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