Cordelia Road AS 9100<br />

Morgan Hill, CA 95037 Fairfield, CA 94534 USA Registered<br />

Tel 408 776 0700 Tel 707 359 3400 www.tencate.com<br />

Fax 408 776 0107 Fax 707 359 3459 E-mail: tcac-usa@tencate.com

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